327 Sentences With "oleo" | Random Sentence Generator

Oleo will keep, refrigerated, for up to one month. 3.

By the time your tea's cooled down, your oleo saccharum will be ready.

Make the oleo: Combine the sugar and lemon peels in a zip lock bag.

Recipes: What-You-Will Punch | Serpent's Tooth | Blood-Orange Oleo-Saccharum cooking cooking cooking

Peter, who was just a boy, who ate oleo on white bread for dinner.

It's the Kumquat, made with brown butter-washed rum, apple juice, kumquat oleo, and spices.

My first entry, after having plowed through the clue list twice, was OLEO at 16 Across.

When we talk about "shortening" in crossword puzzles, we're either talking about OLEO or an abbreviation.

Oleo 100 has been registered for use in vehicle fleets such as trucks and buses, but not passenger cars.

You could eat this meal with a fresh baguette or toasted white bread spread with oleo and still record a win.

OLIO means "Mélange," or a miscellaneous collection of things, while OLEO is a type of margarine or spread made from vegetable oils.

Servings: 1 Total: 15 minutes Ingredients: for the mint bols: 20 grams fresh mint 10 ounces bols genever for the oleo saccharum: 123 lemons, zest only 10 grams granulated sugar 1 cup fresh lemon juice for the cocktail: 5 dashes angostura bitters 5 dashes orange bitters 2 ounces mint bols 1/4 ounce oleo mint sprig, to garnish Directions 1.

The new fuel, called Oleo 100, will be made from French rapeseed only and produced in Avril's existing factories, its chief executive Jean-Philippe Puig told reporters.

The only hard work involves making the secret sauce known as oleo saccharum, a blend of lemon peels and sugar that's the basis for many classic punches.

We're talking ETUI (needle case), APSE (section of a church) and OLEO (a type of margarine), which is not to be confused with OLIO (a miscellaneous collection).

"One morning I went out to my truck to go to work and there were about a hundred bars of oleo surrounding my vehicle," Mr. King said.

My favorite clue that I've not yet had a chance to use in one of my own puzzles: "I can believe it's not butter" for OLEO. 10.

This newly identified fatty taste was named "oleogustus" in the study, as the Latin term "oleo" is a root for oily or fatty and "gustus" refers to taste.

In a previous round, Brazilian independent oil firm Ouro Preto Oleo e Gas had joined British-based Seacrest Capital and Anglo-French firm Perenco to deliver a bid.

He combined the infused Bols with some oleo saccharum—a combination of sugar and lemon juice that hung out overnight with some lemon peel—and shakes in some bitters.

Made with Bols Genever and oleo saccharum, which might sound slightly scary to the home mixologist, just know that it only requires a little forethought and a few easy steps.

I was obsessed with the song "Oleo Strut" for a very long time and it remains a huge touchstone for me when trying to accomplish a lot with very little.

Although Lauren geo-tagged all of her pictures "Cancún, Quintana Roo," instead of Óleo Cancún Playa like Cameron, she used the hashtag "#OleoCancunPlaya" or "#Oleo" for a number of her beach pictures.

The process kicked off in mid-2018, when Petrobras entered exclusive talks to sell the asset to a consortium composed of Ouro Preto Oleo e Gas and private equity firm EIG Global Energy Partners.

Avril's aim is to produce "several hundred thousand tonnes" of Oleo 100 per year, out of the group's total annual biodiesel output in France of between 1.5 million and 1.6 million tonnes, he said.

The oil companies OGX Petroleo and OGX Oleo e Gas and mining company MMX, which were founded by Batista, said on Monday he no longer holds administrative roles and his arrest would have no material impact on them.

SAO PAULO (Reuters) - Brazilian energy company Ouro Preto Oleo e Gas delivered the highest bid to acquire a pair of Brazilian oil clusters from state-run oil company Petroleo Brasileiro SA, two sources with knowledge of the matter said.

The oil companies OGX Petroleo e Gas SA and Oleo e Gas Participações SA and mining company MMX , which were founded by Batista, have said he no longer held administrative roles, and his legal woes would have no impact on them.

The oil companies OGX Petroleo e Gas SA and Oleo e Gas Participações SA and mining company MMX, which were founded by Batista, said on Monday that he no longer held administrative roles, and his arrest would have no impact on them.

Perishable ingredients like fresh fruit or even lemon juice can quickly cause a cocktail to turn rancid, which is why the team turned to shrubs or oleo saccharum, made by extracting the aromatic oils from lemon peel with sugar, to add brightness.

RIO DE JANEIRO, July 29 (Reuters) - Brazil's Petrobras has signed a two-year contract to lease a drilling rig from Ocyan, formerly known as Odebrecht Oleo e Gas, an executive told Reuters, in the first deal between the firms since a corruption scandal erupted five years ago.

Among the possible bidders for the firm's Pampo and Enchova shallow-water fields are Trident Energy, backed by private equity firm Warburg Pincus, and a group composed of Brazilian independent oil firm Ouro Preto Oleo e Gas, UK-based Seacrest Capital and Anglo-French firm Perenco, said the sources.

Trident Energy, an independent oil company backed by private equity firm Warburg Pincus, is in the pole position, though Petrobras has invited other firms to submit a final bid, including Rio de Janeiro-based Petro Rio SA and a consortium of EIG Global Energy Partners and local independent Ouro Preto Oleo e Gas, the sources said.

Oleo supports editing the same spreadsheet in concurrent application instances.

The aircraft had a fixed, tailwheel undercarriage with a track. Messier oleo strut landing legs were mounted on the wing spar. Legs, mainwheels and the steerable tailwheel, also on an oleo strut, were enclosed in fairings.

The mainwheels have oleo-pneumatic damping and mechanical brakes; the nosewheel swivels.

Resinoids are extracts of resinous plant exudates (balsams, oleo gum resins, and natural oleoresins).

All were fabric-covered. The amphibious N-2C had mainwheels on short oleo strut legs close to the hull sides with rear drag struts and an oleo tailskid at the extreme rear fuselage. Wheel retraction was manual and took about 30 seconds.

The KAL-2 has a retractable tricycle undercarriage with oleo-pneumatic shock absorbers and hydraulic brakes.

Gerry Strey. "The 'Oleo Wars': Wisconsin's Fight over the Demon Spread". Wisconsin Magazine of History, vol. 85, no.

2005, pg 415 The oleo was a versatile drop for any sort of entertainment. The oleo drop often hung in the in-one position, subdividing the stage into a shallower depth that was more appropriate for a brief interlude.Beuder, Susan Crabtree & Peter. Scenic Art for the Theatre: History, Tools, and Techniques.

The original design for the oleo-pneumatic shock-absorbing strut was patented by British manufacturing conglomerate Vickers Armstrong during 1915. It had been derived from the recuperative gear design of the Vickers gun, controlling recoil by forcing oil through precisely sized orifices. Vickers' oleo strut was first applied to an aeroplane by the French aircraft company Breguet Aviation. The design proved to be viable and was extensively adopted across the aviation industry for fixed undercarriages, becoming simply referred to as an "Oleo unit" or undercarriage leg.

Upward sloping half-axles met centrally under the fuselage at the vertex of a transverse V-strut and, on each side, a faired, long displacement oleo leg and a faired drag strut, both from the lower fuselage longeron, carried the outer end of the axle. The tailskid also had an oleo strut.

The Quadro range of motor scooters use the oleo strut, which is claimed to give favourable low speed lean characteristics.

The undercarriage was fixed and conventional with mainwhels on oleo struts, enclosed in aerofoil section trouser fairings, and a skid under the tail.

The use of oleo struts for electric-powered automatic guided vehicles has also been evaluated. According to Engineering360, by 2019, the oleo-pneumatic strut had become the most common type of shock absorber in use upon modern aircraft. In particular, the oleo strut has seen heavy use amongst the largest cargo airplanes in the world, such as the Antonov An-124 Ruslan; it reportedly provides for a rough-field landing capacity while carrying payloads of up to 150 tons. This design also cushions the airframe from the impacts of taxiing, resulting in greater levels of comfort for passengers and crew alike.

Oleo saccharum ("oil sugar") is a sugar-oil mixture produced by coating citrus or other oil-rich fruit rinds in an excess of sugar. The essential oils extracted into the sugar give a concentrated aromatic mixture rich in terpenes that would otherwise not be possible through aqueous extraction processes due to the oils' hydrophobicity and volatility. In mixology, oleo saccharum can be used to sweeten beverages by their direct use or as an ingredient in flavored syrups. Oleo saccharum is a key component in many punch recipes, being listed as an ingredient as early as 1670.

A simulated oleo-pneumatic tricycle undercarriage comprises three jacks which can be lowered and dummy oleos extended. In a simulated oleo collapse, the rig lowers onto unobtrusive fixed supports. The main wheel assemblies are removable and a realistic braking system permits training in main wheel removal and fitting. The cockpit incorporates a simulated Mk10 Martin Baker ejection seat and associated safety devices.

Torsten Beyer, GNU mal wieder, iX magazine, April 1996 It claimed to be "better than the high priced spread",Oleo manual a reference to old oleomargarine advertisements promoting margarine over the more expensive butter. Oleo also worked well in a BSD environment; a FreeBSD port was available. By 1995, sc had acquired an X Window front-end called xspread, which added graphics capabilities.

Each undercarriage unit carried a single low pressure wheel, equipped with a brake, between two oleo- pneumatic legs. There was a fork-mounted tailwheel.

It has a conventional braced tailplane and a taildragger undercarriage with divided axle long-stroke oleo legs for the main gear, and a fixed tailwheel.

Its track was determined by the separation of the outer engines, as each vertical, shock absorbing oleo strut was fixed to the second wing spar within the nacelle. Instead of an axle each wheel hub was mounted on a near-horizontal V-strut, hinged on the lower fuselage longeron. The wheels had hydraulic brakes. At the rear there was an oleo-damped, steerable tailskid.

Ju 288 V1 prototype with twin BMW 801 engines. Is it being held in flying attitude by a support under the tail. The actuator rods for the landing gear's oleo struts are visible behind the main struts. The Ju 288's intricate main landing gear system's design proved to be troublesome, possessing twin vertical members comprising the main "Y-shaped" retraction strut unit, directly behind a single oleo strut,Archive photo of Ju 288 starboard main landing gear for each pair of twinned wheels mounted through a forward-projecting lever-action arm, to the lower end of the uniquely attached main oleo strut unit.

The main landing gear was sprung with oleo struts, and a castoring tailwheel was fitted on all versions except the VN model, which had a nosewheel.

The wheels, in spats, were below the outer engines with a track of . The mainwheels had independent brakes and the tailwheel castored on its oleo strut.

This single-tube oleo strut was pivoted off the lower end of the twin-member, "Y-shaped" retraction strut unit, and was rotated in the vertical plane about this single attachment in a rearwards direction during retraction of the main-gear unit, separate from the twin-member unit to help "shorten" its stowed length within the engine nacelle. This distinctive type of design required the oleo strut's freely moving top end to physically rotate downwards and aftwards during the rear-swinging retraction of the main "Y-shaped" member, operated by a lever and gear-sector system mounted on the portside of each main gear assembly, operated with a long lever that had its upper end pivoted from a fixed bracket, anchored to the firewall's rear surface. The lever/sector gear system swiveled the oleo strut about its attachment point during the retract cycle, through an arc of roughly 180º from its position when the main gear was fully extended. The stowed position of the oleo strut ended up orienting it aftwards within the rear of the engine nacelle, and placing the wheels' axle location just ahead of and above the oleo strut's pivot point when fully retracted.

It had fixed landing gear, with each mainwheel on a cranked axle assisted by a trailing drag strut, both hinged on the central fuselage underside. Tall, inward-leaning oleo struts were mounted from the same upper fuselage point as the forward wing struts. The small tailskid also had an oleo shock absorber. Its tail surfaces were round-tipped, with the horizontal tail mounted on top of the fuselage.

Recorded at the legendary Rudy Van Gelder studios, Mr. Martino chose a 12 string guitar to define his interpretations of his own compositions and "Oleo" by Sonny Rollins.

The final development of the Velocette KTT, the Mk VIII KTT was introduced in 1938 at that year's Earls Court Show, and was the first motorcycle to use the now-conventional swinging-arm rear fork with a shock absorber unit (in this case, an oleo-pneumatic unit built by the Oleo Strut Co. of England). The rear suspension system was designed by Veloce development engineer Harold Willis, and was inspired by the Oleo strut landing gear on the DeHavilland Hornet he borrowed at the Midland Aero Club, while his beloved DeHavilland 'Moth' was undergoing repair. Contact with the Oleo company led to several pairs of air shocks built for Veloce in 1936, for which the factory's racing rigid-frame racers (similar to the Mark VII KTT) were adapted with a swinging-fork rear end and bolt-on subframe for the seat. The experimental first swinging-arms used an adapted steering head lug turned sideways, with the cup-and-cone bearings retained.

Oleo is an album by New York Unit, consisting of tenor saxophonist George Adams, pianist John Hicks, bassist Richard Davis, and drummer Tatsuya Nakamura. It was recorded in 1989.

By 1931, innovations in the field were reportedly being made in the United Kingdom, France, and North America. During subsequent decades, the oleo strut became commonly used for aviation purposes around the world. By the twenty- first century, a wide range of different shock-absorbing struts were in use, but typically employ common principles, despite considerable variations in size, weight, and other performance criteria. Furthermore, continued refinements to the technology behind the oleo strut.

The system was developed by Veloce designer Harold Willis, who flew a light plane with Oleo suspension legs; he contacted the Oleo company for a special pair of air shocks, which were used by Veloce for their factory racing motorcycles from 1937 onwards, and appeared on the production KTT Mark VIII in 1938. Production of the Velocette Mark VIII KTT ended in 1949, with around 238 models built. Around 1000 KTTs were produced in total from 1929 - 1950.

It has support for macro programming, and for printing purposes it supports ASCII and PostScript output.Michael M. Murphree, Top 10 Linux console applications, Linux.com, April 26, 2005 Still, by 2000 it could not import Excel spreadsheets, while newer open source alternatives like Gnumeric offered this feature, and could also import Oleo spreadsheets.Michael Hall (June 6, 2000) Suites for the Sweet: GNOME Office, LinuxPlanet Oleo was still recommended as a console spreadsheet application in a 2005 article in Linux.

Its mainwheels had a track of and were on half axles from the lower longerons. On each side an oleo strut ran rearwards from the wheels to the centre of the fuselage underside.

Tricycle-gear Champs use the steel tube and oleo strut main gear, mating these with an oleo strut nose gear. Models 7AC, 7CCM, 7DC, and 7EC were approved as floatplanes, with the addition of floats and vertical stabilizer fins; the floatplane versions were designated the S7AC, S7CCM, S7DC, and S7EC, respectively. The 7GC and 7HC may also be operated with floats but are not given a special designation in this configuration. All floatplane versions have increased gross weights over the corresponding landplanes.

This was later changed to typing a number directly, although typing a number in a cell that already contains one appends to it rather than overwrite it.Tuxtraining.com (March 23, 2008) Oleo: a commandline spreadsheet Graphics are drawn using the device-independent library libplot, the centerpiece of the GNU plotutils. Oleo offers spreadsheet access to the GNU Scientific Library, a large collection of mathematical functions. It also offers some database connectivity, allowing access to MySQL database via queries, Xbase and DBF file access.

Oleo-Mac ed Efco are the brands for the company's gardening and forestry machines. For the general agricultural sector the reference brands are Bertolini and Nibbi, which are distributed also by agricultural machinery and tractor dealerships.

"Oleo" is a hard bop composition by Sonny Rollins, written in 1954. Since then it has become a jazz standard, and has been played by numerous jazz artists, including Miles Davis, John Coltrane, and Bill Evans.

1,597 were built. ;172H The 1967 model 172H was the last Continental O-300 powered model. It also introduced a shorter-stroke nose gear oleo to reduce drag and improve the appearance of the aircraft in flight.

An oleo strut is a pneumatic air–oil hydraulic shock absorber used on the landing gear of most large aircraft and many smaller ones. This design cushions the impacts of landing and damps out vertical oscillations. It is undesirable for an airplane to bounce on landing as it could lead to a loss of control, and the landing gear should not add to this tendency. A steel coil spring stores impact energy from landing and then releases it, while an oleo strut instead absorbs this energy, reducing bounce.

During 1954, hydropneumatic suspension was introduced, which utilizes the same principle of a gas that compresses (nitrogen) and a fluid that does not; in this application, an engine-driven pump is used to pressurize the hydraulic fluid. Another such example was a US patent filed by Jarry Hydraulics during 1958. During the 1960s, the British Ministry of Technology sponsored research into theoretical studies into improved oleo-dampening technology. In 2012, it was proposed that the vibration-dampening qualities of the oleo strut could be enhanced by using semi-active control to adjust fluid viscosity.

The church of San Giovanni in Oleo, with the Porta Latina in background. San Giovanni in Oleo is a chapel adjacent to the church of San Giovanni a Porta Latina in Rome. It commemorates the place where, according to legend, in 92 CE, at the hands of the emperor Domitian, the apostle John was immersed in a vat of boiling oil from which he emerged unharmed. Tradition relates that, having failed to execute the apostle, Domitian exiled him to the island of Patmos where John wrote the biblical Book of Revelation.

In 1998, Oleo acquired a Motif-like GUI, relying on the royalty-free LessTif widget set. A GTK version was also under development. By 1999 Oleo was still judged as "not completely usable",Larry Ayers xxl: A Free Spreadsheet for Linux, Linux Journal, January 1st, 1999 due to the awkward graphical interface lacking in user friendliness like X-style cut, copy, and paste or tear-off menus. In the 1995 version, to type a number into a cell the user had to hit the "=" key first, similar to the early versions of Excel.

Holland & Barrett are Europe's largest health food chain, with 1,400 stores. Triton Showers (the UK's largest shower company) are based in Nuneaton; Adams Childrenswear, formerly on the A4254 on the Attleborough Fields Ind Est, closed most of its stores in 2010. South of Nuneaton, at the A444/B4113 roundabout is the national distribution centre of Dairy Crest, where it also packages Cathedral City cheese. North of Coventry, Oleo International (its name is from the Oleo strut) is a world leader in railway buffers based on the B4113 in Exhall, next to the M6.

The land undercarriage was of the single-axle type, with forward-leaning oleo legs to the lower fuselage ahead of the leading edge and rearward struts. The wheels incorporated servo-assisted brakes operated from the rudder bar. The land- and seaplane undercarriages were designed to be rapidly interchangeable and shared the same attachment points, though the oleo legs were moved aft for the floats and there were additional bracing struts forward from their feet to the fuselage. The floats, linked by a pair of horizontal struts, were duralumin with a single step and water rudder.

The mainwheels were sprung on rubber blocks and were fitted with brakes; the nosewheel had an oleo shock absorber. The Prometheus 12 was a variant with a span wing to improve the performance envelope and increase structural strength.

Z-6-B users could choose between two shock-absorbing systems with either conventional inward-leaning Bendix oleo struts, extended to the upper fuselage longerons, or Goodyear Airwheels, large, low pressure balloon tyres more suitable for soft strips.

The wings are supported by V-struts with jury struts. The landing gear incorporates oleo shock absorbers on all three wheels. The nosewheel is steerable and mainwheel brakes are standard. Dual controls are standard, but cockpit doors are optional.

Faired long oleo struts were attached to the upper fuselage. The wheels had cable brakes; the pilot could choose to use them differentially operation for steering on the ground. There was a steel spring tailskid which could castor freely.

Each mainwheel was mounted on a steel tube leg hinged on the lower fuselage longeron. Together with an oleo strut, each leg was enclosed in a fairing; the wheels also had fairings and were fitted with brakes. The tailskid was steerable.

The UTC's sponsors include the Warwick Manufacturing Group at the University of Warwick, and the major local employer Jaguar Land Rover, together with local firms such as OLEO Savery and Automotive Insulations, and national companies including Bosch and National Grid.

He explained how at Guam "they eat coconuts" ("mangiano cochi") and that the natives there also "anoint the body and the hair with coconut and beniseed oil" ("ongieno el corpo et li capili co oleo de cocho et de giongioli").

These essentially identical aircraft differed mainly in undercarriage design; the PA-33 had fully cantilevered oleo-pneumatic undercarriage legs and the PA-34 had strut mounted split axles with oleo-pneumatic shock-absorbers attached to the top fuselage longerons. The fuselage was constructed of welded steel tube with fabric covering and light alloy fairings. The 3-bladed folding rotor was mounted on a braced bi- pod with legs fore and aft of the front cockpit. The tail unit consisted of a very wide chord fin and rudder with a strut supported tail-plane sporting up- turned wing-tips.

1950 brought the introduction of the Aeronca 7EC, which features a Continental C90-12F engine of , standard long-throw oleo strut main gear, thicker seat cushions, additional interior insulation for noise reduction, an improved heater and electrical system, the addition of a parking brake, and a change in center of gravity for enhanced speed. Advertised empty weight is . Standard gross weight is , or with "Lower End Landing Gear Oleo Strut Assembly." Standard fuel capacity is unchanged from the 7DC; an optional system was offered, increasing the manufacturer's empty weight by .Aircraft Specification A-759 2011, p. 6 and p. 23.

A stipulation within Term 46 prohibited the sale of margarine to the rest of Canada but allowed the manufacture and sale of margarine within Newfoundland as noted herein: After the joining of the Dominion of Newfoundland into confederation with Canada the Newfoundland Butter Company became the first margarine manufacturing plant in Canada. Due to Term 46 regarding the sale of margarine it became unlawful to ship to any other province within Canada. This turn of events did not please everyone and it drew well known Newfoundland political satirist and poet Greg Power (1909 - 1997) to write the poem The Ballad of Oleo Margarine. > The Ballad of Oleo Margarine > I pray that I shall never know > A future without oleo, > Or live to see my little sons > Turn up their noses at my buns; > But there is one with soul so dead, > Who’d sacrifice our spread for bread, > And ban from every Newfie table > Our wholesome, rich, improved Green Label.

Vietnam GI, Aug 1969 p. 4 The meeting lasted all night and when 43 men remained in the morning they were arrested by the military police for refusal to follow orders. The Oleo Strut supported the arrested soldiers and helped with their legal defense.

Its wheels were independently mounted, with axles at the vertices of V-struts hinged to the central lower fuselage and oleo strut shock absorbers from the axles to the upper fuselage. The wheels, apart, were fitted with brakes and fairings. Its tailwheel was steerable.

The Régnier 12 had a wide track, conventional undercarriage. Each mainwheel was at the end of a vertical oleo strut mounted on the forward wing spar, together with a rearward drag strut to the lower fuselage longeron. Its steel tailskid had two coil springs.

Each mainwheel was mounted on a V-strut hinged on the lower fuselage frame with a single, shock absorbing oleo landing leg to the upper frame. Undercarriage legs and struts were enclosed in dural fairings. There was a steel-shod, castoring, rubber cord sprung tailskid.

The unbalanced rudder was full and rounded. The Touroplane had a fixed, conventional undercarriage with a track of . Its mainwheels, fitted with brakes, were on split axles from the central fuselage underside. Oleo strut legs and drag struts were mounted on the lower longerons.

An olio curtain being raised and lowered An olio drop (also spelled oleo The spelling of the word olio versus oleo is disputed and vague, and is interchangeable. They are both pronounced the same.), also called olio curtain or roll drop (though never an olio drape), consists of a single large canvas called a drop, which is attached at the bottom to a long rigid tube rigged to roll as it rises out. The canvas is often decorated with a mural. Olio drops were popular in vaudeville theatre as they require a minimum of overhead space, were simple to construct, and in most cases could be operated by a single person.

The tailwheel's retraction mechanical design possessed a set of pulleys to guide the aforementioned cable to the top of the tailwheel's oleo strut, pulling it upwards along a diagonal track within the fin, into the lower fuselageAnimation of Fw 190 tailgear reaction sequence — this mechanism was accessible through a prominently visible triangular-shaped hinged panel, on the left side in the fin's side sheetmetal covering. On some versions of the Fw 190 an extended tailwheel oleo strut could be fitted for larger-sized loads (such as bombs or even a torpedo) beneath the fuselage. Most aircraft of the era used cables and pulleys to operate their controls.

Zeiger highlights the history of the coffee houses that sprang up near army bases where many of the activist meetings took place, including the Oleo Strut, where Zeiger worked as a teenager. "The GIs turned the Oleo Strut into one of Texas's anti-war headquarters, publishing an underground anti-war newspaper, organizing boycotts, setting up a legal office, and leading peace marches." Epilogue: The Myth Of The Spitting Hippie. As the U.S. military and its allies flee Vietnam in disarray in the spring of 1975, the government, the media, and Hollywood begin a 20-year process of erasing the GI Movement from the collective memory of the nation and the world.

The wheels were enclosed in fairings and equipped with brakes. Its tailskid, which protruded from the extreme fuselage tail, also had an oleo shock absorber. The Courier could also be flown as a floatplane after replacing the main gear with a pair of Edo single-stepped floats.

Typically they are applied to a high-wing monoplane and act in tension during flight. Struts have also been widely used for purely structural reasons to attach engines, landing gear and other loads. The oil-sprung legs of retractable landing gear are still called Oleo struts.

This could accommodate three passengers or two stretcher cases with a doctor. Unfurnished it could carry of mail. The Type 20 had retractable landing gear. Each mainwheel was on a vertical oleo strut under the engine and hinged on a bent axle and a drag strut, both tubular.

The Journal of Oleo Science is a monthly peer-reviewed academic journal covering the various agricultural, biological, chemical, health, medical, nutritional, and physical properties of fats and oils. It is published by the Japan Oil Chemists' Society and the editor-in-chief is Osamu Shibata (Nagasaki International University).

The aircraft produced by Maule Air are tube-and- fabric designs and are popular with bush pilots, thanks to their very low stall speed, their tundra tires and oleo strut landing gear. Most Maules are built with tailwheel or amphibious configurations, although the newer MXT models have tricycle gear.

The empennage is conventional, with the tailplane set at mid-fuselage; its elevators are balanced and fitted with trim tabs. The fin is straight-edged but the short, broad, balanced rudder is curved. The Aeroneer has a tailwheeel undercarriage. Its mainwheels are on parallel, forward-raked oleo strut legs.

A Note on the Economic Values of Chinese Tallow Tree by Puran Singh, Indian Forester (1918), Vol. XLIV, No. 9. 53\. Note on the Preparation of Turpentine, Rosin and Gum from Boswellia serrata (Roxb.) gum-oleo-resin by R.S. Pearson and Puran Singh, Indian Forest Rec. (1918) Vol.

The C.580 had conventional landing gear with a track of . Its balloon-tyred mainwheels, under large fairings, were attached by short vertical oleo struts to the wing spars. The tailskid had a case-hardened steel shoe on a rubber block fixed to a pair of welded steel shells.

The name was picked because an oleo strut is a shock absorber in the landing gear of many aircraft and the Strut's purpose was to help GIs land softly.The Clio: Oleo Strut Logo for Fatigue Press, the G.I. underground newspaper at Fort Hood army base in Killeen, Texas from 1968 to 1972 The Strut's grand opening, on July 5, 1968, was a counter-culture "love-in" at a local park that "included folk and rock performances, antiwar speeches, and copious amounts of marijuana." Among the 800 attendees were over 200 Fort Hood GIs. The Killeen establishment was not at all pleased, and by the end of the day, the local police broke up the party in riot gear.

Over the next year the Oleo Strut's staff tried various strategies in their attempts to sustain the relevance of the coffeehouse to the Fort Hood GIs. They tried being more politically left wing and opening a bookstore, they stopped being a coffeehouse, becoming more a radical political center, and they brought in live entertainment like rock bands from the nearby popular music scene in Austin. Some of these strategies were more successful than others, but by 1972, as Richard Nixon's Vietnamization strategy pulled more and more U.S. army troops out of Vietnam, the Oleo Strut was attracting very few GIs. It closed its doors for good and stopped publishing the Fatigue Press in the summer of 1972.

In order to avoid cutting the outer wing formers with outward retracting gear, Rether decided to have the landing gear retract directly to the rear. To lie flat, the wheel would have to be rotated through 90° as it retracted, with its mainwheel resting atop the lower end of the strut as with the contemporary American Curtiss P-36 Hawk fighter design. To do this, Rethel placed the main oleo strut inside a larger tube that was mounted to the pivot point on the lower leading edge of the box-spar. As the gear retracted a small arm would pull on a lever mounted to the oleo, turning the leg inside the larger tube.

A 108 hp (80 kW) Lycoming O-235 flat-four engine drove a two-blade propeller. The fixed tricycle undercarriage had rearward-sloping oleo legs mounted to the wings, giving a track of 2.40 m (7 ft 10 in). The first flight of the L-17 was scheduled for May 1956.

The R.16 had large diameter wheels, independently mounted and fitted with brakes that could be use for steering, enclosed under large fairings. Each wheel was on a cranked steel half axle from the lower fuselage with a trailing recoil strut and a vertical oleo leg to the engine mounting.

The title track was written by Milt Jackson (“Bags” is his nickname) and the three compositions written by the young Sonny Rollins all went on to become jazz standards. On "Oleo", Davis used the Harmon mute to obtain a peculiar sound, and it would become an important feature of his playing.

Oleo is an album by American jazz guitarist Grant Green featuring performances recorded in 1962 and released on the Blue Note label in Japan in 1980.Grant Green discography accessed September 16, 2010 The tracks were later re-issued in 1997 as part of The Complete Quartets with Sonny Clark.

The Sport's main undercarriage was fixed and of wide track, with the wheels on separate axles mounted on the lower fuselage longerons, as were the drag struts. Legs, including oleo struts, were mounted on the forward wing struts at points reinforced by short struts to the upper and lower longerons.

All the essential parts, including the gun's barrel and the oleo-pneumatic recoil mechanisms were manufactured by French State arsenals: Puteaux, Bourges, Châtellerault and St Etienne. A truck-mounted anti-aircraft version of the French 75 was assembled by the automobile firm of De Dion- Bouton and adopted in 1913.

McDonnell continued studies, proposing afterburning Mk.101 engines in 1962, while trials of an F-4B fitted with an extendable nosewheel oleo took place aboard in 1963. In 1964, the company proposed the model 98FC, which was identical to the F-4D variant but would have been fitted with the RB.168-25R.

The fuselage was a fabric-covered steel tube structure. The engine mountings accepted several versions of the ADC Cirrus engine, the Cirrus II, Cirrus III or Cirrus Hermes. Instructor and pupil had separate open cockpits in tandem, equipped with dual controls. Its conventional landing gear was also steel, with oleo-rubber landing legs.

Resinous plant exudates (balsams, oleo gum resins, and natural oleoresins) and animal secretions (ambergris, castoreum, musk, and civet) are extracted with solvents such as methanol, ethanol, toluene, or acetone. Yields range from 50 to 95%. The products mainly consist of nonvolatile, resinous compounds. They are usually highly viscous and are sometimes diluted (e.g.

However, Vicker's initial design had placed air above the oil, an arrangement that did not pose any problem until the introduction of retractable landing gear during the mid-1930s. The engineer Peter Thornhill devised a novel undercarriage strut that used a free-floating piston, not only being a lighter arrangement but enabling the whole strut to be inverted and to work while at an angle, eliminating the weakness of using an oil and air mixture. Oleo-pneumatic technology was subsequently reused by the manufacturer to produce several other products, including hydraulic railway buffers and industrial shock absorbers. During 1926, the Cleveland Pneumatic Tool Company designed and introduced its own oleo strut, one of the first to be purpose-designed for use upon airplanes.

Behind the wing the fuselage tapered further to a cantilever T-tail. The broad vertical tail was essentially tetragonal in profile, with a generous rudder. The horizontal tail was also tetragonal but much smaller in area. The KAI-19 landed on an electrically operated, fully retractable monowheel with an oleo strut and a disc brake.

Emak is an Italian manufacturer and distributor of machines, components and accessories for gardening, agriculture, forestry and industrial applications. Emak's brands are: Efco, Oleo-Mac, Bertolini and Nibbi. The product range comprises more than 250 models of chainsaws, brushcutters, lawnmowers, garden tractors, hedgetrimmers, rotary tillers, rotary cultivators, flail mowers, cutterbar mowers, transporters and similar products.

Animation of Ju 288 maingear retraction cycle Such a complex main gear design, with only the single pivoting retraction point for its oleo struts taking the primary stress of touchdown, was likely only one of the many potential sources of trouble causing the Ju 288's main gear units to repeatedly collapse on touchdown.

The tail unit, which shared similar construction to the wings, was fitted with a cantilever fin, a braced tailplane, while the elevators were furnished with Flettner tabs. The P.24 was provided with a conventional "scissor-type" fixed landing gear arrangement; each leg incorporated an independently spring oleo- pneumatic shock absorber, built by Avia.

Abe naxidwodwok oleo. Nebou jan oboita, ilong naxidwodwok: “Xidwodwok!” Xinasi xo xidwodwok iruk ni xatemeni xa nebou: “Kwek.” Nebou inamaxi da, ilong cebu: “Xidwodwok?” Abito xidwodwok iruk: “Kweek.” Nebou cebu ifirixi da ilong cebu ari: “Xidwodwok?” Abito xidwodwok cebu iruk ari ne xatemeni na nebou olama bebe: “Kweek.” Ixwa nebou ojojo oxirwat bane naxidwodwok.

Bdellium resin Bdellium , also bdellion, is a semi-transparent oleo-gum resin extracted from Commiphora wightii of India (also called false myrrh) and from Commiphora africana trees growing in Ethiopia, Eritrea and sub-saharan Africa. According to Pliny the best quality came from Bactria (today Afghanistan). Other named sources for the resin are India, Arabia, Media, and Babylon.

Downstream expansion and sustainability will be achieved by capturing the lucrative market segments that focus more on refined products such as oleo-derivatives, food, health products, and bio- fuels. The government says these projects will require funding of RM124 billion over the next 10 years with 98 percent of the funding coming from the private sector.

The undercarriage consisted of tall, strut braced oleo-pneumatic main-legs, attached at the outer engine nacelles, with a light alloy steerable tail-wheel at the end of the fuselage. A second aircraft, built as the MB.61 powered by three Lorraine 5Pc, first flew in February 1931. Neither the MB.60 or MB.61 garnered any production orders.

Normally the main undercarriage was made up of a pair of vees, sprung with oleo/spring struts and provided with brakes as standard equipment, and a free-castoring tailwheel sprung with triangulated shock cords.Simpson, 2001, p. 574 was fitted to most aircraft, although a small number for Brazil were fitted with a tail skid.Brandley, 1981, p.

The Cessna 152 is equipped with fixed tricycle landing gear. The main gear has tubular steel legs surrounded by a full-length fairing with a step for access to the cabin. The main gear has a wheelbase. The nosewheel is connected to the engine mount and has an oleo strut to dampen and absorb normal operating loads.

The tail sections were built up from steel tube and fabric-covered. The Pitcairn Mailwing had a ground-adjustable fin and in-flight adjustable tailplane. The undercarriage was of outrigger type with Oleo-Spring shock absorbers and disc brakes on the mainwheels. All versions looked very similar and changes were minor, with several fuselage extensions being the most obvious.

The split axle undercarriage used oleo-pneumatic shock absorber struts, dispensing with the bungee cords used on previous Travel Airs. It rode on 8.00 x 10 low pressure tires and was equipped with brakes. Both tailwheels and tailskids were used. A spate of accidents in Bolivia, and the resulting complaints resulted in a redesigned, taller tailskid for the Bolivian examples.

The U.S. Navy did not get into combat with the type until September 1943. The work done by the Royal Navy's FAA meant those models qualified the type for U.S. carrier operations first. The U.S. Navy finally accepted the F4U for shipboard operations in April 1944, after the longer oleo strut was fitted, which eliminated the tendency to bounce.Tillman 1979, pp. 15–17.

The latter have constant chord and carry flaps. The fin and rudder are swept, with a shallow dorsal fin. The single seat cockpit is covered with a windscreen and a separate, prominent, single piece blown bubble canopy. The Pegasus has a fixed tailwheel undercarriage with oleo-pneumatic shock absorbers within faired legs carrying the main wheels within long wheel spats.

None of the designs was selected for production orders; it has been suggested that the required performance could not be achieved within the constraints of the Specification. Construction was primarily wooden, with plywood-skinned spruce frames. The cantilever oleo-pneumatic fixed main undercarriage legs were faired with spats. The undercarriage, tail unit and outer wing panels were adapted from the Parnall Heck 2C.

Their unit was 37 Squadron, Royal Corps of Transport (Army). At least one was oleo sent to Borneo, during 'confrontation' and RCL 977, sank there, resulting from damage. Most were painted grey and had tropical canopies rigged over the cargo space. Tuesday 9 September 1947, p.2.Thousands Islands Life, The Army Landing Barges ‘Wolfe Islander 1’ and ‘Wolfe Islander 2’.

When this was done, the landing gear was slightly improved by enhancing the oleo struts and using reinforced tires. Approximately 1,300 Fw 190 Gs of all variants were new built. Due to war conditions, the manufacturing environment, and the use of special workshops during the later years of the war, the actual number of G models built is almost impossible to determine.

All configurations provided space for 180 lb (82 kg) of baggage. The mainwheels of the fixed tricycle undercarriage were mounted on almost horizontal V-form half-axles from the bottom corner of the fuselage, with vertical oleo-pneumatic shock absorber legs joining axles to the wing underside aft of the engines. Brakes were fitted. The nosewheel, mounted on a similar shock absorber.

The fin and tailplane were broadly straight-edged, carrying curved elevators and rudder. The latter extended to the keel and worked in a cut-out between the elevators. The Comet's landing gear was of the fixed, tailwheel type, with cantilever oleo strut legs from the lower fuselage frame providing a track of . Legs and wheels were enclosed in generous fairings.

Dining table, painted between 1857 y 1859, oleo sobre tela (oil on canvas) by Agustín Arrieta Pear, Quince and Psidium cajeta. In 2010 declared the Bicentennial Dessert of Mexico. Mexican cuisine is known for its blending of Indigenous and European cultures. The cuisine was inscribed in 2010 on the Representative List of the Intangible Cultural Heritage of Humanity by UNESCO.

All LeO C-30 autogyros were destroyed or captured by German forces during the invasion of France in 1940. ;Lioré et Olivier LeO C-30S: Construction number 26 was completed as the sole C-30S. ;Lioré-et-Olivier LeO C-301: Improved C-30s with uprated Messier oleo- pneumatic shock absorbers, flotation devices to facilitate ditching at sea and tripod main rotor support.

Traditional narrow street of the island. Skopelos is one of the greenest islands in the Aegean Sea. The island has a wide range of flowers, trees and shrubs. The local vegetation is chiefly made up of forests of Aleppo pines (Pinus halepensis), Kermes oaks (Quercus coccifera), a small forest of Holm oaks (Quercus ilex), Oleo-Ceratonion maquis, fruit trees, and olive groves.

Aster was a major supplier of automobile components to both vehicle manufacturers and end users. As shown in its advertising and exhibition stands, both the French parent and the English associate were suppliers of : engines, gear boxes, gears, chassis, steering gear, radiators, spark plugs, magnetos, coils, accumulators, Oleo plugs, C.M.F. and lubricators.Official Aster advertising images and posters displayed on this page.

Paul Dauenhauer (born 1980), a chemical engineer and MacArthur Fellow, is the Lanny Schmidt Honorary Professor at the University of Minnesota (UMN). He is recognized for his research in catalysis science and engineering, especially, his contributions to the understanding of the catalytic breakdown of cellulose to renewable chemicals, the invention of oleo-furan surfactants, and the development of catalytic resonance theory.

The tailplane incidence could be adjusted in-flight. Its quadrant-shaped fin mounted a rudder which extended down to the keel. The U 8 had fixed, conventional landing gear of the single axle type which was more refined than that of the U5, with a longer oleo strut to mid-fuselage and rearward drag struts. There was a short tailskid.

The fuselage was of wooden construction, plywood covered and tapering strongly in elevation to the tail. The fin was triangular and carried a semicircular rudder moving above the tailplane and elevators. The main undercarriage oleo legs were attached close to the fuselage end of the lift struts. A glazed cabin placed the pilot ahead of the two side-by-side seated passengers.

Walter Theodore "Sonny" Rollins (born September 7, 1930) is an American jazz tenor saxophonist who is widely recognized as one of the most important and influential jazz musicians. In a seven-decade career, he has recorded over sixty albums as a leader. A number of his compositions, including "St. Thomas", "Oleo", "Doxy", "Pent-Up House", and "Airegin", have become jazz standards.

The wheels were large, with low pressure tyres of 1,150 mm diameter and 250 mm width (45 × 10 in). Each unit had an axle, articulated at the lower longeron, and a pair of oleo legs fixed to the stub wing where the lift struts joined. The Latécoère 350 first flew on 2 February 1931, piloted by Antoine de Saint-Exupéry.

The project was started in 1992 by Tom Lord, and became part of the GNU initiative around 1994.Clifford Smith, , BSD Today, August 2000 At the time, the only open source alternative was the older text-based sc, both products having similar functionality to early versions of Lotus 123 or Microsoft Excel. Oleo's key bindings however were inspired from the Unix world, and similar to those used by the emacs editor, which frustrated novice users familiar with the DOS counterparts.Dean Oisboid, Novice to Novice, Linux Journal, August 1st, 1995 Oleo and sc were the first Unix spreadsheet applications to acquire a graphical user interface.Vincent Granet, The Xxl Spreadsheet Project, April 1st, 1999, Linux Journal Because Oleo was officially part of the GNU project, it was dubbed "GNU's response to Excel" in a 1996 article in iX magazine.

History of the Royal Academy, 1862 Nearly all Drummond's children from his three marriages became artists (five daughters and one son): Rose Emma from the first, Ellen, Eliza Ann and Jane from the second to Rose Hudson and Rosa Myra and Julian from the third one. After Waterloo por Samuel Drumond, obra presentada al concurso de 1816 de la ARA (Royal Academy of Arts). Oleo sobre tabla.

Aircraft Specification A-759 2011, p. 1. (Other 65-hp engines by Lycoming and Franklin were also fitted.) A supplemental type certificate allows the installation of a Lycoming O-235.Aircraft Specification A-759 2011, p. 1 and p. 23. The Champ featured a conventional landing gear configuration, with shock absorption in the main gear provided by oleo struts. The aircraft had no electrical system.

The control surfaces were horn balanced and the tail plane incidence could be trimmed in flight. The fin, too, was directionally adjustable, but only on the ground. The undercarriage was fixed, with semi-cantilever faired legs from the leading edge stubs braced high up the legs and inwards to the fuselage bottom with faired struts. The optionally spatted wheels were oleo damped and had differential brakes.

In late 1968 Sharlet visited the Oleo Strut, the highly activist GI coffee house, and nearby Fort Hood in Killeen, Texas. Run by Josh Gould and Janet "Jay" Lockard, it was associated with the strike of the "Fort Hood 43,""Fort Hood Strike", Vietnam GI, Stateside edition, September 1968, p. 1. Black troops who refused riot duty at the August 1968 Democratic National Convention in Chicago.

Haluoleo Airport (formerly Wolter Monginsidi Airport) is an airport in Kendari, South East Sulawesi, Indonesia . The previous name of the airport was named for Robert Wolter Monginsidi, an Indonesian national hero who was executed by the Dutch during the Indonesian National Revolution. Since February 13, 2010, the airport is renamed to honor Buton Sultanate's sixth sultan, Halu Oleo. The new terminal was opened on 6 April 2012.

Advert for Begbie Oleo sparking plugs from May 1904, fitted on all Aster engines The Whitlock company, based in Holland Park London, moved into the car industry in 1903 when they rebadged a 'Century' car manufactured in Willesden, London as a 'Whitlock Century'. (See 'Century' above). In 1905 'The Whitlock Automobile Company' was formed to market Whitlock-Aster cars. They produced a 10-12 h.p.

Up to four bombs could be carried on underwing racks. The specification required the Pike to fly with wheels or floats. As a landplane the Pike had a single-axle undercarriage, with a pair of oleo legs mounted at the wing root front spar and with rearward bracing. The axle carried arrester hooks, which engaged on landing with the longitudinal arrestor wires of those days.

Various types of rosin for violins, violas and cellos A piece of rosin for violins, violas and cellos Rosin is the resinous constituent of the oleo-resin exuded by various species of pine, known in commerce as crude turpentine. The separation of the oleo-resin into the essential oil (spirit of turpentine) and common rosin is accomplished by distillation in large copper stills. The essential oil is carried off at a temperature of between ° and , leaving fluid rosin, which is run off through a tap at the bottom of the still, and purified by passing through straining wadding. Rosin varies in color, according to the age of the tree from which the turpentine is drawn and the degree of heat applied in distillation, from an opaque, almost pitch-black substance through grades of brown and yellow to an almost perfectly transparent colorless glassy mass.

The fin was also triangular, with a tall, trapezoidal rudder which extended to the keel. The Wibault 220 had fixed, conventional landing gear with its mainwheels on V-struts hinged to the lower fuselage frames. The wheels were positioned below the engines, to which they were connected by vertical Messier oleo legs so that the track was a generous . The tailskid also had a Messier shock absorber and was steerable.

79 a major consideration given the Granville Brother's prior history of running a mobile aircraft repair facility.Granville, 2006, pp.11 & 13 The outrigger undercarriage oleo struts were attached to the fuselage framework with brass universal joints, to ensure that in an accident, they would shear off without buckling the fuselage framework. This was soon tested when Granny found himself in a snowstorm in February 1930 while flying between exhibitions.

The D.480 had a fixed, conventional undercarriage with a track of . Each mainwheel was mounted on a stub axle at the vertex of a V-strut hinged on the lower fuselage longeron, with a near-vertical sprung leg, with an oleo strut shock absorber, to the wing spar. The tailwheel was on a long, hinged leg close to the rear fuselage with a short, vertical shock absorber.

The fuselage is flat sided, with rounded decking into which the single piece, starboard hinged canopy merges. The cockpit seats two in tandem with the pilot in front when flying solo; dual controls are fitted. There is a baggage area behind the rear seat. The Speedtwin has a fixed conventional undercarriage, its mainwheels, fitted with hydraulic brakes, on oleo legs from below each engine, giving it a track.

Its fixed surfaces were plywood-covered; the elevators and rudders were fabric- covered with mass and aerodynamically balances. The rudders had trim tabs. The NC.510 had a fixed, conventional undercarriage with vertical, oleo shock absorber legs attached to the forward wing spar just inside the engines, braced with a strut to the rear spar. Legs and wheels were enclosed in fairings, and there was a sprung tail skid.

Bellanca 7GCAA Introduced in 1965, the Champion 7GCAA, like the 7ECA, featured wood- spar wings and oleo-shock main gear. The major difference was in the engine, which in the 7GCAA was a Lycoming O-320-A2B of . Champion switched to spring steel main gear legs in 1967. Bellanca continued production of the 7GCAA as the Citabria "A" Package (a designation apparently begun by Champion), but with no significant design changes.

A trim tab on the elevator replaced the elastic rope balance and the undercarriage was also new, each side having an oleo leg fixed to the lower fuselage longeron and braced at its lower end by a V-form strut, hinged on the fuselage centreline. At 420 kg (926 lb), its empty weight was close to that of the E.114M. Maximum speed was 170 km/h (106 mph).

Uecker with the Braves in 1962 Though he has sometimes joked that he was born on an oleo run to Illinois, Uecker was born and raised in Milwaukee, Wisconsin. He grew up watching the minor-league Milwaukee Brewers at Borchert Field. He signed a professional contract with his hometown Milwaukee Braves in 1956. With the Braves, Uecker bounced around for six years, playing with affiliates at various levels.

The F.E.6 was a larger version of their F.E.3. The aircraft was driven by a Austro-Daimler/Beardmore engine, which drove a four-bladed propeller. The tail unit was on a single steel boom which projected aft through the propeller shaft. The biplane had ailerons on both upper and lower wings, with no wing stagger, while landing gear consisted of mainwheels on oleo struts with an auxiliary nosewheel.

Although nutraloaf can be found in many United States prisons, its use is controversial. It was mentioned by the U.S. Supreme Court in 1978 in Hutto v. Finney while ruling that conditions in the Arkansas penal system constituted cruel and unusual punishment. Prisoners were fed "", described as "a substance created by mashing meat, potatoes, oleo [margarine], syrup, vegetables, eggs, and seasoning into a paste and baking the mixture in a pan".

No Sir! (2005), on the Vietnam GI anti-war movement screened in theaters across the country and recently shown on Sundance Channel, co- dedicated to Sharlet, as the director David Zeiger put it, "for starting it all."In the late 1960s David Zeiger had been a civilian volunteer at the Oleo Strut, the GI coffee house near Fort Hood, Texas. For his filmography as a writer/director, see David Zeiger-Moviefone.

A twist-beam rear suspension is very similar except that the arms are connected by a beam, used to locate the wheels and which twists and has an anti-roll effect. Some aircraft also use trailing arms in their landing gear, with oleo struts for shock absorption. A trailing arm landing gear results in smoother landings and a better ride when taxiing compared to other types of landing gear.

The aircraft's right gear touched down from the runway threshold. The left gear touched down 9 seconds later, from the threshold. Only when the left gear touched the runway did the ground spoilers and engine thrust reversers start to deploy, these systems depending on oleo strut (shock absorber) compression. The wheel brakes, triggered by wheel rotation being equal to or greater than , began to operate about 4 seconds later.

The tail surfaces were conventional with a triangular fin and tailplane, the latter mounted on top of the fuselage. The control surfaces were trapezoidal. The Osprey's landing gear was of the fixed, split-axle, tailwheel type, with a track of . The axles and drag struts were mounted on the lower fuselage longerons and the original Bendix system had short, oleo strut shock-absorbing landing legs to the engine mountings.

The engine mountings were steel tube structures supported by the longerons; the engine cowlings were most prominent above the wings. The main legs of the track landing gear, with fairings mounted on the front of, them retracted rearwards into the cowlings. The undercarriage was completed with an oleo mounted, steerable tailwheel. There were fuel tanks in the central section of the wings between both the engines and the longerons.

The M.112 had conventional, fixed landing gear. Its mainwheels, fitted with brakes, were on cranked axles and drag struts, both hinged from the lower fuselage longerons. There were short, vertical Messier oleo struts from the outer axles to the forward wing spars in the centre-section, giving it a track of . Its tailskid, which could be replaced with a wheel, castered and had twin small bungee shock absorbers.

Both the Scion and the Scion II were produced as either landplanes or floatplanes, the majority as landplanes (see the table below). On the landplanes the landing gear comprised a single wheel on each side of the fuselage, mounted on a vertical coil-spring and oleo leg inboard of the engine; there was a small castoring tailwheel mounted below the rear end of the fuselage.Barnes and James, p.287.

The fuselage tapered to the rear, where the tailplane was mounted on top and braced to a cropped triangular fin that carried a rounded balanced rudder. The Mac had conventional, fixed landing gear, with separate, cranked axles from the lower fuselage providing a track of . Its oleo strut legs were mounted on the forward wing struts at points strengthened by struts to the upper fuselage. Its tail wheel was hydraulically damped.

The tailwheel configuration was retained although new oleo legs to handle the heavier take-off weight were required. New plastic fuel tanks, still mounted between the front and rear wing spars, were of 21.5 imperial gallons capacity each, giving a total capacity of 43 gallons (195 lit.). Therefore, the practical working endurance remained at two hours or so. The fuselage was an all new design optimized for the topdressing role.

Both had divided-type, fixed, conventional landing gear with half-axles and with radius rods from the lower fuselage longerons. There were differences in the forward, shock absorbing legs; the LKL IV had oleo struts from the upper longerons and the LKL V had faired, compressed rubber legs from the bases of the forward wing struts. In 1934 the LKL IV's undercarriage was shortened, though without changing the geometry.

Structurally these surfaces were steel tube framed and fabric covered. It had fixed tailwheel landing gear with a track of . The mainwheels, equipped with brakes, were independently mounted on bent axles hinged from the central fuselage and restrained by drag struts from the forward lower fuselage frames. Each wheel had a short, vertical oleo strut from the forward part of the outer end of the wing centre- section.

The P-51A-NA modified with skis In early 1944, the first P-51A-1-NA, 43-6003. was fitted and tested with a lightweight retractable ski kit replacing the wheels. This conversion was made in response to a perceived requirement for aircraft that would operate away from prepared airstrips. The main oleo leg fairings were retained, but the main wheel doors and tail wheel doors were removed for the tests.

Both the rudder and the elevator were statically and aerodynamically balanced. The undercarriage was of a split-type configuration, being oleo-sprung and equipped with Dunlop-built wheels. The wheels, which were housed within streamlined fairings, were fitted with brakes; for conducting operations under winter conditions, skis could also be fitted to the undercarriage. According to reports from pilots who flew the B-534, it possessed excellent handling characteristics for the era.

The S.XII had conventional, fixed tailwheel landing gear with a track of . Each wheel was mounted on its own cranked axle from the lower fuselage longeron and had a rearwards drag strut from that longeron. A short, vertical Messier oleo strut was attached to the forward wing strut which was reinforced at that joint by two short struts to the fuselage side. The mainwheels had Bendix brakes and the tailwheel was castored.

At the rear the rectangular tailplane was built into the upper fuselage and carried larger area, separate, balanced elevators. The round edged fin was wire braced to the tailplane and carried a deep, round- topped rudder, also balanced. The W-100 had a fixed, wide track undercarriage, with each mainwheel on a V-form axle and drag strut hinged from the lower fuselage. A faired Messier oleo strut was attached to the upper fuselage.

Pneumatic systems like the oleo strut generally have long operating lives, and the construction is not unusually complex for maintenance purposes. Nitrogen is usually used as the gas instead of air, since it is less likely to cause corrosion. The various parts of the strut are sealed with O-rings or similar elastomeric seals, and a scraper ring is used to keep dust and grit adhering to the piston from entering the strut.

Its tapered tailplane was mounted on top of the fuselage, braced by two struts on each side to the lower fuselage, and carried narrow, full-span elevators. It had a fixed undercarriage with its main wheels on V-struts hinged from the lower fuselage and on vertical shock absorbing oleo struts to the engine mountings. The wheels were under large fairings; under the tail the D.430 had a long, leaf spring tail-skid.

A parallel development to the Consolidated PT-3 series, the XO-17 was a converted PT-3 with such refinements as improved fuselage streamlining, oleo shock absorbers, wheel brakes, balanced elevators and increased fuel capacity. It was used almost exclusively as a cross-country flying, gunnery, photographic and radio trainer. The O-17 had a removable fairing (carrying a Scarff ring mounting for one .30 cal (7.62 mm) trainable Browning machine gun}.

The fixed undercarriage features faired axleless wheels, complete with pneumatic brakes, which are attached via a pair of triangle-shaped struts onto the lower fuselage longeron. The undercarriage's vertical stresses are absorbed by an oleo-pneumatic strut bolted to the central wing's single spar and is integral with the fuselage.NACA 1933 p. 2. The D.500 was furnished with low-mounted elliptical, all-metal cantilever wing, possessing an aspect ratio of 8.9.

Undeterred, Rivers reintroduced the bill every year and made so many speeches in favor of the repeal of the tax that he was nicknamed "Oleo" Rivers.Rivers, p. 78 In 1949, he circulated a petition in the House to force the bill out of the agriculture committee and to the full House for a vote. The bill passed the House and then the Senate and was signed into law by President Truman in 1950.

There is a baggage compartment with a maximum load of . Aft of the cabin the fuselage tapers, with an upswept underside, to a tall swept fin and balanced rudder. The rectangular tailplane, externally braced from above and carrying separate, unbalanced elevators with a cut-out for rudder movement, is mounted on the fin a little above the fuselage. The tricycle undercarriage has mainwheels on sprung cantilever legs and a steerable oleo sprung nose wheel.

629, 632. The engine cowling features an inlet that draws cooling air into a tank; a pair of tinned steel oil tanks are also contained within the cowling. Welded steel construction was used for the nacelles, which attach to the centre section of the wing at four separate rubber-insulated joints. The retractable undercarriage of the Oxford was internally designed, featuring broken-braced twin oleo legs that retract rearward into each engine nacelle.

The tailplanes were mounted just below the top of the fuselage, each braced from below with a single strut and carrying a balanced elevator. A curved, deep, balanced rudder, mounted on a small fin and slightly pointed on top, worked in elevator cut-outs. The airliner had a fixed tailwheel undercarriage. The two mainwheels were mounted independently on V-struts from the lower fuselage with near-vertical oleo struts to the wing roots.

Patterned after the successful de Havilland Mosquito, the Calquín had a wooden structure similar to the FMA AeMB.2, and was the first twin-engined aircraft designed and built in Argentina. The I.Ae.24 design was based on a cantilever mid-mounted wooden (indigenous woods were used throughout) wings with fabric-covered flying surfaces. The conventional main twin-oleo undercarriage retracted into the engine nacelles while the tailwheel retracted into the aft fuselage.

It had a single propeller, mounted in a pusher configuration. The aircraft had an oleo- pneumatic undercarriage, an unusual feature for the time.Mason 1992, pp. 107–8. Plans called for the F.B.25 to mount a small searchlight in the nacelles nose, have a nosewheel to reduce the chance of the aircraft turning over during night landings, and use the same 200-horsepower (149-kilowatt) Hispano-Suiza 8 planned for the F.B.23.

Amber Books, 2004. . The main changes were corrosion protection, more powerful T700 engines, single- stage oleo main landing gear, removal of the left side door, adding two weapon pylons, and shifting the tail landing gear forward to reduce the footprint for shipboard landing. Other changes included larger fuel cells, an electric blade folding system, folding horizontal stabilators for storage, and adding a 25-tube pneumatic sonobuoy launcher on the left side.Leoni 2007, pp. 206–9.

The wings were duralumin structures, fabric covered, with simple, near-parallel interplane struts between the spars. The centre section was supported by a pair of struts from the upper fuselage on each side. Long Frise ailerons were fitted to the upper wing only. The wheeled undercarriage was a simple single-axle arrangement, with oleo legs forward to the engine bulkhead and rearward bracing struts to the root of the rear wing spar.

"Oleo" is one of a number of jazz standards to be based on the same chord progression as that employed by George Gershwin's "I Got Rhythm". Other standards which use "Rhythm" changes include Charlie Parker's "Anthropology", Dizzy Gillespie's "Salt Peanuts", and Thelonious Monk's "Rhythm-a-Ning". The A section is transcribed, whilst the B section is left empty either for the performer to improvise in, or for the rhythm section to 'comp' over.

The control surfaces were not balanced. The MB.141 had a fixed tail wheel undercarriage with a track of ; its main wheels were mounted on vertical, faired oleo struts and had brakes operated by a lever on the control column. Its small, castoring tail wheel also had a shock absorber. Its first flights were made towards the end of July 1934, piloted by Bloch's test pilot Zacharie Heu, who spoke highly of its handling.

In plan the horizontal tail was roughly elliptical, with an in-flight adjustable tailplane and single-piece elevator. The fin had a quadrantal profile and carried a near-semicircular unbalanced rudder. The A-20 had fixed, conventional landing gear, with a track of . Each mainwheel, fitted with a brake, was on a V-strut hinged from the lower longeron, almost horizontal on the ground, with a long oleo strut to the upper longeron.

The flat cabin top continued behind the cabin to the engine housing, where an 82 kW (110 hp) Alfa-Romeo 110-I 4-cylinder inverted air-cooled in-line engine was mounted in pusher configuration. The LB.2 was one of the first Italian aircraft with a tricycle undercarriage. This was non-retractable, with the mainwheels on short vertical oleo legs wing mounted at the root of the tailbooms. The nosewheel was steerable.

Its mainwheels were on faired, cranked axles hinged from the central fuselage underside, braced by drag struts hinged further aft; these members were enclosed in balsa and fabric airfoil fairings. Short, vertical oleo legs were attached to the bottom of the outer engine mountings. The wheels had independent Bendix brakes and were almost entirely enclosed in large dural tube, fabric covered fairings. A small tailwheel was mounted on a rubber- sprung pylon.

The tailplane was mounted at mid-fuselage and was braced to the fin by a single strut on each side. The control surfaces were unbalanced and the bottom of the rudder was cropped to allow elevator movement. The JG.40 had fixed landing gear, with split axles and drag struts hinged from the central fuselage underside and with vertical Messier oleo-legs from the forward wing spars. The mainwheels had hydraulic brakes.

He also executed frescoes (1658) for the church of San Giovanni in Oleo and a San Giovanni in Patmos(1660–1665) for San Giovanni in Laterano. He also painted an altarpiece of the Martyrdom of St. Lazarus for the church of Santi Luca e Martina. He also worked in Camerino; Pistoia (an Annunciation for the church of San Francesco and a Repose in Egypt for the Umilta); and Perugia (Casa Borgia-Montemellino).F. Tolomei, page 152-153.

The Journal of Oil Palm Research (formerly known as Elaeis: The International Journal of Oil Palm Research and Development) is a quarterly peer-reviewed open-access scientific journal covering research on palm oil fats, oils, and oleo-chemistry. It is published by the Malaysian Palm Oil Board and the editor-in-chief is Dr. Ahmad Parveez Ghulam Kadir (Malaysian Palm Oil Board). According to the Journal Citation Reports, the journal has a 1.564 impact factor for 2019 .

The community of El Cercado was founded in 1845 by President Pedro Santana. It previously belonged to the municipality of Bánica and was called the Sabana del Bohío, and was elevated to town by President Fernando Arturo de Meriño in 1888. The first families to settle in this area were Florencio Montero, Telésforo de Oleo, Encarnación, Manuelica y Fidel Matos and Leonardo Brito. El Cercado people have the reputation for being very hospitable, friendly and kind.

7ECA at Kyneton, Victoria Introduced in 1964, the 7ECA was the first version of the design and utilized the Continental O-200-A engine of . When introduced, it featured wood-spar wings and oleo-shock main gear. Within the first year of production, Champion began offering the Lycoming O-235-C1 engine of as an alternative to the Continental. In 1967, Champion switched to spring steel main gear legs; by then, the Lycoming engine had become the standard.

The latter were connected to a horizontal box containing the integrated oleo type shock absorbers. Its tailskid had an oil filled shock absorber. The exact date of the first flight of the DB-20 is not known but it was not long before the beginning of October 1929, flown from Mérignac by Charles Descamps, the Dyle and Bacalan test pilot. First impressions of speed and manoeuvrability were good, though the armour had yet to be fitted.

In its open position it creates a frilled, tent-like viewing frame for the performance: a top "scallop" with the rest of the curtain gathered at the sides. As it does not fully clear the stage, tabs tend to limit the audience's view, and thus it is rarely used except in very small venues; however, it requires no overhead space (like a traveler), nor does it require a track or any sandbag counterweights (like an oleo or an Austrian).

A longer, telescopic strut to mid-fuselage containing rubber rings acted as a shock absorber, though oleo struts could be fitted instead. There was a spring-steel tailskid. The AT.35 first flew in 1928 and was displayed at the Paris Salon in mid-summer. By the following spring the Anzani engine had been replaced by a Salmson 9Ad nine-cylinder radial and the aircraft consequentially redesignated as the AT.40 or as the AT.1.

By mounting the fixed undercarriage at the junction, Handley Page's designer Gustav Lachmann was able to use a weight-saving short undercarriage. Originally the intention was to save weight further with internally sprung wheels, but these proved unavailable and a heavier pair of wheels on either side, each on a standard oleo leg within a broad chord fairing was used. In the few photographs of the H.P.46 the undercarriage is unfaired. An arrester hook was fitted.

The airframe of the 175 is all metal, constructed of aluminum alloy. The fuselage is a semi-monocoque structure, with exterior skin sheets riveted to formers and longerons. The strut-braced wings, likewise, are constructed of exterior skin sheets riveted to spars and ribs. The landing gear of the 175 is in a tricycle arrangement, with main gear legs made of spring steel, along with a steerable nosewheel connected through an oleo strut used for shock absorption.

The AP had fixed, tailskid landing gear with the main wheels on split axles, each mounted together with a rear drag strut on the lower fuselage longerons. Vertical shock absorbing oleo struts were mounted on the forward wing struts at points strengthened with struts to both to the upper and lower longerons. Only four APs were built, including the prototype. One was powered by a Kinner K-5 and the other three by Kinner B-5s.

The community of El Cercado was founded in 1845 by President Pedro Santana. It previously belonged to the municipality of Bánica and was called the Sabana del Bohío, and was elevated to town by President Fernando Arturo de Meriño in 1888. The first families to settle in this area were Florencio Montero, Telésforo de Oleo, Encarnación, Manuelica y Fidel Matos and Leonardo Brito. El Cercado people have the reputation for being very hospitable, friendly and kind.

They are very similar to Class 319 units, sharing the same traction equipment and body design, but are fitted with cabs of the same design as the ABB Networker family. TOPS numbers are on the front of the cabs under the driver's window in a non-standard typeface (Plantin, the then corporate typeface of Royal Mail), and the units were numbered 325001 - 325016. The units are fitted with large round oleo buffers, and have no gangways between carriages.

Bruce 1968, p. 36.Raleigh 1922, pp. 249–250. By this time, the "pusher" configuration was aerodynamically obsolescent, but was retained to allow a clear forward field of fire. F.E.2a with original undercarriage F.E.2b with "V" undercarriage The undercarriage of the "third" F.E.2 was particularly well designed – a small nose wheel prevented nose-overs when landing on soft ground, and the oleo type shock absorbers were also appreciated by crews landing in rough, makeshift fields.

The Shelter Half opened in Tacoma in late 1968. Following the Oleo Strut's example of using a military term, it was named after a common piece of military equipment – the shelter-half. Really half a tent, soldiers each carry one shelter-half along with half the poles and other pieces, then when they camp, they pair off and erect a two-man tent. The name was meant to imply "strength through solidarity and cooperation", as well as "shelter" from the military environment.

The horizontal tail was straight-tapered but the elevators had prominent horn balances. The Amiot had a conventional fixed undercarriage with its mainwheels on axles mounted at the vertices of V-struts, with the forward components hinged on the central fuselage underside and the rear drag struts on the lower fuselage longerons. Each axle had a long oleo strut mounted on the mid-side of the fuselage, just aft of the engine. The type 130 first flew in April 1931.

Within a short time the Kinner engine was replaced with a Cessna Anzani engine of 120 HP. And the bungee landing gear was replaced with oleo type struts by Mr. Potts at McCoy airport at Dodge City, Kansas. One owner had his Sullivan for ten years and said that he liked it very much. configuration , enclosed cabin, low wing monoplane with conventional landing gear powered by a Kinner K-5. The fuselage is constructed of welded steel tubing with aircraft fabric covering.

Evans used Adderley's solo and the song's tempo to improvise, as he scattered Bud Powell-like clusters. Journalist Lindsey Planer later called the performance "slippery and triple-jointed", and went on to state "The band plays as if Monk might have been in the room that night. This is Davis at his most muted magnificence." The Sonny Rollins-penned "Oleo" followed along at a wild Paul Chambers bass tempo, as Evans' fluid orchestral piano technique suggested multiple key centers and modal impressions.

According to Tertullian, as quoted by Saint Jerome, in year 92, St John the Evangelist survived martyrdom at Rome under the Emperor Domitian by being immersed in a vat of boiling oil, from which he emerged unharmed. He was later exiled to island of Patmos. This event was traditionally said to have occurred at the Latin Gate (located on the southern portion of the Roman wall). The nearby chapel of San Giovanni in Oleo is said to be on this very spot.

The C.570's hydraulically retractable main undercarriage had wheels on Messier oleo struts which folded backwards behind the engines, giving it a track of . The C.570 had a twin tail with its tailplane mounted at the top of the fuselage. Together with the elevators it was trapezoidal in plan; the fins were of the endplate type, oval in profile and with rudders split into two sections to allow elevator movement. Both horizontal and vertical control surfaces had Flettner-type servo tabs.

American Champion has been using aluminum spars in the aircraft it has produced and has, as well, made the aluminum-spar wings available for retrofit installation on older aircraft. The landing gear of the Citabria is in a conventional arrangement. The main gear legs of most Citabrias are made of spring steel, though American Champion began to use aluminum gear legs in 2004. Early Citabrias were fitted with a steel tube main gear which uses an oleo strut for shock absorption.

It had outrigger landing gear with spring oleo shock struts, and the range was 375 miles. The sale price started out at $4,990 dollars but as the depression came it was lowered to $3,985. The first four Sport Trainers built were of a rare straight-wing design, one of which was modified into a special racer. Because of problems recovering from flat spins, the top wing was swept back and that is what most people recognize first when looking at a Sport Trainer.

Though the MN-A and the Maillet 20 had much in common, one obvious difference was in the landing gear. Both designs had mainwheels on vertical legs from the outer part of the wing inner section but the earlier model also had diagonal V-struts from axles to lower fuselage, whereas those of the Maillet 20 were cantilevers, without struttage. The legs had Messier oleo shock absorbers and mounted the wheels in forks. Both legs and wheels were enclosed in fairings.

Sonic Explorations is the debut album by American jazz pianist Matthew Shipp and alto saxophonist Rob Brown, originally issued on LP in 1988 on Cadence Jazz. Both musicians played together for about 5 years before. "Sonic Explorations" is a suite in 6 sections (including a piano solo and a sax solo section). The duo also plays jazz standards Oleo by Sonny Rollins and Blue in Green (credited to Miles Davis on Kind of Blue, but Shipp believes that Bill Evans wrote the piece).

On the prototype the axle ends were rubber sprung to faired steel V-struts from the lower fuselage longerons, though production aircraft would have had oleo strut shock absorbers. A steel spring tailskid reached out beyond the end of the fuselage. The date of the first flight is not known precisely: in early October it was described as just completed but by mid-November it had obtained its certificate of airworthiness. It was still flying at the Villacoublay test ground in February 1930.

There were access doors and rear view transparencies on both sides. At the rear, the tailplane was mounted at mid-fuselage and the fin and deep rudder were straight tapered except near the keel and almost triangular above the fuselage. The first and only SE-2300 had a fixed conventional undercarriage with oleo-pneumatic springing, faired main legs and wheels and a swivelling tailwheel. The two SE-2310s had tricycle undercarriages, the first unfaired but the second with faired legs and spats.

The Robin, a workmanlike cabin monoplane, had a wooden wing and steel tubing fuselage. The cabin accommodated three persons; two passengers were seated side-by-side behind the pilot. Early Robins were distinguished by large flat fairings over the parallel diagonal wing bracing struts; the fairings were abandoned on later versions, having been found to be ineffective in creating lift. The original landing gear had bungee rubber cord shock absorbers, later replaced by an oleo-pneumatic system; a number of Robins had twin floats added.

The high aspect ratio vertical tail comprised a fin, constructed like the tailplane and an all-metal rudder which ended above the elevators. The JG.10 had fixed, conventional landing gear, its mainwheels on bent axles with rearward drag struts, all hinged to the central fuselage underside. Vertical oleo struts from the ends of the axles were attached to the forward wing spars; the track was . A vertical tube extending from the extreme rear of the fuselage carried a small castering tailwheel below a shock-absorbing spring.

It had a finless, comma shaped rudder, a tailplane mounted on top of the fuselage, braced from below and carrying separate elevators. Tailplane incidence was adjustable from the cockpit. The undercarriage was the divided type with wide splayed main oleo legs joining the fuselage below and between the wing struts. There were bracing struts forward to the engine bulkhead and the axles sloped inwards and upwards to a post below the fuselage, all rather like a strengthened version of the on the Parnall Elf.

Its curved and slightly pointed empennage was steel- framed and fabric-covered with a rudder that extended down to the keel. The tailplane's angle of incidence could be adjusted in flight. There were separate elevators, each identical to each other and to the rudder, keeping costs down. The M.N.5 had a wide track, divided undercarriage with mainwheels on cranked half-axles hinged from the fuselage underside centreline; a Vickers oleo strut from the stub wing and a radius arm formed a V-strut on each side.

This narrow rear fuselage provided a wide rearward and downward view even from the back of the cabin where the rear gunner sat with a twin Lewis gun on a flexible mount. The tail was conventional, with a near triangular fin and straight-edged rudder. The NiD 590's tailplane was straight tapered and mounted on top of the fuselage. Its undercarriage was fixed, its mainwheels on bent axles with streamlined drag struts and short, vertical oleo struts to the forward engine mounting frame.

An improved version of the L-16, the L-16B/7CCM featured a Continental C90-8 engine, an enlarged vertical tail, hydraulic brakes, and a gross weight increase to ; an additional gross weight increase to is allowed when "Long Stroke Oleo Landing Gear" is installed and placard, "Intentional spinning prohibited when baggage carried", is installed on the instrument panel. An additional fuel tank is used, increasing total fuel capacity to .Aircraft Specification A-759 2011, p. 3. Gross weight increases to when configured as an S7CCM floatplane.

The serial number was 34-25. The only outward differences between it and the YP-29A were the addition of a one-piece wing flap similar to that of the YP-29, an additional one degree of dihedral in the wing, and an oleo tail wheel assembly similar to that of the YP-29. The YP-29B was sent to Chanute Field in Illinois for service testing. It was eventually redesignated P-29B, adding to the bewildering succession of designations for essentially the same model.

This set had audio and visual indications and operated on low volt batteries. This backpack style detecting set came with two probes, batteries, detecting plate, ple, and other basic electronics in an organized seal fiberglass box. Bendix Aviation developed and manufactured advanced carburetion for aircraft engines; landing gear oleo struts; jet engine fuel controls for early J79 engines; and designed guidance systems and assembled the Talos missile for the US Navy. Bendix aviation masks and gauges were modified and tested for use in diving and hyperbaric applications.

The AA-2 was different from the AA-1 in that it had doors instead of the Yankee's trademark sliding canopy and an oleo strut in place of the Yankee's spring steel tube nose gear. The aircraft had provisions for retractable gear to be installed on a later version, although the prototype had fixed landing gear. The AA-2 was powered by a 180 hp (134 kW) Lycoming engine. The prototype, registered "N488AA", was completed in 1970 and test flying was commenced early in that same year.

The elevators carried trim tabs. In its initial configuration the fin was longer in chord than high, carrying a nearly semicircular rudder that extended down through a cut out in the elevators to the base of the fuselage. The vertical, faired main oleo legs of the split axle undercarriage were mounted on the forward lift struts, with two more articulated struts on each side to the bases of the lift struts. The single mainwheel on each side was initially uncovered but later acquired spats.

Renault launched its R19 range, a three- and five- door hatchback aimed to compete with cars such as the Ford Escort and Volkswagen Golf. It succeeded the R9 and R11 ranges, and was powered by 1.4 and 1.7 petrol engines as well as a 1.9 diesel. Peugeot launched the 605 range, a four-door saloon with 2.0 four-cylinder and 2.9 V6 petrol engines as well as a 2.1 turbo-diesel. Citroen replaced its CX range with the XM featuring self-levelling oleo-pneumatic suspension.

Under the canopy the two seats were in tandem and had dual controls; in emergency, the canopy could be jettisoned. The Delanne 20-T had tailwheel, fixed landing gear, each of its mainwheels independent mounted on a pair of converging tubular legs to the lower fuselage. The rear member was an oleo strut shock absorber and the pair was enclosed in a fairing, as was the wheel. There was also a light strut from the bottom of the pair to the central fuselage underside.

The Southern Martlet was the first aircraft designed by teams led Frederick George Miles, whose company was Southern Aircraft of Shoreham. It was a modified Avro Baby, differing in the tail unit, undercarriage and engine, the 85 hp A.B.C. Hornet air-cooled flat four. Like the Baby, it was a single-bay staggered tractor biplane, with fixed two-wheel main and tail-skid undercarriage. The undercarriage was a combination of "oleo and coil-spring shock absorbing gear" designed by Basil Henderson of Hendy Aircraft, Shoreham.

When bonded to an ethyl group it is used for regiospecific analysis of triglycerols.Ando, Y; Tomita, Y; Haba, Y. Preparation of Ethyl Magnesium Bromide for Regiospecific Analysis of Triacylglycerols Journal of Oleo Science, 2008, 57, 459 Magnesium bromide hexahydrate is being worked with to be used as a flame retardant. It was found that if 0.125 mol/L of magnesium bromide hexahydrate was added to a cotton material it acted as a flame retardant. Magnesium bromide was used to synthesize the first stable magnesium silylenoid.

Behind the wing the fuselage tapered to the tail with the tailplane mounted on top, wire-braced from a triangular fin which carried a broad and largely straight-edged rudder. The Junior's landing gear was fixed and conventional, with a long tailskid. It had Goodyear Airwheel mainwheels, with large, low pressure tyres on split axles with semi-oleo landing struts from the upper fuselage longerons and drag struts from the lower longerons. The wheeled undercarriage was designed so it could be easily replaced by floats.

The Aeronca high- wing formula used a welded steel tube fuselage covered with fabric, wooden wings covered with plywood and fabric braced by V-struts to the rear undercarriage attachment point on the lower fuselage. Tail surfaces were also built up with welded steel tubing covered with fabric. The fixed tail-wheel undercarriage, sprung with oleo struts and faired triangular side members hinged at the fuselage. A small tail-wheel on a spring steel leaf at the extreme rear of the fuselage completed the under-carriage.

The rudder and elevator are both statically and aerodynamically balanced and carry trim tabs. The fuselage of the KAT-1 is a stressed skin alloy semi-monocoque, with a 240 hp (179 kW) Lycoming GO-435 flat-six engine installed in the nose, driving a two-blade variable-pitch propeller. Student and instructor occupy tandem cockpits fitted with dual controls under individual sliding sections in the continuous glazing. The KAT-1 has a retractable tricycle undercarriage with oleo-pneumatic shock absorbers and hydraulic brakes.

The aircraft, originally designated the F.K.7, was designed by Dutch aircraft designer Frederick Koolhoven as a replacement for the Royal Aircraft Factory B.E.2c and the Armstrong Whitworth F.K.3. It was a sturdier aircraft than the F.K.3, with a larger fuselage and wings, and was powered by a 160 hp (110 kW) Beardmore water-cooled engine. The undercarriage used oleo shock absorbers and the observer was equipped with a Scarff ring mounting for a .303 in (7.7 mm) Lewis machine gun.

The prototype and the -14 variant have fins with a full rounded leading edge but those of the -2 and -3 are straight edged and vertical. A fixed, conventional undercarriage with a small tailwheel has mainwheels on faired V struts hinged on the lower fuselage. On all but the -3, half-axles with bungee cord shock absorbers run to a central compression frame. The -3 variant has instead oleo legs attached to the outside of the V struts and to the mid fuselage sides.

The Perch had a two-wheel, solid-axle undercarriage, mounted on oleo legs joined to the fuselage close to the leading edge of the wing and the engine bulkhead. It was braced by rearward struts. The same legs and struts were used when wheels were replaced by floats, though they were augmented with a pair of struts about two-thirds the way along the float, steeply angled back to the lower fuselage. The floats had a step close to their tip; there was no water-rudder.

This movement compresses the gas, which acts as a spring, and forces oil through the orifice, which acts as a damper. A tapered rod is used on some designs to change the size of the orifice as the piston moves, providing greater resistance as compression of the strut increases. Additionally, a check valve is sometimes used to uncover additional orifices so that damping during compression is less than during rebound. Oleo struts absorb and dissipate forces by converting and emitting a portion of the accumulated kinetic energy into thermal energy.

Elevators and rudder were covered with fabric, aerodynamically balanced in the Ar 77A and without aerodynamic balance horns in the Ar 77B. The fixed tailwheel undercarriage consisted of cantilevered oleo-pneumatic main leg struts fitted with brakes and a tailwheel under the rear fuselage. The four crew members, being pilot, navigator or instructor, and two students, were accommodated in a cabin with full-length windows along the fuselage sides. The Arado Ar 77 was characterised by the relatively low placement of its engines in relationship to the wings.

Some instruments like the fuel gauge are visible from either seat. At the rear the tail also has a steel tube structure. The tailplane and elevators are mounted on top of the fuselage and the fin and unbalanced rudder have a rounded profile. The landing gear is fixed and of the split axle type, with mainwheels on V-struts from the central fuselage underside and with vertical oleo struts from the outer axle to the wing leading edges, where single bracing struts connect to the upper fuselage longerons.

On September 18 and 19 the FTA performed in Killeen, Texas just outside Fort Hood Army base and then in San Antonio on the 20th. Again the organizers had applied for permission to perform on base and had been denied. They then applied to rent the local high school auditorium and, when that was turned down, took the issue to court. The day before the first scheduled show the court denied their petition forcing the performances into the relatively small local GI Coffeehouse, the Oleo Strut, whose maximum legal capacity was 250.

Additionally, an uncommon Champ variant—the 7HC—was produced with an enlarged rear seat allowing 2 passengers to be carried. The landing gear of most Champs is in a conventional arrangement, though two variants with tricycle gear were produced, and a model with reversed tricycle gear was tried. Conventional-gear Champs feature a steerable tailwheel and most have steel tube main gear which use an oleo strut for shock absorption. One variant utilized sprung-steel main gear, and American Champion uses aluminum gear legs in its production model of the Champ.

Under the Hood Cafe describes itself as being part of the tradition of The Oleo Strut, a famous GI coffee house during the Vietnam war. The cafe continues in this tradition by hosting the Fort Hood chapter of Iraq Veterans Against the War, which holds its meetings at Under the Hood. In 2009, the coffeehouse was the staging area for the first anti-war marches in Killeen since the Vietnam War. It also provided support for two war resisters, Victor Agosto and Travis Bishop, in their public campaigns against the War in Afghanistan.

32 and Percival P.20 were also proposed against specification T.1/37, but not accepted for being built as prototypes. None of the designs was selected for production orders; it has been suggested that the required performance could not be achieved within the constraints of the Specification. Construction was primarily wooden, with plywood-skinned spruce frames, open framed movable flying surfaces, some monocoque sections, all fabric-covered. The cantilever oleo-pneumatic fixed main undercarriage legs were raked forward and faired with spats, and the tailwheel was also spatted.

It continued to stick half- closed when retracted, although luckily it returned to the down position for landing. Repeated attempts to find the problem were fruitless, when they put the plane on blocks in the hangar it would always work flawlessly. Eventually, it was found that the air pressure on the front of the strut in flight made the oleo jam in its tube so it couldn't rotate. Another problem discovered during construction of the V1 was that Rethel's monocoque technique in fact turned out to be much heavier than expected.

Liss 1970, p. 7. The all-metal fuselage of the P.11 was matched to a twin-spar shoulder- mounted wing (which was also all-metal) via bearers set upon the upper portion of the first and second fuselage frames. The wing and the tail employed similar construction techniques, making use of Daude-type rivets, a corrugated duralumin sheet exterior and solid duralumin struts and plates for strengthening. The undercarriage comprised V-shape streamlined struts, furnished with Avia-type oleo pneumatic shock absorbers (including the tail skid) and were braced with steel wire.

Historically, coupling chains were no more than that, a short length of heavy chain (typically three links long) with no adjustment. These would result in a 'loose-coupled train' in which the buffers of adjacent vehicles would only touch when the coupling chain was fully slack, such as when being pushed or going down hill. Although the buffers in the very earliest days of railways were rigid (dumb buffers), they soon came to be spring-loaded, while those fitted to modern locomotives and rolling stock incorporate oleo-pneumatic shock absorbers.

The C3 was a rugged biplane with simple straight wings, a tough undercarriage with oleo shock absorbers and two open cockpits with the pilot in the rear and two side- by-side passenger seats in the front. In fact, it was a slightly modified version of the earlier model C2 aircraft. Changes included an increased volume oil tank and larger sized baggage compartment. Introduced in 1928, the C3 was powered by a variety of engines of between 128 hp and 225 hp, each version having its own designation.

Ginter 1995, p. 31. Operational testing by the Naval Air Test Center at Naval Air Station Patuxent River that included carrier acceptability tests revealed additional problems: The piston engine tended to overheat until electrically operated cowl flaps were installed, the catapult hooks had to be moved, and the nosewheel oleo shock strut had to be lengthened by . Carrier suitability tests began aboard the escort carrier in early January 1945. The aircraft successfully made five catapult takeoffs using the piston engine as well as three takeoffs using both engines.

The fin and rudder were tall and rounded; the latter extended down to the keel and worked in a cut-out between the elevators. The Courier had split-axle, tailskid landing gear with its bent axles articulated from a small pyramid of steel tubes from the fuselage underside centre-line and with drag struts back to the centre-line. Another, longitudinal, tube from the drag struts' meeting point braced the pyramid. Long-travel oleo struts to the upper fuselage, medium pressure tyres and a track of assisted landings on rough ground.

The doors were "bowed" out to give three more inches of shoulder and hip room which was needed in the small cabin. The "G" model also saw a new short-stroke nose oleo introduced to reduce the drag created by the nosewheel assembly. The previously fitted generator was replaced by a 60-ampere alternator, reflecting the increasing avionics that the planes were being fitted with. The "G" model was also the first Cessna 150 variant certified for floats. A total of 2114 "G" models were built, plus 152 built by Reims as F150G.

A partition separated him from the instructor and his access was by an upward-hinged door on the starboard side which gave access to the full length of the space behind the primary cockpit. Alternatively, the roof could be retained and the clear, ventilated compartment space used to carry a stretcher, supported above the floor on oleo struts and loaded via the side door. The tail of the Styx was conventional, with horizontal surfaces mounted on top of the fuselage. They had ply-covered dural frames and were tapered in plan with rounded tips.

Other modifications to the Goshawk included its reinforced airframe, the adoption of a more robust and widened landing gear, complete with a catapult tow bar attachment to the oleo strut of the new two-wheel nosegear design,"T-45A fact file." US Navy, Retrieved: 15 September 2017. and an arresting hook. Additionally, the wingtips were squared off, a 6-inch (0.152 m) extension to the tail fin and an increased span tailplane (which was also furnished with squared-off tips) were installed, along with a single ventral fin in front of the arrestor hook.

All versions of the Couzinet 100 had fixed, tailwheel landing gear. When the Couzinet 100, powered by Salmson 9 ADb radials made its first flight it had mainwheels in trouser fairings and relied on low pressure tyres to absorb landing shocks. One flight was enough to see its return to the factory, where a more conventional three strut arrangement was installed. The Couzinet 101 had similar gear, each wheel with a near-vertical oleo strut to the forward spar in the inner wing and a cranked axle and drag strut from the lower fuselage.

Elam co-invented the Oleo Sponge, a polyurethane foam engineered to absorb oil from water. Researchers engineered the material to be oleophilic and hydrophobic using sequential infiltration synthesis (SIS), a patented-material synthesis method Elam co-invented that has been cited by multiple companies. SIS was used to coat the interior surfaces of the foam with a thin layer of metal oxide “primer” that acts as a glue for attaching a monolayer of oleophilic molecules. The result is a reusable sponge capable of adsorbing up to 90 times its weight in oil.

Curzerene is a volatile, aromatic terpenoid found in many herbs and spices, such as Curcuma zeodaria. It is bioactive isolate of Caribbean corals and is also found in myrrh. More specifically it has been found to make up a significant portion - 12.97% - of the smoke produced from burning Commiphora myrrha oleo gum resin. It is also a major component of myrrh oil, which has been shown in vitro to possess anti-inflammatory properties at sub-toxic by inhibiting the production of the inflammatory cytokine IL-6 by human gingival fibroblasts.

In November 1931, the first two employees were recruited. The company's first success involved Dowty's newly-invented internally sprung wheel; the first order for six of these wheels was placed by the Japanese Kawasaki Company, manufacturing was performed at the company's Lansdown Terrace premises. In 1934, Dowty achieved a major sale after approached aviation engineer Henry Folland of Gloster to demonstrate his own design for oleo struts; these were promptly ordered for the Gloster Gauntlet aircraft. This initial and sizable production order was rapidly followed by a similar order for the Gloster Gladiator.

The floats were long, with marked chine and two steps, the second close to the tip where there was also a water rudder. They used the same oleo legs as the landplane, augmented by a pair of forward-reaching struts to the fuselage behind the lower radiator, and another pair aft. The Pike first flew on 14 March 1927, with Frank Courtney at the controls and having made a few earlier hops at Parnall's Yate factory airfield. From there it went to the MAEE at Felixstowe for trials on water.

Two retractable main undercarriage legs were fitted with oleo- pneumatic shock-absorbers, medium pressure braked Dunlop wheels, as well as the non-retractable castoring Dowty tailwheel. Provision for fitting a retractable tailwheel undercarriage was also provided. Two engines were intended to be fitted to the welded steel tube engine nacelles but the prototype was fitted with two Walter Major 6 engines, with instruments fitted to the inner sides of the nacelles where they were clearly visible to the flight crew. Two fuel tanks of each were housed in the wings with oil tanks in the engine nacelles.

Externally, the An-124 is similar to the American Lockheed C-5 Galaxy, having a double fuselage to allow for a rear cargo door (on the lower fuselage) that can open in flight without affecting structural integrity. It is slightly shorter, with a slightly greater wingspan, and a 17% larger payload. Instead of the Galaxy's T-tail, the An-124 uses a conventional empennage, similar in design to that of the Boeing 747. The An-124's main engine is the Lotarev D-18 (238–250 kN). The aircraft uses oleo strut suspension for its 24 wheels.

The pilot's seat was positioned halfway between the wings and the tail surfaces: a passenger seat was fitted behind the engine. The main undercarriage employed oleo-pneumatic suspension, and there was a single steerable tailwheel. It was intended that lateral stability would be achieved by automatic differential movement of the two halves of the upper wing, this feature being the subject of a patent filed by Bréguet. In a turn, the greater speed of the outer wing would cause the angle of attack to be reduced, so eliminating the increase in lift that the greater speed would otherwise have produced.

The F.K.35 was powered by a 600 hp (444 kW) Bristol Pegasus VI nine cylinder radial engine driving a two blade propeller. Its fuel was held in lower wing tanks, which could be jettisoned in an emergency. Its fixed undercarriage was conventional, with a wide track. The mainwheels were mounted on bent axles hinged on the central fuselage bottom, forming a central transverse inverted V; the outer ends of the axles were supported by a vertical oleo strut and an oblique strut, together forming a V attached to the wing underside beneath the ends of the wing struts.

The Redoutable-class submarines were able to fully submerge in thirty seconds. Prométhée was still undergoing trials, and it was one of the boat's first voyages at sea. As the commander had not seen anyone at the command post, and the accident occurred when the order was given to start the diesel motors, the commission concluded on 13 July that an "unexpected, rapid and general opening of the purges" had flooded the ballast tanks with water, which rendered the submarine heavy and sank her. This unexpected opening could have been due to an error, or connectivity in the oleo-pneumatic section valve systems .

As exhibited in Paris, the P.10 had a tall single axle undercarriage mounted on a pair of vee- struts on either side. These were bungee sprung, though there were plans for oleo dampers. The P.10 was not the first metal British aircraft, for the unlikely looking Seddon Mayfly holds that priority; but it never had a realistic hope of flight. One lesser novelty, which was to become a standard Boulton & Paul feature was the mounting of the Lucifer on a hinge so that it could be swung sideways for servicing without disconnecting pipework etc.

Diorama of local Neolithic landscape, at the Museum. In the Neolithic, the inhabitants of the site had access to varied vegetation environments from the surrounding mountains, plain, and coast. Along the coastline the flora was mainly oleo-ceratonion shrubland, with shrubs like the European fan palm (Chamaerops humilis), lentisk (Pistacia lentiscus), heather (Erica sp.), olive tree (Olea europaea), juniper (Juniperus sp.) and Aleppo pine (Pinus halepensis). Elsewhere there were forests of sclerophyllous and deciduous oak trees (Quercus sp.), strawberry trees (Arbutus unedo), buckthorns (Rhamnus sp.) or mock privet (Phillyrea sp.), and adler (Alnus sp.), as attested by charcoal fragments found in the mines.

The YUH-61 was designed to meet the UTTAS requirements for improved reliability, survivability and lower life-cycle costs, resulting in features such as dual-engines with improved hot and high altitude performance, and a modular design (reduced maintenance footprint); run-dry gearboxes; ballistically tolerant, redundant subsystems (hydraulic, electrical and flight controls); crashworthy crew (armored) and troop seats; dual-stage oleo main landing gear; ballistically tolerant, crashworthy main structure; quieter, more robust main and tail rotor systems; and a ballistically tolerant, crashworthy fuel system.Leoni 2007, pp. 42–48. Transport aboard the C-130 limited the UTTAS cabin height and length.Leoni 2007, pp.

This arrangement did little for the car's road-holding, although few cars of the period handled particularly well. However the car used Lockheed oleo- pneumatic struts in place of the conventional coil spring and damper units, it being thought at the time that this aviation-derived system would become a common road car arrangement. Another significant departure from previous designs was the use of twin centrifugal rather than Roots-type superchargers, developed by Rolls-Royce based on the units used on later versions of the Merlin aero engine. This was to prove one of the car's main shortcomings.

The oleo-pneumatic undercarriage retracted inwards with the wheels housed in the lower fuselage faired into the lower engine cowling by small doors. The empennage is built up from wood and control surfaces are metal framed with fabric covering. In January 1939, the Armée de l'Air placed an order for 50 aircraft, to be powered by Gnome-Rhône 14N engines. Due to the unavailability of Gnome-Rhône engines and French instruments, just 17 aircraft – six F.K.58s and 11 F.K.58As – were completed at the Koolhoven works, with Dutch supplied engines and instruments – and delivered to the Armée de l'Air.

Unlike its siblings the Champ and Chief, both of which employ oleo struts for shock absorption, the Sedan makes used of bungee cords to absorb landing and taxi loads. The Sedan is powered by the Continental C-145-2 or Continental O-300-A engine of ; the Franklin 6A4-165-B3 and Franklin 6A4-150-B3, of 165 and , respectively, are also approved for installation. The Sedan features an electrical system, including a starter, as standard equipment. As it had with many of its other models, Aeronca certified a seaplane version of the Sedan, the model S15AC.

With the formation of Airship Industries production of the Skyship 500 could commence and five further airships were produced.\- The Skyship 500 consists of a polyester fabric envelope, retaining helium gas, and carrying a gondola for the control cabin, passenger cabin, propulsion systems and ballast (fixed and jettison-able). The envelope is of a traditional streamlined shape with cruciform tail surfaces which carry rudder and elevator control surfaces for yaw and pitch. The undercarriage consists of a castoring twin-wheeled oleo-pneumatic strut at the rear of the gondola, with ground handling ropes for ground crew to manoeuvre the airship on the ground.

On 17 July 1939, R2052, the first, unarmed, prototype, conducted its maiden flight, a little more than eight months after development had formally started. The rapid pace of development is partly due to the re-use of many elements of the Beaufort design along with frequently identical components. R2052 was initially operated by Bristol for testing purposes while it was based at Filton Aerodrome. Early modifications to R2052 included stiffening of the elevator control circuit, increased fin area and lengthening of the main oleo strut of the undercarriage to better accommodate weight increases and hard landings.

The anhedral of the wing's center- section also permitted the wing and fuselage to meet at the optimum angle for minimizing drag, without using wing root fairings. The bent wing, however, was heavier and more difficult to construct, offsetting these benefits. The Corsair's aerodynamics were an advance over those of contemporary naval fighters. The F4U was the first U.S. Navy aircraft to feature landing gear that retracted into a fully enclosed wheel well. The landing gear oleo struts—each with its own strut door enclosing it when retracted—rotated through 90° during retraction, with the wheel atop the lower end of the strut when retracted.

Any aircraft fuelled to fly the Atlantic was going to be heavy and undercarriage design was critical, as Martinsyde found to their cost. The Atlantic used a split axle arrangement: on each side the short main leg extended from below the forward and innermost interplane strut. There was a second member back to below the aft interplane strut and an axle from the large single wheel upwards and inwards, hinged to the lower fuselage longeron. Shocks were absorbed by a combination of oleo-pneumatic and bungee elastic components. At 21 ft 0 in (6.40 m) the track was very wide."The Boulton & Paul Commercial Machine", Flight 30 October 1919, vol.

Aircraft landing gear includes wheels equipped with solid shock absorbers on light planes, and air/oil oleo struts on larger aircraft. Skis are used for operating from snow and floats from water. (Helicopters use skids, pontoons or wheels depending on their size and role.) The landing gear represents 2.5 to 5% of the MTOW and 1.5 to 1.75% of the aircraft cost but 20% of the airframe direct maintenance cost. A suitably-designed wheel can support , tolerate a ground speed of 300 km/h and roll a distance of ; it has a 20,000 hours time between overhaul and a 60,000 hours or 20 years life time.

The LH.41 was a small low-wing, cantilever monoplane built largely of wood with fabric and plywood skinning. The LH.41 was supported on a wide-track strut mounted undercarriage, incorporating oleo-pneumatic shock-absorbers, with a tail-skid. For initial flight testing the LH.41 was fitted with a Lorraine 7Mb Mizar 7-cylinder radial engine with a distinctive oil cooler on the port side of the fuselage forward of the cockpit. After initial testing the LH.41, re-engined with the intended Lorraine 9Nb driving a Levasseur metal fixed pitch propeller fitted with a dorsal oil cooler in place of the side-mounted cooler.

Emak was incorporated in 1992 by the merger of Oleo-Mac and Efco, two companies specialised in the production of gardening and forestry machines, both of which had been active since the 1970s in the province of Reggio Emilia (Italy). The combination of the manufacturing and managerial resources of the two companies soon allowed the new industrial complex to achieve a competitive position on the international market. In 1996 Emak secured ISO 9001 certification and from June 1998 it has been listed on the Milan Stock Exchange, forming an international group thanks to the acquisition of 9 companies. In 2008, following the acquisition of Bertolini S.p.

The undercarriage was the main structure in this part of the aircraft. Each main unit comprised two oleo legs and a single wheel. It was retracted electrically via the crew in the cockpit. The adoption by the Luftwaffe midway through the war, of a general system of unitized powerplant installations for twin and multi-engined combat aircraft incorporating as many of the engine's auxiliary components (radiator and oil cooler, and all fluid and mechanical connections) into a single, easily interchangeable unitized "bolt-on" package, known as the Kraftei (power-egg) concept, was being widely adopted by the time of the Do 217's initial frontline appearance.

The radio operator and navigator sat behind, with the bomb aimer's position further aft. Long side windows stretched rearwards from the cockpit almost to the end of the cabin, which was about halfway between the trailing edge and the tail. The undercarriage was intended to be robust enough for rough field operation: long travel Messier oleo legs ran upwards in front of the lower leading edge to the start of the boom, forming a split axle undercarriage bearing large wheels with their centres (when parked) not far below the fuselage floor. A tailwheel was mounted under a fairing at the extreme rear of the cabin.

To spread the load across the elliptical planform high aspect ratio wings, the undercarriage was of four mainwheel oleo struts - one in each engine nacelle - with a single balloon-tyred wheel on each. The defensive guns were mounted in barbettes at the rear of each outboard nacelle, which were to be remotely operated by a gunner in a pressurised compartment in the extreme tail. The Windsor used Wallis's geodetic body and wing structure that Vickers had previously used in the Wellesley, Wellington and Warwick bombers. The wing structure had no spars but a hollow geodetic tube from tip to tip, passing through the fuselage truss.

To meet specification N.15/44 for a navalised Mosquito for Royal Navy use as a torpedo bomber, de Havilland produced a carrier-borne variant. A Mosquito FB.VI was modified as a prototype designated Sea Mosquito TR Mk 33 with folding wings, arrester hook, thimble nose radome, Merlin 25 engines with four-bladed propellers and a new oleo- pneumatic landing gear rather than the standard rubber-in-compression gear. Initial carrier tests of the Sea Mosquito were carried out by Eric "Winkle" Brown aboard HMS Indefatigable, the first landing-on taking place on 25 March 1944. An order for 100 TR.33s was placed although only 50 were built at Leavesden.

IMDb: George Coleman Coleman recorded into the 2000s. His CD as co-leader, Four Generations of Miles: A Live Tribute To Miles, with bassist Ron Carter, drummer Jimmy Cobb and guitarist Mike Stern was released on Chesky Records in October 2002, and it concentrates on the 1960s working repertoire of Miles Davis. Tracks include: "There Is No Greater Love", "All Blues", "On Green Dolphin Street", "Blue in Green", "81", "Freddie Freeloader", "My Funny Valentine", "If I Were a Bell", and "Oleo". He was featured on Joey DeFrancesco's 2006 release Organic Vibes, along with vibraphonist Bobby Hutcherson, Billboard's Top Jazz Album Chart, peaked to No. 17.

Sei Mangkei Special Economic Zone has an area of 2002.77 hectares, which is being built along with Port of Kuala Tanjung as part of strategy to turn North Sumatra as an international hub. SEZ Sei Mangkei consists of three zones, namely industrial zone, logistics zone and export processing zone. This KEK is adjacent to the village of Keramat Kubah in the north; with PTPN IV Kebun Mayan in the south; with PTPN IV Kebun Gunung Bayu in the east; and with the River Bah Bolon in the west. Until the end of 2017, SEZ Sei Mangkei absorbed Rp 10.5 trillion of investment, which includes an Oleo-chemical plant of Unilever Indonesia.

The Hamilcar was fitted with tailwheel landing gear, with oleo-pneumatic shock absorbers that could be deflated to bring the fuselage nose down for loading or unloading purposes.Lloyd 1982, p. 65. A jettisonable undercarriage was initially designed for the glider, as it was discovered that it travelled for a shorter distance when it landed only on its skids. However, this was eventually replaced with a fixed undercarriage – the same as had been designed for ferrying operations – as pilots found that they preferred to land on wheels because of the extra control it gave them and the ability to avoid other gliders and potential collisions in the landing area.

A breakthrough arrived in 1954 when he recorded his famous compositions "Oleo", "Airegin", and "Doxy" with a quintet led by Davis that also featured pianist Horace Silver, these recordings appearing on the album Bags' Groove. In 1955, Rollins entered the Federal Medical Center, Lexington, at the time the only assistance in the U.S. for drug addicts. While there, he volunteered for then- experimental methadone therapy and was able to break his heroin habit, after which he lived for a time in Chicago, briefly rooming with the trumpeter Booker Little. Rollins initially feared sobriety would impair his musicianship, but then went on to greater success.

The cockpit placement of the F.K.8 The type had several teething troubles: the oleo undercarriage was unable to withstand rough use on the front line airfields, tail skids frequently broke and the original radiators blocked up quickly. Following instructions issued on 30 April 1917, some F.K.8s were refitted with simplified vee-undercarriages from Bristol F.2 Fighters. This soon led to a temporary shortage of these undercarriages and the practice had to be discontinued until May 1918, after which several F.K.8s were fitted with revised undercarriages. Most production F.K.8s had modifications to the wings, gunner's seat and the exhaust system.

At the rear of the Possum the fabric-covered wooden empennage was conventional. The fin had a straight and vertical leading edge but a curved top that blended into a rounded rudder which extended downwards between separate elevators; the tailplane was mounted just above the fuselage. Underneath, unusually for the time, there was a tailwheel rather than a skid, which was steerable and fitted with an automatic brake which provided increasing resistance with increasing load, unless the pilot overrode it. The main undercarriage was less innovative, with a pair of wheels single axle- mounted on short oleo legs to the wings with rear bracing.

The next major effort was directed at Fort Hood which at the height of the Vietnam War housed more than 40,000 soldiers, 65% of whom had recently returned from thirteen-month stints in the war. As the army itself soon realized, these returnees with little time left in the military, were the soldiers most likely to become involved in political activity against the war. In June 1968, Gardner and other activists rented an old shop at 101 Avenue D in Killeen, TX where Fort Hood was located. When Gardner left town to help set up other coffeehouses, Josh Gould and Janet "Jay" Lockard stepped in to become the principle operators of the soon to open Oleo Strut.

The combination of an aft cockpit and the Corsair's long nose made landings hazardous for newly trained pilots. During landing approaches, it was found that oil from the opened hydraulically- powered cowl flaps could spatter onto the windscreen, severely reducing visibility, and the undercarriage oleo struts had bad rebound characteristics on landing, allowing the aircraft to bounce down the carrier deck. The first problem was solved by locking the top cowl flaps in front of the windscreen down permanently, then replacing them with a fixed panel. The undercarriage bounce took more time to solve, but eventually a "bleed valve" incorporated in the legs allowed the hydraulic pressure to be released gradually as the aircraft landed.

Its empennage was conventional with a large balanced rudder which reached down to the keel, hinged on a small fin. The in- flight adjustable, wire-braced, triangular tailplane was mounted on top of the fuselage frame, carrying balanced elevators. The MS.300 had fixed, conventional landing gear with its mainwheels independently mounted on V-struts hinged to the lower fuselage, with vertical Messier oleo strut shock absorbers. These were mounted on the forward wing strut at a point which was strengthened by two additional short struts to the fuselage. Little is recorded about the trials and careers of the MS.300 and 301 and the exact dates of first flights are not known.

Antonov An-124 Ruslan landing gear An oleo strut consists of an inner metal tube or piston, which is attached to the wheel axle, and which moves up and down in an outer (or upper) metal tube, or cylinder, that is attached to the airframe. The cavity within the strut and piston is filled with gas (usually nitrogen, sometimes air—especially on light aircraft) and oil (usually hydraulic fluid), and is divided into two chambers that communicate through a small orifice. When the aircraft is stationary on the ground, its weight is supported by the compressed gas in the cylinder. During landing, or when the aircraft taxis over bumps, the piston slides up and down.

The D.B. Martin Co.'s Flagship Facility in Philadelphia, PA (1908) In 1876, D.B. Martin founded the D.B. Martin Company in Delaware (USA), and later (1904) incorporated the company in Philadelphia (USA). A processor of animal- derived fats, oils, fatty acids, soaps, and fibers, the company experienced rapid growth in the United States and Canada, becoming the largest meat packing and processing operation east of Chicago.> Martin contracted architect C.B. Comstock to design a state of the art, all-in-one facility in Philadelphia at a cost of $1,000,000. Opened in 1908, the building incorporated an abattoir, corporate headquarters office space, rooftop stock pen, cold storage, and oleo processing operations, along with advanced environmental controls to protect city residents.

Keeping the prop clear of the deck required long landing gear, which, combined with the shortened fuselage, gave the Bearcat a significant "nose-up" profile on land. The hydraulically operated undercarriage used an articulated trunnion which extended the length of the oleo legs when lowered; as the undercarriage retracted the legs were shortened, enabling them to fit into a wheel well which was entirely in the wing. An additional benefit of the inward retracting units was a wide track, which helped counter propeller torque on takeoff and gave the F8F good ground and carrier deck handling.Scrivner 1990, p. 4. The design team had set the goal that the G-58 should weigh 8,750 lb/3,969 kg fully loaded.

The design was a development of the Siddeley-Deasy S.R.2 Siskin designed by Major F. M. Green (formerly chief engineer of the Royal Aircraft Factory) of the Siddeley-Deasy Motor Car Company, to meet the requirements of RAF Specification Type 1 for a single-seat fighter powered by the promising ABC Dragonfly radial engine.Mason 1992, p. 148. The SR.2 Siskin was a single-bay biplane of wood and fabric construction. Its wings were of unequal span and the aircraft was fitted with a distinctive fixed conventional landing gear with long oleo strut shock absorbers carrying the axle, which was connected by radius rods to a pair of V-struts situated behind the axle.

Production examples differed from the prototype in having a larger rudder, enlarged baggage compartment, revised undercarriage with oleo struts, and lighter wheel brakes, The passenger cabin was also revised, with additional sound-proofing and ventilation, and the addition of a lavatory. A revision of the general structure produced a weight saving of 125 kg (275 lb) and an increase in top speed from 292 km/h to 319 km/h (182 mph to 199 mph). However, only three aircraft were built here before the facility was needed to build the Polikarpov I-16 and KhAI-1 production was shifted to Zavod 43 in Kiev, where the rest of the aircraft were built.

The two-piece wings are set at 16° dihedral and are supported by a pair of v cabane struts and v-struts either side from approx half-span to the lower centre fuselage. Full span leading edge slats extend automatically and full span trailing edge flaps / drooping ailerons can be extended manually by the pilot. The fixed tailwheel undercarriage attaches to the fuselage with long struts and oleo pneumatic shock absorbers. It was a proof-of-concept design for a 'fool-proof' trainer intended for novice pilots with only one hour of ground instruction, the hour being reduced to five-minutes for those who had already flown gliders, and was intended to be impossible to either stall or spin.

Romania could cash in four billion dollars from the Constanta-Trieste pipeline.Romania could cash in four billion dollars from the Constanta-Trieste pipeline. Pumping oil could pay off in Romania as benefits from the Constanta-Trieste pipeline could amount to more than four billion dollars. The benefits could range from 2.27 to 4.39 billion dollars over 20 years, depending on the capacity of the new oleo duct, according to Hill International's feasibility study. Romania has considerable natural resources for a country of its size, including coal, iron ore, copper, chromium, uranium, antimony, mercury, gold, barite, borate, celestine (strontium), emery, feldspar, limestone, magnesite, marble, perlite, pumice, pyrites (sulfur), clay, arable land and hydropower.

In 1934, Dowty achieved its breakthrough sale of its innovative undercarriage designs, being contracted by the Gloster Aircraft Company to provide oleo struts for the Gloster Gauntlet biplane. In 1935, as the business expanded to meet demand, Dowty founded a new manufacturing venture to produce his aviation products, which was named Dowty Aviation. It would quickly secure numerous additional orders and manufacturing facilities to cope with the pressing demands of the Second World War, a significant majority of British aircraft production incorporating the firm's various products. By the end of the conflict, Dowty Aviation was a major British manufacturing interest, possessing many production plants at home and overseas in Canada and the United States.

In this way, some writers while describing the area surrounding the port of Sanitja, have pointed out the existence of pottery fragments and other objects scattered on the surface, as well as some structures belonging to old buildings.Authors such as J.Ramis Ramis (1785); F. Oleo y Quadrado and Luis Salvados during the 19th century, supported the idea that Sanisera could have been related to the ruins at Sanitja. Furthermore, there are legends derived from local folklore about the place, such as the legend of "Ses Vilotes" gathered by F.Camps i Mercadal,“ A sa part ponent des port de Sa Nitja, hi ha mostres- sa principal és el cementiri o carnatge d´haver- hi existiti una població. Es nom des rodol en fa esment: es diu Ses Vilotes.

The aircraft was built in Convair's San Diego facility at Lindbergh Field and was taken to San Diego Bay for testing in December 1952. On 14 January 1953, with E. D. "Sam" Shannon at the controls, the aircraft inadvertently made its first short flight during what was supposed to be a fast taxi run; its official maiden flight was on 9 April. An XF2Y-1 in flight The underpowered engines made the fighter sluggish, and the hydro-skis were not as successful as hoped; they created violent vibration during takeoff and landing, despite the shock-absorbing oleo legs they were extended on. Work on the skis and legs improved this situation somewhat, but they were unable to resolve the sluggish performance.

"Jealous Heart" has become a standard of Latin music via a Spanish language rendering by Mexican lyricist Mario Molina Montes entitled "Celoso" ("jealous"). Recorded in Nashville in March 1966 by Trio Los Panchos led by Johnny Albino, "Celoso" entered the Top Ten in Mexico in April 1967 and - ranked in tandem with a cover by Marco Antonio Muñiz - the track reached No. 1 that summer spending five months in the Top Ten. In addition the Trio Los Panchos version reached No. 2 - in a tandem ranking with covers by José Feliciano and Oleo Guillot - in Argentina that autumn when the Muñiz version reached No. 1 in Puerto Rico. "Celoso" has also been recorded by Galy Galeano, Ezequiel Peña, José Luis Rodríguez and Sergio Vega.

Undaunted by the lack of interest the Regia Aeronautica (Italian Royal Air Force) had displayed in the Caproni Ca.70 night fighter after official tests in 1926, the Caproni company designed a derivative. It was initially designated the Ca.70L and then redesignated the Ca.71. Like the Ca.70, the Ca.71 was designed to ensure good low-speed handling and good visibility from both cockpits, without any of the aircrafts structural elements obstructing the view of either crewman. Its two wings were of unequal span, and it had tailskid landing gear, an unusual feature of which was an oleo-pneumatic shock absorber on the main landing gear which allowed the wheels to travel forward in their linkage while the plane was taxiing.

The Caproni company designed the Ca.70 to ensure good low-speed handling and good visibility from both cockpits, without any of the aircrafts structural elements obstructing the view of either crewman. Its two wings were of unequal span, and it had tailskid landing gear, an unusual feature of which was an oleo-pneumatic shock absorber on the main landing gear which allowed the wheels to travel forward in their linkage while the plane was taxiing. The 9-cylinder, 313-kilowatt (420-horsepower) Bristol Jupiter radial engine gave the Ca.70 a top speed of per hour. Armament consisted of two fixed forward-firing 7.7-millimeter Vickers machine guns and a flexible 7.7-millimeter Lewis machine gun on a Scarff ring in the rear cockpit.

Following on from the earlier Lorraine Hanriot LH.42 racing aircraft, Monsieur Louis Montlaur, at the behest of Lorraine Hanriot's parent organisation, the Société Générale Aéronautique (SGA), designed an aircraft with metal structure and skinning of similar layout to the LH.42. The mid-set monoplane wings had a single metal spar supporting wooden ribs which were fabric covered aft of the metal-skinned leading edge. The fuselage was a built up Duralumin structure with sheet metal skinning The undercarriage consisted of strut mounted wide-track main gear with faired wheels, Hanriot Spécial oleo-pneumatic shock-absorbers and a steel tail skid. Power for the HL.130 was supplied by a single Lorraine 9Nb 9-cylinder radial engine (serial no.

Plant resins are valued for the production of varnishes, adhesives, and food glazing agents. They are also prized as raw materials for the synthesis of other organic compounds and provide constituents of incense and perfume. The oldest known use of plant resin comes from the late Middle Stone Age in Southern Africa where it was used as an adhesive for hafting stone tools. Lumps of dried frankincense resin Protium Sp. - MHNT The hard transparent resins, such as the copals, dammars, mastic, and sandarac, are principally used for varnishes and adhesives, while the softer odoriferous oleo-resins (frankincense, elemi, turpentine, copaiba), and gum resins containing essential oils (ammoniacum, asafoetida, gamboge, myrrh, and scammony) are more used for therapeutic purposes, food and incense.

Though the A-10 had been designed from the start to be convertible into an ambulance aircraft and to accept Salmson engines of similar power to the Hispano, the A.XI or A-11S (S for sanitaire or ambulance) was not reported until 1932, fitted with a closely cowled Salmson radial. It also had a different undercarriage to that of the first A-10, retaining the cranked axles but adding drag struts to the fuselage centre-line and inward- sloping oleo struts to the lower longerons. In April 1932 it was undergoing official tests at Villacoublay which continued at least into June. In October it was one of five prototypes that took part in the Tour de Propagande (Publicity Tour), flying around northern France in eight daily stages.

A two-disc CD version of the complete concert was released by Sony/Columbia in 1998. This album has the first half of the concert on CD 1 and the second half on CD 2. This is the only CD edition of the album to feature the original mono mix. Track listing: CD 1 #"So What" (Miles Davis) - 12:01 #"Spring Is Here" (Lorenz Hart, Richard Rodgers) - 4:03 #"Teo" (Davis) - 9:10 #"Walkin'" (Richard Carpenter) - 9:32 #"The Meaning of the Blues" / "Lament" (Troup, Worth/J.J. Johnson) - 4:34 #"New Rhumba" (Ahmad Jamal) - 4:07 Track listing: CD 2 #"Someday My Prince Will Come" (Frank Churchill, Larry Morey) - 2:55 #"Oleo" (Sonny Rollins) - 7:19 #"No Blues" (Davis) - 10:38 #"I Thought About You" (J.

1971 Armed Farces Day antiwar demonstration at Fort Hood army base Fonda's May 11, 1970 visit gave an unexpected boost to the Fort Hood soldiers and their civilian supporters who were building for nationally coordinated antiwar demonstrations near military bases on May 16, Armed Forces Day. While Killeen's business community traditionally held patriotic and pro-military events in the town, antiwar activists felt it was important to express resistance in the wake of the recent escalated bombings in Cambodia and the shooting of protesting students at Kent State and Jackson State. Called Armed Farces Day, the antiwar activity "ended up being a much larger event than its organizers anticipated." "Several hundred GIs, many in uniform, assembled at the Oleo Strut" before marching to a nearby park where they were joined by hundreds of others.

Zlokazov formed a small design bureau, at the GVF repair plant at Irkutsk, to create a transport aircraft for use in the Arctic regions. The aircraft was based on the PS-4, which was a Soviet built Junkers W33, with an enclosed, heated, cockpit and cabin for ten passengers or 880 kg of cargo loaded through a double set of doors on the port fuselage side. The undercarriage introduced oleo-pneumatic shock absorbers with large low-pressure tyres which could be exchanged for skis when necessary, and a good field performance was ensured through use of powered landing flaps. The ARK-Z-1 satisfactorily completed the factory flight test programme and the aircraft was then flown to Moscow for testing by the NII GVF during the Autumn of 1935.

On the C3-225, an additional removable fuel tank was added in the fuselage, and the wing tank acted as a header tank. The prototype had a conventional undercarriage similar to those used on most World War One aircraft, with a pair of vees braced from the lower longerons, connected with a spreader bar and suspension provided by bungee cords. This was replaced with a split axle undercarriage on the C3-1 and C3-2, which had the legs braced to the opposite lower longerons. From the C3-3 onwards, each undercarriage leg was triangulated with two struts braced to a central keel in the bottom of the fuselage, and one oleo strut on each side to the upper longeron, providing a greater range of movement and reducing camber changes.

Further changes were the use of large round Oleo buffers with a pneumatic withdrawal mechanism rather than the traditional coach style (oval) saddle buffer which relied on a pin and spring mechanism. As the JA examples came in for overhaul over the years, the saddle buffers were also replaced making visual identification of the differing machines almost impossible from a distance. From new, all members of the class were fitted with the Pullman style rubbing plate between the buffers allowing them to close couple with Southern Region electro-pneumatically controlled electric multiple units and diesel electric multiple units for push-pull train operation – the reason for retractable buffers. Being built to the Hastings Line gauge, the locomotives were able to be used on all routes of BR's Southern Region network.

The lift engines were mounted vertically in side-by-side pairs in a central bay so that their resultant thrust line passed close to the centre of gravity of the aircraft. These pairs of engines could be swivelled fore-and- aft to produce vectored thrust for acceleration/deceleration along the aircraft's longitudinal axis. SBAC show in 1961, showing the oleo leg fairings and the lift engine automatic inlet louvres added in mid-1960 During conventional flight, the lift engines would be shut down; before beginning the transition from horizontal to vertical flight, they would be started using compressed air from the single cruise engine. The compressed air provided the initial rotation of the engine but a pressure drop from intake to exhaust had to be present also as the compressed air alone was not adequate for reaching idle speed.

Ju 288 V1 first prototype, showing its complex "folding" main undercarriage. The limited space available to stow landing gear has led to many complex retraction mechanisms, each unique to a particular aircraft. An early example, the German Bomber B combat aircraft design competition winner, the Junkers Ju 288, had a complex "folding" main landing gear unlike any other aircraft designed by either Axis or Allied sides in the war: its single oleo strut was only attached to the lower end of its Y-form main retraction struts, handling the twinned main gear wheels, and folding by swiveling downwards and aftwards during retraction to "fold" the maingear's length to shorten it for stowage in the engine nacelle it was mounted in. However, the single pivot-point design also led to numerous incidents of collapsed maingear units for its prototype airframes.

The Philippine coconut industry was responsible for 26% of the volume of the agricultural sector and was reportedly present in 68 of the 81 provinces of the country. Next to sugar, coconut products was also the leading agricultural export of the Philippines, with 37 products and by-products that were exported to 114 countries. The major exports were crude and refined oil, copra meal, desiccated coconut, activated carbon, and oleo-chemicals. About one-third of the Philippine population depended mainly on coconut production for its livelihood. The legal beginnings of the levy can be found in Republic Act 1145 enacted on June 17, 1954 under President Ramon Magsaysay which calls for the creation of the Coconut Development Fund. Subsequent amendments were made with the enactment of Republic Act 6260 on 19 June 1971 under President Ferdinand Marcos.

A description on how the Ferula galbaniflua oleo-gum resin is collected is brought down in Howes F.N. (1950), p. 314. The problem arising from this identification, however, is that Maimonides writes that it is "a tree endemic to the Grecian cities,"Maimonides (1974), Hil. Kelei Hamikdash 2:4, who writes explicitly that the galbanum is “like black syrup whose smell is strong, being an oleoresin derived of trees in the Grecian cities.” whereas Ferula is only an herbaceous plant. The name maiʻah, however, has yet another meaning. Ibn Rushd, also known as Averroës (1126-1198), says of this resin: “Maiʻah, it is the peel of a tree that resembles the apple [tree] and it has a white fruit... now, it is the dried and liquid galbanum which is pressed from the heart of its heartwood and is called lebni...”Amar, Z. (2002), p. 85.

Standardized on the A-3's longer rear fuselage, strengthened wing, shortened undercarriage oleo legs, ETC 2000/XII wing racks and an increase in maximum external load. ;;He 177 A-5/R1 :Version optimized for Fritz X and Hs 293 guided bombs, equipped with Kehl control gear. ;;He 177 A-5/R2 :Armed with a single MG 81 in the nose, a single MG 151 cannon in the forward end of the Bola ventral gondola, an MG 131 in the rear end of the ventral gondola, a pair of MG 131 in an FDL 131Z remotely controlled forward dorsal turret, a single MG 131 in a manned aft dorsal turret, and a single tail-mounted MG 151 cannon. ;;He 177 A-5/R4 :Simplified bomb rack installation, equipped with Kehl control gear. ;;He 177 A-5/R5 :Tested with a supplementary pair of MG 131 in an FDL 131Z aft ventral remote turret aft of the rear bomb-bay, only one built.

This pioneer of Spanish industrial design has a long professional career. Among other works, he was the person responsible for the design in automotion for Coast Workshops 1957–1958, he planned the remodeling of the Rock jewelry of J.M. Sert 1969, he was made charge of the new outer and inner design of the Banco Bilbao de la Via Laietana of Barcelona, it carried out a centerpiece for Barcelona'92, it created two candelabras for Nanimarquina in 1993, oil/vinegar recipients for Hojiblanca Oleo Cristal (2003) and two standard lamps for Iluminil Sa. The works of this author, I Reward National of Design, they speak about its capacity to work in areas of its professional disciplines.Noticias El MundoEl Mundo In his professional facet he has combined with collaborations as a columnist in Saw of Gold, M+D, Hogares Modernos, Cuadernos de Arquitectura, and Bonart. Also, he has worked its facet as a sculptor and has participated in different exhibitions.

The twin-wheeled nose and main gears had levered suspension and different tracks to improve rough-field performance. The kneeling undercarriage was initiated at the start of the takeoff run and gradually bled oil out of the Oleo-pneumatic strut until the required incidence of three degrees was reached just before liftoff. After takeoff the undercarriage was selected to retract which reversed the oil flow as the undercarriage retracted. All undercarriages were enclosed with fairings and doors when retracted. The bicycle undercarriage arrangement was tested on the Alekseyev I-215D. The seven-stage axial compressor Lyul'ka TR-3A (later AL-5) turbojet engines, with variable exhaust nozzles and petrol engine starters, were housed in the streamlined nacelles attached to pylons at 26% span. To boost takeoff performance, four '126-1' JATO rockets of 2,000 kg (4,410 lb)for 17s could be attached to the rear fuselage ('129-1' JATO bottles were used on the prototype). The control system of the '150' was revolutionary for its time, with irreversible, electrically signalled and electrically driven screwjacks operating the control surfaces.

Iskandar Malaysia (IM; Jawi: إسکندر مليسيا), formerly known as Iskandar Development Region (IDR; ; Jawi: ولايه ڤمباڠونن إسکندر) and South Johor Economic Region (SJER), is the main southern development corridor in Johor, Malaysia. It was established on 8 November 2006.New township planned for Malaysia's Iskandar economic zone, Richard High, 4 July 2008, KHL Group Iskandar Malaysia has been rapidly growing since its inception in 2006. Strategically located at the southernmost tip of mainland Asia and more than 3 times the size of neighbouring Singapore, it sits on the world’s busiest shipping routes and is within a 6-hour reach of major Asian cities through the Senai International Airport. Iskandar Malaysia’s development is guided by the Comprehensive Development Plan (CDP) and the Circle of Sustainability, ensuring that the region grows holistically into a prosperous economy with a high-quality living ecosystem and a resilient environment. Iskandar Malaysia’s generous land area, strategic location and abundant ready infrastructure boosted its 9 promoted sectors which are Electrical & Electronics, Petrochemical and Oleo-Chemical, Food & Agro-Processing, Logistics, Tourism, Creative, Healthcare and Financial.

Jorge Carrillo Oleo was exonerated by Judge María del Rosario Rojas Lara on February 16, 2003. He became a writer for La Jornada newspaper and Proceso magazine, both in Mexico City, specializing in security affairs. In 2011, Carrillo Olea wrote México en Riesgo, Una visión personal sobre un Estado a la defensiva (Mexico at Risk, A Personal View of a State on the Defense), which is a reflection on the Mexican security apparatus during the presidencies of Luis Echeverría, José López Portillo, Miguel de la Madrid and Carlos Salinas de Gortari; as well events such as the Tlatelolco massacre of October 2, 1968, the 1973 Chilean coup d'état, the 1985 Mexico City earthquake, the collapse of the computer system during the 1988 Mexican election, and his own governorship of Morelos. In 2018, Carrillo Olea wrote Torpezas de la inteligencia: Las grandes fallas dela seguridad nacional y sus posibles soluciones (Clumsiness of intelligence: The great failures of national security and its possible solutions), which is a description of his observation of how Mexican presidents have fused strategic intelligence and government.

The most noticeable feature of the Ar 232 was the landing gear. Normal operations from prepared runways used a tricycle gear — a then-novel feature for German military aircraft—but the sideways-retracting main gear's lever-action lower oleo-strut suspended arm – carrying the main gear's wheel/tire unit at the bottoms of the maingears' struts could "break", or kneel, after landing to place the fuselage closer to the ground and thereby reduce the ramp angle. An additional set of eleven smaller, non-retractable twinned wheels per side, mounted along the ventral centreline of the fuselage from just behind the semi-retractable nosewheel aftwards to just forward of the wing's trailing edge, supported the aircraft once the main landing gear's lever-action lower arm had "knelt", or could be used for additional support when landing on soft or rough airfields. The aircraft was intended to be capable of taxiing at low speeds on its row of small wheels, thus being able to negotiate small obstacles such as ditches up to 1.5 m (5 ft) in width.

The F/A-18L version followed to coincide with the US Navy's F/A-18A as a land-based export alternative. This was essentially an F/A-18A lightened by about ; weight was reduced by removing the folding wing and associated actuators, implementing a simpler landing gear (single wheel nose gear and cantilever oleo main gear), and changing to a land-based tail hook. The revised F/A-18L included wing fuel tanks and fuselage stations of the F/A-18A. Its weapons capacity would increase from , largely due to the addition of a third underwing pylon and strengthened wingtips (11 stations in total vs 9 stations of the F/A-18A). Compared to the F-18L, the outboard weapons pylons are closer to the wingtip missile rails. Because of the strengthened nonfolding wing, the wingtip missile rails were designed to carry either the AIM-7 Sparrow or Skyflash medium-range air-to-air missiles, in addition to the AIM-9 Sidewinder as found on the F/A-18A. The F/A-18L was strengthened for a 9 g design load factor compared to the F/A-18A's 7.5 g factor.Northrop F/A-18L design brochure 1978.

DFS 230-A at Luftwaffenmuseum der Bundeswehr ;DFS 230 A-1 :Initial production version ;DFS 230 A-2 :A-1 with dual-controls ;DFS 230 B-1 :Braking parachute added, able to carry defensive armament (MG 34 machine gun) ;DFS 230 B-2 :B-1 with dual-controls ;DFS 230 C-1 :Late production version; B-1 with nose braking rockets ;DFS 230 D-1 :C-1 with improved nose braking rocket design, one prototype (DFS 230 V6) ;DFS 230 F-1 :Larger version with capacity for 15 soldiers, one prototype (DFS 230 V7, DV+AV) ;DFS 203: Two DFS 230 fuselages joined by an enlarged cantilever centre section, with span of and length of due to the rear fuselage being extended. Wind tunnel testing revealed little or no advantage over the standard DFS 230 so further work was abandoned. ;Focke-Achgelis Fa 225:A single DFS 230 converted to an auto-gyro by replacing the wings with the 3-bladed rotor from a Focke-Achgelis Fa 223, mounted on a pylon above the fuselage. The undercarriage was revised to include long oleo shock absorbers with a wide track for stability.

In the late 1960s, the United States Army began forming requirements for a helicopter to replace the UH-1 Iroquois, and designated the program as the Utility Tactical Transport Aircraft System (UTTAS). The Army also initiated the development of a new, common turbine engine for its helicopters that would become the General Electric T700. Based on experience in Vietnam, the Army required significant performance, survivability and reliability improvements from both UTTAS and the new powerplant.Leoni 2007, pp. 8–10. The Army released its UTTAS request for proposals (RFP) in January 1972.Leoni 2007, pp. 11, 39. The RFP also included air transport requirements. Transport within the C-130 limited the UTTAS cabin height and length.Leoni 2007, pp. 39, 42–43. The UTTAS requirements for improved reliability, survivability and lower life-cycle costs resulted in features such as dual-engines with improved hot and high altitude performance, and a modular design (reduced maintenance footprint); run-dry gearboxes; ballistically tolerant, redundant subsystems (hydraulic, electrical and flight controls); crashworthy crew (armored) and troop seats; dual-stage oleo main landing gear; ballistically tolerant, crashworthy main structure; quieter, more robust main and tail rotor systems; and a ballistically tolerant, crashworthy fuel system.

By May 1942, in desperation, it was suggested that the Daimler-Benz DB 606 be used instead, even though it was considerably larger and heavier (1.5 tonnes) and was well known to have serious problems. Prototypes of both designs with these engines were ordered, although the Fw 191 was just getting into the air with the BMW 801 radials at this point and the Ju 288 was showing a continual tendency to break its main landing gear on touchdown, partly due to its undercarriage problems caused by its complex method of stowing the oleo struts during retraction. The RLM had no designs to fill the gap left if Bomber B did not work, even though some minor designs like the Henschel Hs 130, usually powered with two DB 603 or 605 engines and the Dornier Do 317, being tried with the same, trouble-prone DB 606 or 610 "welded-together engines" on some of its prototype airframes were also being considered. A slightly improved Ju 88, based on the prototype Ju 88B design, was ordered as the Ju 188 and several prototypes of stretched versions of existing bomber designs with four engines were also ordered, as with Junkers' Ju 488 in 1943–44.