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Aerol Oleo-Pneumatic strut. During 1926, the Cleveland Pneumatic Tool Company designed and introduced an oleo strut, one of the first to be purpose-designed for use on airplanes. The company subsequently marketed the product as an Aerol strut, which had entered widespread use within the United States within the space of a decade.
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, [2] for each pair of twinned wheels mounted through a forward-projecting lever-action arm, to the lower end of the uniquely attached main ...
The principles illustrated by the successful use of hydropneumatic suspension are now used in a broad range of applications, such as aircraft oleo struts and gas filled automobile shock absorbers, first patented in the U.S. in 1934 [31] by Cleveland Pneumatic Tool Co. Similar systems are also widely used on modern tanks and other large military ...
Design and development [ edit ] Based on the Maule M-4 , it is a high-wing, strut-braced monoplane of conventional configuration, available with tailwheel or optional tricycle wheeled undercarriage [ 1 ] and frequently used as a floatplane with twin floats.
Its landing gear was fixed and conventional with wheels on a central fuselage-mounted split axle, their ends each supported by an oleo strut and a rearward drag strut. Its tailwheel was also on an oleo strut. The floatplane gear had a large, V-bottomed, single step float on vertical struts from the lower longerons, stabilized by a pair of small ...
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. [3]
The later D.K.D.5 was a fully aerobatic and final development of the D.K.D.4 design. It was powered by a 63 kW (85 hp) Cirrus III four cylinder upright air-cooled inline engine mounted exposed. An aerodynamic clean-up included a divided undercarriage with cranked axles and a long oleo strut from the outer axle to the upper longeron on each side ...
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. [1]