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The two forward sections were semi-monocoque (i.e. open channels) with braced longitudinal upper members which, bolted together, held the engine, a water-cooled inline upright 140 hp (100 kW) Hispano-Suiza) and the pilot's cockpit. Aft, two more sections, both true monocoques, held the observer and carried the tail unit.
The word monocoque is a French term for "single shell". [1] First used for boats, [2] a true monocoque carries both tensile and compressive forces within the skin and can be recognised by the absence of a load-carrying internal frame. Few metal aircraft other than those with milled skins can strictly be regarded as pure monocoques, as they use ...
Modern airframe history began in the United States during the Wright Flyer's maiden flight, showing the potential of fixed-wing designs in aircraft. In 1912 the Deperdussin Monocoque pioneered the light, strong and streamlined monocoque fuselage formed of thin plywood layers over a circular frame, achieving 210 km/h (130 mph). [3] [4]
The greatest novelty of the P.10 was that this part of the fuselage was not only a monocoque structure (still fairly unusual at the time), but a monocoque of steel with a load-bearing plastic skin riveted between the formers and stringers. [2] Specifically, the plastic was Bakelite-Dilecto, a hard, synthetic cellulose-formaldehyde product. [1]
National origin: France Manufacturer ... The S.36 was a biplane with a monocoque fuselage of wood and canvas construction. Only one airframe was built, and flight ...
The Vought XO4U-1, BuNo A-8641, [3] [4] was built in 1931, and was Vought's first airplane with a deep monocoque two-place fuselage, [5] and had a metal and fabric-covered metal wing structure. [6] Both sets of wings joined the fuselage ahead of the pair of cockpits with the pilot seated in a cut out on the trailing edge of the shoulder-mounted ...
The airframe was of all-metal semi-monocoque construction with flush-riveted stressed duralumin skinning and highly stressed parts made from high-strength steel. The cantilever shoulder-mounted wings were trapezoidal in plan-form with rounded wing-tips.
The UTVA 75 features a fully metallic, semi-monocoque airframe, which provides structural strength and durability. The aircraft is powered by a Lycoming O-360 engine, capable of delivering 210 horsepower. This engine configuration allows the aircraft to achieve a maximum speed of 209 km/h (113 knots) and a service ceiling of 4,178 meters ...