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Expired
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GB14210/47A
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B64C3/38—Adjustment of complete wings or parts thereof
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Engineering & Computer Science
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Mechanical Engineering
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Aviation & Aerospace Engineering
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Other Liquid Machine Or Engine Such As Wave Power Use
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Abstract
623,885. Aircraft wings. MAKHONINE, J. May 28, 1947, No. 14210. Convention date, July 2, 1946. Drawings to Specification. [Class 4] The deflection of aircraft wings is reduced in flight by mounting inside or outside each wing masses capable of spanwise movement located adjacent to the wing tips during flight and adjacent to the undercarriage during landing and take-off. In one embodiment, fuel tanks may be located in the aforementioned positions on each wing, the fuel being pumped from one tank to the other to achieve a spanwise movement of mass. In a second embodiment solid weights are movable along each wing from an outboard to an inboard position.
GB14210/47A1946-07-021947-05-28Improvements in aircraft wings
ExpiredGB623885A
(en)
Flight measurements of buffet characteristics of the F-104 airplane for selected wing-flap deflections(Flight tests to determine effects of moderate deflections of wing leading and trailing edges of F-104 aircraft buffet characteristics at subsonic and transonic speeds)
Influence of ground proximity on aerodynamic forces on an oscillating tilted airfoil(Effect of wing wake deflection due to ground proximity on flutter associated with takeoff and landing of vtol and stol tilted wing aircraft)
DO 31 experimental program: Results and conclusions obtained and future outlook(Design, development, and characteristics of Do-31 V/STOL aircraft to include solution of operational problems caused by ground effect and transition flight)
Rotocraft: A crashproof STOL aircraft(Crashproof rotorcraft STOL aircraft for rescue operation, discussing orthodox rigid and special rotary wings design, air tunnel experiment and flight tests)