Double cam mounting assembly for mounting an aircraft wing to a

Details Double cam mounting assembly for mounting an aircraft wing to a Double cam mounting assembly for mounting an aircraft wing to a

1981-11-25

1984-04-24

Barefoot, Galen L.

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

403DIG7, 403408, 403365, 411273, 244131, B64C 338, B64C 126, F16D 112

Patent

active

044443650

ABSTRACT:
Bracket members secured respectively to the end of the wing at a forward or aft location, and to the aircraft fuselage form with a clevis pin a clevis connection with the clevis pin projecting through the bracket members. The pin bears integrally a first cam fitted within a circular opening of one bracket member. A pair of cam bushings rotatably mounted on the clevis pin to the side of the first cam are positioned within circular openings of dual ribs of the other bracket member forming the clevis connection. The cam bushings and the clevis pin are independently rotated to vary the angle of attack of the wing mounted to the fuselage and are locked at adjusted positions.

REFERENCES:
patent: 1769005 (1930-07-01), Van Dusen
patent: 1949787 (1934-03-01), Dugan

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