Drive for leading edge flaps of aircraft wings

Details Drive for leading edge flaps of aircraft wings Drive for leading edge flaps of aircraft wings

1980-04-17

1984-03-20

Blix, Trygve M.

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

244210, B64C 350

Patent

active

044376316

ABSTRACT:
A leading edge slat of an aircraft wing is connected to the ends of two rods each of them being linked to a crank arm which, in turn, is swung over a particular angular range by means of a planetary gear being driven by a common shaft. Arcuate guide rails on the slat run in rolls which are journalled on the wing case.

REFERENCES:
patent: 1472199 (1923-10-01), Thomson
patent: 2191839 (1937-12-01), Zap
patent: 2222935 (1940-11-01), Chilton
patent: 2381681 (1945-08-01), Maxwell
patent: 2383102 (1945-08-01), Zap
patent: 2702676 (1955-02-01), Delaney
patent: 2740597 (1956-04-01), Wittman
patent: 3263946 (1966-08-01), Roberts et al.
patent: 3640150 (1972-02-01), Leiner et al.
patent: 3831886 (1974-08-01), Burdges et al.
patent: 4159089 (1979-06-01), Cole

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