Method and apparatus for rolling control of airplanes by means o

Aeronautics and astronautics – Aircraft control – Rudders and empennage

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244213, B64C 932, B64C 1332

Patent

active

042707129

ABSTRACT:
This invention relates to a method for rolling control of an airplane by means of spoilers mounted at lift surfaces, which comprises subdividing the entire control range into a plurality of firmly graduated and successively adjustable control steps, and adjusting the individual control steps by means of a series of different partial spoiler surfaces actuatable in dependence upon each other either individually or in combination. The invention also relates to an apparatus for performing the method.

REFERENCES:
patent: 2070006 (1937-02-01), Eaton et al.
patent: 2635837 (1953-04-01), Grant
patent: 2925232 (1960-02-01), Murray et al.
patent: 3628756 (1971-12-01), Johnson

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