Spoiler control system

Details Spoiler control system Spoiler control system

1976-02-05

1977-08-02

Blix, Trygve M.

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

244 83G, 244 90A, B64C 904, B64C 1332

Patent

active

040391620

ABSTRACT:
Control system for aircraft wing spoilers in which the amount of centering moment provided by the downwardly moving or aerodynamically inactive spoiler is increased as the aircraft flaps are extended, the control system including a differential linkage mechanism interconnecting the flaps and the spoiler actuating mechanism. In effect different schedules of spoiler motion in response to cockpit control inputs are generated with wing flaps in different positions.

REFERENCES:
patent: 2494208 (1950-01-01), Schultz

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