Vibration-insulating stability improving torque force device

Details Vibration-insulating stability improving torque force device Vibration-insulating stability improving torque force device

1981-10-21

1984-01-31

Blix, Trygve M.

Aeronautics and astronautics

Aircraft control

Stabilizing weights

244 75A, 244220, 244 80, 267 571A, B64C 1704

Patent

active

044285507

ABSTRACT:
A conventional aircraft having horizontal stabilizers and hinged elevators, which is controlled, preferably, through push-pull rods, is provided with a dynamic torque (bob) weight connected to a rotating member, in the direct line of control to the elevator surfaces. The torque member is located in the nose portion of the aircraft with its center of gravity angled up from 20.degree. to 50.degree. when the elevator surfaces are in the neutral position. The torque member is also mounted in a flexible manner to isolate it from horizontal tail vibrations, or flutter.

REFERENCES:
patent: 2797882 (1957-07-01), Servanty
patent: 2941792 (1960-06-01), Stutz
patent: 3006627 (1961-10-01), Paulsen

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