Improved aircraft suspension system with mechanism operable to e

Details Improved aircraft suspension system with mechanism operable to e Improved aircraft suspension system with mechanism operable to e

1976-12-03

1979-03-06

Kelmachter, Barry L.

Aeronautics and astronautics

Aircraft, heavier-than-air

Helicopter or auto-rotating wing sustained, i.e., gyroplanes

244104R, B64C 2560

Patent

active

041426983

ABSTRACT:
A passive aircraft landing gear system in which the spring rate and damping for aircraft rolling motions about a longitudinal axis are independent of the spring rate and damping for aircraft vertical motions, thereby permitting the landing gear system to optimally accomplish both landing impact attenuation and ground resonance instability abatement.

REFERENCES:
patent: 2139192 (1938-12-01), Krekel
patent: 2326210 (1943-08-01), Falk et al.
patent: 2774553 (1956-12-01), Jensen
patent: 2933271 (1960-04-01), Maltby
patent: 3042345 (1962-07-01), Holland
patent: 3173632 (1965-03-01), Woods

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