Aircraft landing gear, in particular for helicopters

Details Aircraft landing gear, in particular for helicopters Aircraft landing gear, in particular for helicopters

1984-10-29

1986-12-23

Blix, Trygve M.

Aeronautics and astronautics

Landing gear

Wheel

244104R, 244102SS, 244102A, 244100R, 188297, B64C 2560

Patent

active

046307885

ABSTRACT:
The landing gear comprises: a rod including nested first and second tubes between which there slides a cylinder whose outer end supports a running gear; a strut surrounding the top of the rod and including a steering mechanism cooperating with a rotary tube disposed between the rod and the strut; and a fluid actuator constituted by at least one chamber between the strut and the rod and having a feed inlet only. The landing gear is particularly applicable to helicopters that are required to "kneel down" camel fashion, e.g., for storage in the hold of an aircraft carrier or a cargo plane.

REFERENCES:
patent: 2712422 (1955-07-01), Gerwig
patent: 3401577 (1968-09-01), Partridge
patent: 4291850 (1981-09-01), Sharples

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