Adaptive airplane landing gear

Aeronautics and astronautics – Landing gear – Wheel

Patent

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Details

267 64R, 188299, 188289, B64C 2558

Patent

active

042733030

ABSTRACT:
A duo mode gas hydraulic shock absorbing landing gear strut with a pneumatic spring in combination with a hydraulic fluid controlling orifice for touchdown and automatic means for changing mode after touchdown to impart new pneumatic spring characteristics and to provide duo paths for controlling hydraulic fluid flow.

REFERENCES:
patent: 2735674 (1956-02-01), Smith et al.
patent: 2814482 (1957-11-01), Anderson et al.
patent: 3458016 (1969-07-01), Keech
patent: 3598207 (1971-08-01), Hartel
patent: 3696894 (1972-10-01), Brady et al.
patent: 3724832 (1973-04-01), Ceska
patent: 4065078 (1977-12-01), Jenkins

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