Landing gear having a gas vessel, and methods of maintaining...

Aeronautics and astronautics – Landing gear – Wheel

Reexamination Certificate

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Reexamination Certificate

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11078103

ABSTRACT:
A landing gear includes a shock absorber having first and second elements slidable relative to each other, the slidable elements defining an inside volume which is filled in part with hydraulic fluid so as to leave a first chamber filled with gas under pressure and located at the end of one of the slidable elements. A vessel filled with gas under pressure is housed in the end and is provided with a shutter member that is initially in a closed state and that is suitable for taking up a stable open state when the pressure in the first chamber exceeds the pressure in the vessel by a predetermined threshold amount.

REFERENCES:
patent: 1950995 (1934-03-01), Piecard
patent: 2367977 (1945-01-01), Thornhill
patent: 2389849 (1945-11-01), Gruss
patent: 2721074 (1955-10-01), De Carbon
patent: 3533613 (1970-10-01), Bendicsen
patent: 3540683 (1970-11-01), Foster
patent: 3724832 (1973-04-01), Ceska
patent: 3888436 (1975-06-01), Sealey
patent: 3889904 (1975-06-01), Jones et al.
patent: 4088286 (1978-05-01), Masclet et al.
patent: 4426109 (1984-01-01), Fike, Jr.
patent: 0546902 (1993-06-01), None
patent: 2686857 (1993-08-01), None
patent: 430337 (1935-06-01), None
patent: 637360 (1950-05-01), None

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