Aircraft landing gear with vibration damper

Details Aircraft landing gear with vibration damper Aircraft landing gear with vibration damper

B - Operations, Transporting

64

C

B64C 25/50 (2006.01) B64C 25/58 (2006.01)

Patent

CA 2511067

The present invention relates to an aircraft landing gear with a landing gear housing and a connecting rod accommodated therein, having a first and a second steering arm, the first steering arm of which being directly or indirectly connected with the landing gear housing and the second steering arm directly or indirectly with the connecting rod, and with a vibration damper which has a housing and a damping element, the damping element being movable in a fluid-filled area, preferably an oil-filled area of the vibration damper in such a way that the movement of the damping element is damped by the fluid, and the first or the second steering arm being indirectly or directly connected with the housing and the other steering arm directly or indirectly with the damping element, and with a fluid reservoir, preferably an oil reservoir, which is connected with the fluid-filled area, the fluid reservoir being integrated in the housing of the vibration damper.

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