An aircraft landing gear is disclosed having a first oleo strut include a sleeve portion and a slider portion, the slider portion being slidable within a hydraulic fluid chamber of the sleeve portion, and a second, similar oleo strut. The landing gear also includes a hydraulic fluid balancer having a balance chamber separated into first and second end sections, wherein the hydraulic fluid chamber of the sleeve portion of the first oleo strut is fluidly connected to the first section of the balance chamber and the hydraulic fluid chamber of the sleeve portion of the second oleo strut is fluidly connected to the second section of the balance chamber of the hydraulic fluid balancer.
AIRCRAFT LANDING GEAR
FLUGZEUGFAHRWERK
TRAIN D'ATTERRISSAGE D'AÉRONEF
2024-01-31
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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