A hydro-elastic damper comprising at least one elastic assembly comprising an elastic member between two strength members. The elastic assembly including a compression chamber. The hydro-elastic damper includes a damping assembly provided with an expansion chamber that is defined in a transverse direction by an end wall and by a piston. The compression chamber is hydraulically connected to the expansion chamber by three hydraulic connections comprising respectively: a duct; at least one first passage with an overpressure valve; and at least one second passage with a check valve.
HYDRO-ELASTIC DAMPER AND AN AIRCRAFT
2019-10-03
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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