According to an aspect, a clevis assembly includes a shackle having two ends, each end respectively including an aperture, a structure connecting the apertures and housing a bearing, and a shearing device that includes a frangible point and is in operable communication with the bearing, where the shearing device is housed in a hollow portion of the structure.
FAIL-SAFE TAIL ROTOR SYSTEM
01.07.2021
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
FAIL SAFE Semi-active pantograph fail safe pneumatic control system
Europäisches Patentamt | 2025
|Kraftfahrwesen | 1988
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