Lockheed Martin Corporation
FAIL-SAFE TAIL ROTOR SYSTEM
Last updated:
Abstract:
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.
Status:
Application
Type:
Utility
Filling date:
25 Dec 2019
Issue date:
1 Jul 2021