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