Invention Grant
- Patent Title: Shock strut shrinking system
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Application No.: US16533626Application Date: 2019-08-06
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Publication No.: US11235863B2Publication Date: 2022-02-01
- Inventor: Adam J. Ditzler
- Applicant: GOODRICH CORPORATION
- Applicant Address: US NC Charlotte
- Assignee: GOODRICH CORPORATION
- Current Assignee: GOODRICH CORPORATION
- Current Assignee Address: US NC Charlotte
- Agency: Snell & Wilmer L.L.P.
- Main IPC: B64C25/00
- IPC: B64C25/00 ; B64C25/10 ; B64C25/58

Abstract:
A system for shrinking landing gear includes a shock strut having a cylinder and a piston to be received by the cylinder. The system further includes a collar coupled to a brace linkage and the piston, a torque arm configured to resist rotation between the collar and the piston, and a shrink linkage coupled between the torque arm and the cylinder. The collar rotates relative to the cylinder in response to retraction of the landing gear. Rotation of the collar rotates the piston and the torque arm relative to the cylinder. The rotation of the collar relative to the cylinder forces, via the shrink linkage, the piston towards the aircraft attachment within the cylinder.
Public/Granted literature
- US20210039772A1 SHOCK STRUT SHRINKING SYSTEM Public/Granted day:2021-02-11
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