Invention Application
- Patent Title: TEMPERATURE COMPENSATED LANDING GEAR SHOCK STRUT
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Application No.: US18460173Application Date: 2023-09-01
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Publication No.: US20250026471A1Publication Date: 2025-01-23
- Inventor: HEMANTH M N , BASAVARAJ BODKI
- Applicant: Goodrich Corporation
- Applicant Address: US NC Charlotte
- Assignee: Goodrich Corporation
- Current Assignee: Goodrich Corporation
- Current Assignee Address: US NC Charlotte
- Priority: IN202341048227 20230718
- Main IPC: B64C25/60
- IPC: B64C25/60 ; F16F9/32

Abstract:
A landing gear assembly is provided. The landing gear assembly includes a shock strut. The shock strut includes a shock strut cylinder and a shock strut piston slidably disposed within the shock strut cylinder. The landing gear assembly further includes a temperature control unit assembly disposed within the shock strut cylinder. The temperature control unit assembly is configured to, responsive to a temperature within the shock strut cylinder falling below a predetermined temperature, circulate heated fluid into a chamber of the shock strut cylinder to heat gas within the shock strut cylinder.
Public/Granted literature
- US12291325B2 Temperature compensated landing gear shock strut Public/Granted day:2025-05-06
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