Invention Grant
- Patent Title: Aircraft landing gear shock strut performance monitoring
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Application No.: US14456632Application Date: 2014-08-11
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Publication No.: US09773357B2Publication Date: 2017-09-26
- Inventor: Amir Fazeli , Adnan Cepic , Susanne Reber
- 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: G06F11/30
- IPC: G06F11/30 ; G07C5/08 ; B64C25/60 ; G01M17/04

Abstract:
A system and various methods for monitoring and evaluating the health of a shock strut assembly are illustrated. Multiple sensors, including gas temperature, gas pressure, oil pressure, and position sensor, may be used to gather data and evaluate the performance of the shock strut assembly. Various methods illustrated herein may evaluate the dynamic damping, static load support, and/or controlled stroke performance of the shock strut assembly.
Public/Granted literature
- US20150269794A1 AIRCRAFT LANDING GEAR SHOCK STRUT PERFORMANCE MONITORING Public/Granted day:2015-09-24
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