发明名称 AIRCRAFT LANDING GEAR SHOCK STRUT PERFORMANCE MONITORING
摘要 A system and various methods (200; 300; 400) for monitoring and evaluating the health of a shock strut assembly are illustrated. Multiple sensors (110; 112; 114; 116), including gas temperature (112), gas pressure (110), oil pressure (114), and position sensor (116), 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.
申请公布号 EP2921404(A1) 申请公布日期 2015.09.23
申请号 EP20150159503 申请日期 2015.03.17
申请人 GOODRICH CORPORATION 发明人 FAZELI, AMIR;CEPIC, ADNAN;REBER, SUSANNE
分类号 B64C25/60;G01M17/04 主分类号 B64C25/60
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