A health and monitoring system or "HUMS" (20a, 20b) mounted within a hollow structural subassembly (12) of an aircraft landing gear assembly (10), the subassembly having an access port (16) for access to the HUMS without requiring disassembly of the structural subassembly so as to require jacking up the aircraft.
AIRCRAFT LANDING GEAR ASSEMBLY INCLUDING A HEALTH AND USAGE MONITORING SYSTEM (HUMS) AND METHOD
FLUGZEUGLANDEFAHRWERKANORDNUNG MIT GESUNDHEITS- UND GEBRAUCHSÜBERWACHUNGSSYSTEM (HUMS) UND VERFAHREN
ENSEMBLE DE TRAIN D'ATTERRISSAGE D'AÉRONEF COMPRENANT UN SYSTÈME ET UN PROCÉDÉ DE SURVEILLANCE DE SANTÉ ET D'UTILISATION (HUMS)
2017-04-26
Patent
Electronic Resource
English
AIRCRAFT LANDING GEAR ASSEMBLY INCLUDING A HEALTH AND USAGE MONITORING SYSTEM (HUMS) AND METHOD
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