Aircraft landing gear assembly including a health and usage monitoring system (HUMS) and method

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United States of America Patent

PATENT NO 10858120
APP PUB NO 20170113811A1
SERIAL NO

15297723

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Abstract

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A health and monitoring system or “HUMS” mounted within a hollow structural subassembly of an aircraft landing gear assembly, the subassembly having an access port for access to the HUMS without requiring disassembly of the structural subassembly so as to require jacking up the aircraft.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN LANDING SYSTEMS UK LIMITEDGLOUCESTER GL2 9QH

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Cokonaj, Valerijan Gloucester, GB 4 63

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