Aircraft landing gear shock absorber assembly

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 10625850
APP PUB NO 20180057154A1
SERIAL NO

15683075

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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An aircraft landing gear shock absorber assembly having an outer casing having a bore which extends through the outer casing. The bore has a first opening and a second opening. A rod is slidably coupled within the bore such that a first end of the rod projects out of the first opening of the bore, the first end of the rod being arranged to be attached to a wheel assembly. A closure is provided for the second opening of the bore. The bore has a reduced width portion relative to the second opening of the bore, and the rod includes a radially enlarged portion that is wider than the reduced width portion of the bore.

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First Claim

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Patent Owner(s)

Patent OwnerAddress
SAFRAN LANDING SYSTEMS UK LTDGLOUCESTER GLOUCESTERSHIRE GL2 9QH

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Schmidt, Robert Kyle Gloucester, GB 54 182

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