AIRCRAFT LANDING GEAR STRUT
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United States of America Patent
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app pub date -
Dec 6, 2012
filing date -
Dec 7, 2011
priority date (Note) -
Abandoned
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Abstract
A landing gear rod (1) for an aircraft, the rod comprising a tubular portion (3) for receiving a shock absorber and an axle-carrier portion (2) situated at the end of the tubular portion (3) and adapted to receive a landing gear wheel support mechanism. The tubular portion (3) and the axle-carrier portion (2) are made of mutually distinct metal materials, the tubular portion (3) being made of a first metal material and the axle-carrier portion (2) being made of a second metal material, the tubular portion (3) and the axle-carrier portion (2) being connected together by at least one weld (4).
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