SINGLE AXLE, SEMI-LEVERED LANDING GEAR WITH SHORTENING MECHANISM

A landing gear including a shock strut assembly including an outer cylinder coupled to an airframe, a wheel movably coupled to the outer cylinder so as to reciprocate substantially along a longitudinal axis of the outer cylinder, and a shrink mechanism including a pivot arm pivotally coupled to the...

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Bibliographische Detailangaben
Hauptverfasser: Sonnenburg, George, Cottet, Justin D, Mellor, Mitchell, Drake, Michael L
Format: Patent
Sprache:eng
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