Invention Application
US20110056197A1 LANDING GEAR UPLOCK MECHANISM EMPLOYING THERMAL PHASE-CHANGE ACTUATION 有权
采用热相变动作的起落架齿轮升降机构

LANDING GEAR UPLOCK MECHANISM EMPLOYING THERMAL PHASE-CHANGE ACTUATION
Abstract:
An uplock assembly for retaining and releasing landing gear systems, said uplock assembly comprising: a thermal actuator comprising: a chamber configured to contain expansible material therein; a heating mechanism coupled to said chamber for heating said expansible material and causing volumetric expansion thereof; a piston slidably coupled to said chamber and adapted to extend in response to said volumetric expansion; and an uplock release mechanism releasably engaged by said piston when extended such that said engaged uplock release mechanism causes the release of said landing gear.
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