Landing gear deployment systems and methods

摘要

Some embodiments provide apparatuses configured to deploy a landing gear of an aircraft, comprising: a landing gear coupler 312 configured to couple with the landing gear; a release link 314 configured to cooperate the landing gear coupler with a drive shaft 114 that is configured to drive the landing gear between a stowed position and a deployed position; an override driver 316 cooperated with the landing gear coupler; wherein the release link is configured to releasably maintain a relative position of landing gear coupler relative to the drive shaft, and the release link is configured to disengage a coupling between the drive shaft and the landing gear coupler such that the landing gear coupler is configured to move independent of the drive shaft; and wherein the override driver is configured to drive the landing gear coupler to the deployed position.