A landing gear arrangement may comprise a shock strut, a retraction actuator, and a shrink actuator. The retraction actuator may move the shock strut between a stowed position and a deployed position. The shrink actuator may move between a shrink position and an unshrink position in response to the shock strut moving between the stowed position and the deployed position.
Landing gear arrangement with passive shock strut shrink actuator
2019-11-26
Patent
Elektronische Ressource
Englisch
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