发明名称 DEPLOYMENT APPARATUSES
摘要 Embodiments of the present invention include a deployment apparatus comprising a deployment object, a deployment arm, a deployment link, a pivot housing, at least two linear guides, and a gas spring. The deployment object is coupled to the deployment arm, which is pivotally coupled to the deployment link. An opposing end of the deployment link is fixedly coupled to a structure. The pivot housing is adjacent the connection between the deployment link and the deployment arm. The pivot housing is slidingly engaged with the at least two linear guides. The gas spring is coupled to the pivot housing, which pushes the pivot housing to an upper end of the at least two linear guides and causes the deployment link to rotate the deployment arm from a stowed angle to a released angle and results in a displaced vertical distance.
申请公布号 EP2414235(A2) 申请公布日期 2012.02.08
申请号 EP20100722846 申请日期 2010.03.30
申请人 WEBER AIRCRAFT LLC 发明人 WESTERINK, RIK
分类号 B64D11/00 主分类号 B64D11/00
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