发明名称 Hydraulic actuator for semi levered landing gear
摘要 A device including a first hydraulic piston (206), a second hydraulic piston (202) disposed within the first hydraulic piston, and a third hydraulic piston (204) disposed within both the first hydraulic piston and the second hydraulic piston. The first, second, and third hydraulic pistons are contained within a common outer wall (214). A manifold (210,212,215) is connected to the first, second, and third hydraulic pistons. The manifold is disposed relative to the first, second, and third hydraulic pistons such that a fluid moving in the manifold can control positions of the first, second, and third hydraulic pistons.
申请公布号 EP2455283(B1) 申请公布日期 2016.08.24
申请号 EP20110188624 申请日期 2011.11.10
申请人 THE BOEING COMPANY 发明人 LINDAHL, GARY M.;MELLOR, MITCHELL LOREN RAY
分类号 F15B15/16;B64C25/22;B64C25/34;B64C25/60 主分类号 F15B15/16
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