发明名称 Landing gear system
摘要 <p>A method and apparatus for changing a length of a landing gear system. A first cylinder and a second cylinder are moved relative to each other along an axis extending centrally through the first cylinder and the second cylinder such that the first cylinder and the second cylinder are in an extended position. In response to the first cylinder and the second cylinder being in the extended position, a flow of a fluid is substantially prevented between a first chamber formed between the first cylinder and the second cylinder and a second chamber within the first cylinder and the second cylinder. In response to a pressure applied to the first chamber, the first cylinder and the second cylinder are moved relative to each other along the axis such that a length of the first cylinder and the second cylinder is reduced.</p>
申请公布号 EP2505499(B1) 申请公布日期 2015.12.09
申请号 EP20120159953 申请日期 2012.03.16
申请人 THE BOEING COMPANY 发明人 COTTET, JUSTIN DUANE
分类号 B64C25/60;B64C25/00;B64C25/10;B64C25/22 主分类号 B64C25/60
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