发明名称 Rotor apparatus and methods for vertical lift aircraft
摘要 <p>A rotor blade assembly and a method of operation is disclosed. The blade assembly comprises an elongated support member (124),a rotor blade (116) operatively coupled to the support member, the rotor blade including an inboard end portion, and a lag damper assembly (184). The lag damper assembly includes a housing portion (186) having at least one first engagement surface (194), and a slide member portion (196) having at least one second engagement surface (194), at least one of the housing portion (186) and the slide member portion (196) being coupled to the support member (124) proximate the inboard end portion of the rotor blade, the other of the housing portion and the slide member portion being adapted to be coupled to an adjacent structure, and wherein the first and second engagement surfaces are adapted to frictionally interact to at least partially dampen a movement of the support member relative to the adjacent structure. </p>
申请公布号 EP2236415(A3) 申请公布日期 2012.01.25
申请号 EP20100168654 申请日期 2006.07.26
申请人 THE BOEING COMPANY 发明人 KISMARTON, MAX U.
分类号 B64C27/51 主分类号 B64C27/51
代理机构 代理人
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