发明名称 Composite leg structure for lightweight aircraft seat assembly
摘要 A lightweight leg assembly for an aircraft seat assembly includes a leg frame 10 comprising at least one leg attachment bracket 2 and a main frame member 11 carried by the at least one leg attachment bracket 2 and comprising a thermoplastic material. At least one track fitting 22 may be carried by the leg frame. The leg assembly may further comprise a frame brace 20 extending from the leg attachment bracket 2. A frame stabilizer 25 is preferably provided extending from the leg attachment bracket, said stabilizer comprising a pair of stabilizer arms 26 between which a shock absorber 70 is provided. A method of fabricating a leg assembly for an aircraft seat assembly using thermoplastic plies is also disclosed.
申请公布号 GB2462900(A) 申请公布日期 2010.03.03
申请号 GB20090010384 申请日期 2009.06.15
申请人 THE BOEING COMPANY 发明人 JAMES A FULLERTON;MAX U KISMARTON
分类号 B64D11/06;B60N2/68 主分类号 B64D11/06
代理机构 代理人
主权项
地址