发明名称 Quick fit overhead stowage compartment
摘要 <p>A removable stowage bin assembly (10) for quick conversion of an aircraft between a passenger-carrying mode and a cargo-carrying mode includes a stowage bin (14) and a first assembly comprised of a clevis fitting (32) attached to the framework of the aircraft and a hook (34) attached to the stowage bin, the hook being removably and pivotally attachable to the clevis fitting. A second assembly is comprised of a tie rod (54) having a first end pivotally attached to the framework of the aircraft and a bracket (53) attached to the stowage bin. The tie rod has a second end attachable to the framework of the aircraft in a cargo-carrying mode and attachable to the bracket on the stowage bin in a passenger-carrying mode. A third assembly is compromised of a female fitting (79) having an opening and attached to one of the framework of the aircraft and the stowage bin, and a male fitting (84) having a protrusion and attached to the other of the framework of the aircraft and the stowage bin. The protrusion of the male fitting is mateable in the opening of the female fitting in the passenger-carrying mode. &lt;IMAGE&gt;</p>
申请公布号 EP0861781(A2) 申请公布日期 1998.09.02
申请号 EP19980301385 申请日期 1998.02.25
申请人 HEXCEL CORPORATION 发明人 SPENCER, MARTIN C.
分类号 B64D11/00;(IPC1-7):B64D11/00 主分类号 B64D11/00
代理机构 代理人
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