发明名称
摘要 The structure unit (1) has a set of support frames and a longitudinal reinforcing rib arranged between the support frames, where the structure unit is designed in a self-supportable manner and is mounted in an airplane structure (5) and a floor structure (6). The reinforcing rib transmits force along a longitudinal axis of an airplane, where the structure unit is movable along the longitudinal axis of the airplane. Independent claims are also included for the following: (1) a cabin arrangement for mounting a cabin installation unit with a cabin structure unit (2) a method for mounting a cabin installation unit for an airplane.
申请公布号 JP2010505695(A) 申请公布日期 2010.02.25
申请号 JP20090531775 申请日期 2007.10.11
申请人 发明人
分类号 B64D11/00 主分类号 B64D11/00
代理机构 代理人
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