发明名称 elemento de armaÇço, sistema de montagem de componentes de aeronave, e, mÉtodo de montar um componente em uma aeronave
摘要 The frame element (10) which is attachable to an aircraft structure has a fastening device for fastening aircraft interior component or insulation pack to the frame element. The connecting struts (16,18) of the frame element are provided with recesses (26,28,30,32) for receiving the ribs of the aircraft structure when the frame element is attached to the aircraft structure. An independent claim is included for method of fitting aircraft interior component in an aircraft.
申请公布号 BRPI0715734(A2) 申请公布日期 2013.09.24
申请号 BR2007PI15734 申请日期 2007.08.21
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 CHRISTIAN KOEFINGER;JOACHIM METZGER;MICHAEL AUBURGER
分类号 B64C1/12;B64C1/40;B64D11/00 主分类号 B64C1/12
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