首页> 外国专利> Frame element for aircraft component assembly system, has connecting struts that are provided with recesses for receiving ribs of aircraft structure when frame element is attached to aircraft structure

Frame element for aircraft component assembly system, has connecting struts that are provided with recesses for receiving ribs of aircraft structure when frame element is attached to aircraft structure

机译:用于飞机部件组装系统的框架元件,具有连接支柱,当框架元件附接到飞机结构上时,该连接支柱设有用于容纳飞机结构的肋的凹部

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.
机译:可附接到飞机结构的框架元件(10)具有用于将飞机内部组件或隔热组件紧固到框架元件的紧固装置。框架元件的连接支柱(16,18)设有凹口(26,28,30,32),当框架元件被附接到飞机结构上时,该凹口用于容纳飞机结构的肋。包括对将飞机内部部件安装在飞机中的方法的独立权利要求。

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