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发明申请
US20090272849A1 Frame element, aircraft component assembly system and method of fitting a component in an aircraft 有权
框架元件，飞机部件组装系统以及在飞行器中安装部件的方法

Frame element, aircraft component assembly system and method of fitting a component in an aircraft
摘要：
A frame element (10; 10′) for use in an aircraft component assembly system (46) is attachable to an aircraft structure (36) and comprises at least one fastening device for fastening at least one aircraft interior component (34) or at least one insulation pack (52) to the frame element (10; 10′). An aircraft component assembly system (46) comprises a plurality of such frame elements (10; 10′). In a method of fitting a component (34, 52) in an aircraft, a frame element (10; 10′) is provided. At least one interior component (34) or at least one insulation pack (52) is fastened to the frame element (10; 10′). Then the frame element (10; 10′) having the at least one interior component (34) or the at least one insulation pack (52) fastened thereto is attached to an aircraft structure (36).
摘要（中）：

用于飞行器部件组装系统（46）的框架元件（10; 10'）可附接到飞机结构（36），并且包括用于紧固至少一个飞行器内部部件（34）或至少 一个绝缘包（52）连接到所述框架元件（10; 10'）。 飞机部件组装系统（46）包括多个这样的框架元件（10; 10'）。 在一种将部件（34,52）装配在飞行器中的方法中，提供了一个框架元件（10; 10'）。 至少一个内部部件（34）或至少一个绝缘包（52）被紧固到所述框架元件（10; 10'）。 然后，具有固定到其上的至少一个内部部件（34）或至少一个绝缘包装（52）的框架元件（10; 10'）附接到飞行器结构（36）。

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