An aircraft panel assembly is disclosed, and is with: a panel; and a plurality of stiffeners on the panel. Each stiffener has an attachment part attached to the panel and a structural part spaced apart from the panel. A rib foot beam crosses the stiffeners at a series of intersections. At each intersection the rib foot beam is located between the panel and the structural part of a respective one of the stiffeners.
一种飞行器面板组件,该飞行器面板组件具有:面板;以及位于面板上的多个加强件。每个加强件具有附接至面板的附接部分和与面板间隔开的结构部分。肋条支脚梁在一系列相交部处穿过加强件。在每个相交部处,肋条支脚梁位于面板与加强件中的相应一个加强件的结构部分之间。
AIRCRAFT PANEL ASSEMBLY
飞行器面板组件
2021-07-23
Patent
Electronic Resource
Chinese
European Patent Office | 2025
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