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发明申请
US20160375979A1 AIRCRAFT STRUCTURAL COMPONENT THAT IS ADAPTED FOR ABSORBING AND TRANSMITTING FORCES IN AN AIRCRAFT 审中-公开
适用于飞机吸收和发射力的飞机结构部件

AIRCRAFT STRUCTURAL COMPONENT THAT IS ADAPTED FOR ABSORBING AND TRANSMITTING FORCES IN AN AIRCRAFT
摘要：
An aircraft structural component that is adapted for absorbing and transmitting forces in an aircraft, the aircraft structural component comprising at least one panel element and at least one reinforcing structure. The at least one reinforcing structure is rigidly attached to the at least one panel element such that at least one cavity is defined between the at least one panel element and the at least one reinforcing structure, the at least one cavity being adapted for distributing forces that are absorbed by the aircraft structural component in operation.
摘要（中）：

一种适于在飞行器中吸收和传递力的飞行器结构部件，所述飞行器结构部件包括至少一个面板元件和至少一个加强结构。 所述至少一个加强结构刚性地附接到所述至少一个屏元件，使得至少一个空腔限定在所述至少一个屏元件和所述至少一个加强结构之间，所述至少一个空腔适于分配 被飞机结构部件所吸收。

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