首页> 外国专利> STIFFENER FOR AN AIRCRAFT FUSELAGE, METHOD FOR MANUFACTURING SAME, AND AIRCRAFT FUSELAGE EQUIPPED WITH SUCH A STIFFENER

STIFFENER FOR AN AIRCRAFT FUSELAGE, METHOD FOR MANUFACTURING SAME, AND AIRCRAFT FUSELAGE EQUIPPED WITH SUCH A STIFFENER

机译:飞机机身的加脂剂,其制造方法以及装有这种加劲剂的飞机机身

摘要

This stiffener is intended for a fuselage. It comprises a hollow section that can be trapezoidal, with a base attached to the fuselage or to the floor, high enough rising sides and a top side contributing to the rigidity and cohesion of the stiffener. A direct assembly with the fuselage is possible. The base is made of two edges provided one on the other or in front of the other. This rigid stiffener, in spite of its discontinuous section, can be manufactured by simple foldings of a planar metal sheet at the beginning.
机译:该加劲肋用于机身。它包括一个可以是梯形的中空部分,其底部固定在机身或地板上,足够高的上升侧和顶侧有助于加强板的刚度和内聚力。可以直接与机身组装。基座由两个边缘组成,两个边缘一个接一个,另一个位于另一个的前面。尽管具有不连续的截面,但这种刚性加劲肋可以在开始时通过简单折叠平面金属板来制造。

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