首页> 外国专利> Form-stable pressure resistant casing for aircraft body, has stiffening ribs limiting polygonal fields of skin part, where polygonal fields comprise multiple hexagonal fields that are arranged in dense package next to each other

Form-stable pressure resistant casing for aircraft body, has stiffening ribs limiting polygonal fields of skin part, where polygonal fields comprise multiple hexagonal fields that are arranged in dense package next to each other

机译:用于飞机机体的形状稳定的耐压外壳,具有加强肋,限制了蒙皮部分的多边形区域,其中多边形区域包含多个六角形区域,这些区域在密集的包装中彼此相邻排列

摘要

The casing has a reinforcing structure (11) stiffening with a flexible and fluid-tight skin part of an aircraft (1), and stiffening ribs (12) running along a main plane of the skin part in various directions. The stiffening ribs limit polygonal fields of the skin part, where the polygonal fields comprise multiple hexagonal fields that are arranged in a dense package next to each other. The reinforcing structure and the skin part are made of composite materials. The hexagonal fields are mixed in a cylinder-sleeve-shaped region of the casing with the polygonal fields. An independent claim is also included for a method for manufacturing a form-stable casing.
机译:壳体具有用航空器(1)的柔性且不透流体的蒙皮部分进行加固的加强结构(11),以及沿着蒙皮部分的主平面在各个方向上延伸的加强肋(12)。加强肋限制皮肤部分的多边形场,其中多边形场包括以密集包装彼此相邻布置的多个六边形场。增强结构和皮肤部分由复合材料制成。六边形场在壳体的圆柱套筒形区域中与多边形场混合。还包括用于制造形状稳定的壳体的方法的独立权利要求。

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