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Structural component for an air - or spacecraft, manufacturing method of the same, as well as air - or spacecraft

机译:航空器或航天器的结构部件,其制造方法以及航空器或航天器

摘要

The present invention relates to a structural component for an air - or spacecraft, wherein the structural component a temperature side skin member, a temperature side skin member struts fixed support body, which a corresponding to a surface portion of a rotary body shaped struts support surface, as well as a strut with a corresponding to a section of the surface of the rotary body shaped mating surface comprises. The counter surface is on the struts support surface is supported displaceably in such a way that a along the strut extending strut axis within the high temperature side skin member intersects a rotation axis of the rotary body. Further aspects, the invention relates to an air - or a spacecraft with such a structural component and a method for the manufacture of a structural component. The method comprises a step of providing a high temperature side skin member, a step of fixing of a struts support body, which a corresponding to a surface portion of a rotary body shaped struts support surface, on the temperature side skin member, and a step of the displaceable support of a brace, which a corresponding to a section of the surface of the rotary body has formed opposing surface, in such a way to the struts support surface, that a along the strut extending strut axis within the high temperature side skin member intersects a rotation axis of the rotary body.
机译:航空航天器的结构部件技术领域本发明涉及一种航空器或航天器的结构部件,其中该结构部件为温度侧蒙皮构件,温度侧蒙皮构件撑杆固定支撑体,其对应于旋转体形撑杆支撑表面的表面部分。 ,以及具有对应于旋转体形配合表面的一部分截面的支柱。相对表面在支柱支撑表面上以如下方式可移动地支撑,即,沿着支柱延伸的支柱在高温侧蒙皮构件内沿旋转轴线与旋转体的旋转轴线相交。此外,本发明涉及一种具有这种结构部件的航空器或航天器,以及一种用于制造结构部件的方法。该方法包括以下步骤:提供高温侧蒙皮构件;将支柱支撑体固定在温度侧蒙皮构件上的步骤,该支柱支撑体对应于旋转体形支柱支撑表面的表面部分;支撑件的可移动支撑件的一部分,对应于旋转体的表面的一部分形成了相对于支撑件支撑面的相对表面,使得沿支撑件的支撑杆在高温侧蒙皮内沿支撑件轴线延伸构件与旋转体的旋转轴相交。

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