首页> 外国专利> Adhesive arrangement for gluing two structure components in air- or spacecraft, comprises first structure component, which consists of first material and has first adhesive surface, and a second structure component

Adhesive arrangement for gluing two structure components in air- or spacecraft, comprises first structure component, which consists of first material and has first adhesive surface, and a second structure component

机译：用于粘合航空器或航天器中的两个结构部件的粘合剂装置，包括第一结构部件和第二结构部件，该第一结构部件由第一材料构成并具有第一粘合表面，该第一结构部件具有第一粘合表面。

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摘要

The adhesive arrangement for gluing two structure components in air- or spacecraft, comprises first structure component (2), which consists of first material and has first adhesive surface (3), a second structure component (8), which consists of second material and has second adhesive surface (9), and a glue joint between first- and second adhesive surface. The glue joint comprises fiber and/or woven fiber structures. The fiber length is 10 mm and the fiber diameter is 0.001-0.3 mm. A coating is applied on the first- and second adhesive surface. The adhesive arrangement for gluing two structure components in air- or spacecraft, comprises first structure component (2), which consists of first material and has first adhesive surface (3), a second structure component (8), which consists of second material and has second adhesive surface (9), and a glue joint between first- and second adhesive surface. The glue joint comprises fiber and/or woven fiber structures. The fiber length is 10 mm and the fiber diameter is 0.001-0.3 mm. A coating is applied on the first- and second adhesive surface. The first structure component is formed as stringer for forming a reinforcement means, as Doppler or crack-stopper for preventing cracking or crack growth. The coating has thickness of 0.2 mu m. The first structure component and/or the second structure component are formed as structure components of a lightweight construction structure of an aircraft. The glue joint has a thickness of 0.01-0.3 mm. An independent claim is included for a method for the production of gluing two structure components in air- or spacecraft.

机译：用于在飞行器或航天器中粘合两个结构部件的粘合剂装置包括：第一结构部件（2），其由第一材料构成，并具有第一粘合表面（3）;第二结构部件（8），其由第二材料构成;以及具有第二粘合表面（9），以及在第一和第二粘合表面之间的胶接。胶接包括纤维和/或编织纤维结构。纤维长度为10mm，纤维直径为0.001-0.3mm。在第一和第二粘合表面上施加涂层。用于在飞行器或航天器中粘合两个结构部件的粘合剂装置包括：第一结构部件（2），其由第一材料构成，并具有第一粘合表面（3）;第二结构部件（8），其由第二材料构成;以及具有第二粘合表面（9），以及在第一和第二粘合表面之间的胶接。胶接包括纤维和/或编织纤维结构。纤维长度为10mm，纤维直径为0.001-0.3mm。在第一和第二粘合表面上施加涂层。第一结构部件形成为用于形成加强装置的桁条，用于防止裂纹或裂纹扩展的多普勒或裂纹阻止器。涂层的厚度为0.2μm。第一结构部件和/或第二结构部件形成为飞机的轻型结构的结构部件。胶接的厚度为0.01-0.3mm。包括对在航空器或航天器中粘合两个结构部件的制造方法的独立权利要求。

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公开/公告号DE102006026538A1

专利类型
公开/公告日2007-12-13

原文格式PDF
申请/专利权人 AIRBUS DEUTSCHLAND GMBH;
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申请/专利号DE20061026538
发明设计人 VICHNIAKOV ALEXEI;
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申请日2006-06-07
分类号C09J5/02;B32B7/12;
国家 DE
入库时间 2022-08-21 19:49:57

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