发明名称 Attachment arrangement and installation method
摘要 Disclosed is an attachment arrangement (1)for the attachment of a system (4) to a structure (2) in particular lines to a primary structure of an aircraft, having a base element (10) for retaining the system, a positioning element (12) for positioning the base element in a location on the structure and a fixation device (14) for the fixation of the base element in the location on the structure, wherein the base element has a holding section (18) for holding the system and a clamping section (20) for being clamped to the structure, wherein the clamping section has an alignment element for the alignment on the positioning element, wherein the positioning element has a bonding surface (36) for being bonded to the structure and a positioning section for acting together with the alignment element and wherein the fixation device has a counter element (40) with a clamping area (42) for being positioned on an opposite site on the structure to the clamping section and a fastener 34) for clamping the base element and the counter element to the structure, and an installation method for the installation of such an attachment arrangement.
申请公布号 EP2740982(B1) 申请公布日期 2016.09.28
申请号 EP20120195885 申请日期 2012.12.06
申请人 AIRBUS OPERATIONS GMBH 发明人 SAYILGAN, CIHANGIR;MÜLLER, MARKUS;LINNEMANN, HENRIK
分类号 F16L3/02;H02G3/00;H02G3/32 主分类号 F16L3/02
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