发明名称 Connection arrangement for connecting secondary carrier structure to floor cross beam of airplane for receiving e.g. installation spacer, has connector and receiving element whose relative movement is made towards axis of movement
摘要 <p>#CMT# #/CMT# The arrangement (6) has a link assembly (8) comprising a connector (10) and a receiving element (12) that are releasbly interlocked in a form-fit manner, where the connector is arranged at a component portion and the receiving element is arranged at a base part. A load is transferrable toward a major axis (h) and relative movement between the connector and the receiving element is made towards axis of movement (b). A retainer is formed in a head portion for cooperation with a twist lock element. #CMT# : #/CMT# An independent claim is also included for a method for attaching a component to a base part. #CMT#USE : #/CMT# Connection arrangement for connecting a component i.e. secondary carrier structure, to a base part i.e. primary structure such as floor cross beam, of an airplane for receiving an installation spacer and a booth system. #CMT#ADVANTAGE : #/CMT# The link assembly and/or the connector and the receiving element can be conveniently preassembled, so that the actual assembly and/or the final assembly of the link assembly is made in a sliding movement. The load is transferrable toward the major axis and relative movement between the connector and the receiving element is made towards axis of movement, thus preventing compulsive forces. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a schematic perspective view of a connection arrangement for connecting a component to a base part. b : Axis of movement h : Major axis 6 : Connection arrangement 8 : Link assembly 10 : Connector 12 : Receiving element.</p>
申请公布号 DE102011085450(A1) 申请公布日期 2013.05.02
申请号 DE20111085450 申请日期 2011.10.28
申请人 AIRBUS OPERATIONS GMBH 发明人 EILKEN, WOLFGANG;TIRYAKI, MEMIS;SAUER, DANIEL
分类号 F16B7/04;B64C1/00;B64C7/00;F16B17/00;F16L3/233 主分类号 F16B7/04
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