发明名称 |
VORRICHTUNG UND VERFAHREN ZUR TRENNBAREN VERBINDUNG VON STRUKTURTEILEN, INSBESONDERE IN EINEM FLUGZEUG |
摘要 |
<p>Device (10) comprises a tension lever arrangement (12) assigned to a first component and a clamping pin (14) assigned to a second component. The clamping lever arrangement has an eccentric shaft (20) rotating about a rotary axis on the first component, a clamping lever (16) pivoting on the shaft and a bushing (18) coupled with the clamping lever. The clamping lever arrangement can be displaced between a release position, a ready position and a locking position. The clamping lever releases the clamping lever into the release position. An independent claim is also included for a method for detachedly connecting components in an aircraft using the above device. Preferred Features: The bushing pivots on the shaft. The clamping lever pivots on an eccentric section of the shaft relative to the rotary axis.</p> |
申请公布号 |
AT503901(T) |
申请公布日期 |
2011.04.15 |
申请号 |
AT20070786298T |
申请日期 |
2007.07.24 |
申请人 |
AIRBUS OPERATIONS GMBH |
发明人 |
STEINBECK, HERBERT;WAGNER, KONSTANTIN |
分类号 |
E05B65/08;E05C3/04 |
主分类号 |
E05B65/08 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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