发明名称 |
Releasably fastening cover to structure of aircraft - using conical plug engaging with cap by means of interlocking formations. |
摘要 |
Releasable fastening devices for fixing a cover (2) to a secondary structure (1) of an aircraft each have a conically shaped plug (6) and cap (4). Ring formations (10,11) on the plug and cap respectively create a locking interengagement therebetween. A resilient sealing sleeve (8) surrounds the plug. The plug is made of a resilient material to allow deformation of the ring formations when the plug and cap are pressed together. The interlocking ring formations are of square or rectangular cross-section. A centralising pin (13) formed in the cap engages with a bore (14) in the plug. USE/ADVANTAGE - Low-cost fastening devices which cause less damage to structure during fixing.
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申请公布号 |
DE4215843(A1) |
申请公布日期 |
1993.11.18 |
申请号 |
DE19924215843 |
申请日期 |
1992.05.14 |
申请人 |
DEUTSCHE AEROSPACE AIRBUS GMBH, 21129 HAMBURG, DE |
发明人 |
HARARAT-TEHRANI, MOHAMMAD, 2800 BREMEN, DE |
分类号 |
B64C1/12;F16B21/08;(IPC1-7):B64C7/00;F16B21/06 |
主分类号 |
B64C1/12 |
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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