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.
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 代理人
主权项
地址