发明名称 |
Tube connection in particular for connecting two tubular elements of the airframe of a missile |
摘要 |
In a tube connection, particularly for connecting two tubular elements of the airframe of a substantially tubular a missile, the tubular elements to be interconnected have end portions of substantially identical shapes. Each end portion has a smaller-diameter first circumferential section extending through substantially 180 DEG and a larger-diameter second circumferential section also extending through substantially 180 DEG . The larger-diameter circumferential section of each tubular element overlies the smaller-diameter circumferential section of the other tubular element. The circumferential sections are provided with radial bores for connection screws. Arcuate elements having threaded bores are arranged inside the thus interconnected circumferential sections. These threaded bores are aligned with the radial bores of the circumferential sections and threadedly receive the connecting screws.
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申请公布号 |
US5876072(A) |
申请公布日期 |
1999.03.02 |
申请号 |
US19970845028 |
申请日期 |
1997.04.21 |
申请人 |
BODENSEEWERK GERATETECHNIK GMBH |
发明人 |
BROSS, DIRK;FISCH, PETER GERD |
分类号 |
F16L23/00;F16L23/04;(IPC1-7):F16L25/00;B64C1/00 |
主分类号 |
F16L23/00 |
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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