发明名称 |
Bearing arrangement for the rudder blades of a steerable missile |
摘要 |
Shaft journals (20) of the rudder blade mountings (16) are rigidly connected to be resistant to torsion via a coupling element (32). An annular element (28) is between a first annular shoulder (24) on the shaft journal and a second annular shoulder (26) on a rear structure (10) of the missile, so there is axial play (30). The coupling element may be eccentric, a bellows, or an arcuate protuberance.
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申请公布号 |
DE19827277(A1) |
申请公布日期 |
1999.12.23 |
申请号 |
DE19981027277 |
申请日期 |
1998.06.19 |
申请人 |
DIEHL STIFTUNG & CO. |
发明人 |
DOMMER, JOSEF;SCHROEPPEL, WERNER;STAUDENMEIR, MARTIN |
分类号 |
F42B10/64;(IPC1-7):F42B10/62;F42B10/00 |
主分类号 |
F42B10/64 |
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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