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.
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
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