发明名称 OUTPUT SHAFT ASSEMBLY FOR A MISSILE CONTROL ACTUATION UNIT
摘要 Accordingly, a shaft assembly for coupling a control fin to a missile includes outer and inner shaft portions which are detachably coupled together, allowing removal of one of the shaft portions while the other shaft portion remains in the missile. In an exemplary embodiment, the inner shaft portion, to which the control fin is coupled, is removable. The shaft assembly includes a pair of preload nuts to adjust the position of the control fin relative to the skin of the missile, the preload nuts being for example engaged on opposite threaded ends of the outer shaft portion.
申请公布号 US2002166921(A1) 申请公布日期 2002.11.14
申请号 US20010854273 申请日期 2001.05.11
申请人 JOHNSON GARY H.;OWAN CHRISTOPHER P.;HATALSKY WILLIAM M.;SUNNE WAYNE LEE 发明人 JOHNSON GARY H.;OWAN CHRISTOPHER P.;HATALSKY WILLIAM M.;SUNNE WAYNE LEE
分类号 F42B10/64;(IPC1-7):F42B15/01;F42B10/00 主分类号 F42B10/64
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