发明名称 BLOCK OF STEERING DRIVE OF GUIDED MISSILE
摘要 FIELD: rocket engineering. SUBSTANCE: feedback potentiometer is mounted on body in block of steering drive, is positioned along side chord of control vanes and is connected to rod of vanes of machine and to lever of axle of vanes. Fork is mounted on this lever for turning with respect to lever put of axis of feedback potentiometer. EFFECT: improved operational reliability. 2 dwgc
申请公布号 RU2121649(C1) 申请公布日期 1998.11.10
申请号 RU19970113545 申请日期 1997.08.06
申请人 KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA 发明人 BABICHEV V.I.;ZYBIN I.M.;FIMUSHKIN V.S.
分类号 F42B15/00;(IPC1-7):F42B15/00 主分类号 F42B15/00
代理机构 代理人
主权项
地址