发明名称 GUIDED MISSILE ACTUATOR ASSEMBLY
摘要 FIELD: defence equipment, applicable in design development of guided missiles. SUBSTANCE: actuator assembly improves the dynamic characteristics of the actuator assembly by increasing the developed torque due to spacing of the hinge axes of each pair of control surfaces along the missile longitudinal axis at a distance of not more than 0.4 of the caliber of the control actuator compartment, arrangement of the actuators on different sides of the control - surface hinge axes. EFFECT: improved dynamic characteristics. 2 dwgh
申请公布号 RU2101667(C1) 申请公布日期 1998.01.10
申请号 RU19960119611 申请日期 1996.10.01
申请人 KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA 发明人 ZYBIN I.M.;FIMUSHKIN V.S.;GOLOVANOV N.S.;ZYBIN I.M.;FIMUSHKIN V.S.;GOLOVANOV N.S.
分类号 F42B15/00;F42B10/60;(IPC1-7):F42B15/00 主分类号 F42B15/00
代理机构 代理人
主权项
地址