发明名称 Device for changing the position of the steering fins of a guided missile
摘要 The system controls a projectile which has at least two rudders and two sprockets. The latter are arranged parallel to each other on both sides of the rudder axles about the projectile fuselage. The sprockets are driven by pinions which are driven by electric motors and run continuously. Two free running drive wheels (11,17) are arranged on each rudder axle (18). The drive wheels are in engagement with sprockets (7,8) and rotate with them such that they run in opposite directions. A coupling plate (19) is arranged between the drive wheels. The coupling plate can be connected with a respective one of the drive wheels so that the rudder (3) is rotated in the desired direction.
申请公布号 EP0834717(A3) 申请公布日期 1999.05.06
申请号 EP19970116925 申请日期 1997.09.30
申请人 DAIMLER-BENZ AEROSPACE AKTIENGESELLSCHAFT 发明人 ULLRICH, HANS-GUENTER, ING.
分类号 F42B10/64 主分类号 F42B10/64
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