首页> 外国专利> Unmanned shock system with variable wing sweep

Unmanned shock system with variable wing sweep

机译:可变机翼后掠无人冲击系统

摘要

FIELD: aeronautics; aviation.SUBSTANCE: invention relates to military technology and can be used in automatic complexes for mastering the enemy. Unmanned strike system contains an aircraft with a combat element and is equipped with a control unit, satellite navigation system, video camera, range finder, which determines the distance from the UAV to the target and is electrically connected with the control unit, and the control unit provides the operation of the combat element at a given distance to the target. Wing consoles of the aircraft are movable relative to the body and can be fixed in two positions. Fixation is carried out with pins entering the sleeves fixed in consoles. Longitudinal movement of the pins is carried out by a servo drive.EFFECT: long-term locking and high speed dive to hit the target is provided.1 cl, 4 dwg
机译:领域:航空;航空航天。物质:本发明涉及军事技术,可用于自动装置以控制敌人。无人打击系统包含一架带有战斗机的飞机,并配备有控制单元,卫星导航系统,摄像机,测距仪,用于确定从无人机到目标的距离,并与控制单元和控制装置电气连接单位可在距目标一定距离处提供战斗要素的操作。飞机的机翼控制台可相对于机身移动,并可固定在两个位置。固定是通过销钉进入固定在控制台中的套筒来进行的。销的纵向移动是通过伺服驱动器进行的。效果:提供了长期锁定和高速俯冲以击中目标的能力。1cl,4 dwg

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号