首页> 外国专利> POWER GYROSCOPIC DEVICE COMPONENT FOR ONBOARD CONTROL MOMENT OF ARTIFICIAL EARTH SATELLITE

POWER GYROSCOPIC DEVICE COMPONENT FOR ONBOARD CONTROL MOMENT OF ARTIFICIAL EARTH SATELLITE

机译:人造地球卫星机载控制力矩的动力陀螺装置组件

摘要

FIELD: physics, measurement.;SUBSTANCE: invention refers to electromechanical actuators of satellite position control systems. Power gyroscopic device component for onboard control moment of artificial Earth satellite contains electric motor with cylindrical flywheel on its axis coaxial to rotor of electric motor. Aspect of invention is that the flywheel completely covers stator of electric motor and is provided with grooves parallel to electric motor axis. These grooves contain conducting rods interconnected with end electroconductive washers and decelerating rotation in geomagnetic field. Electric motor knot represents tube fixed on stator of electric motor and coaxial to rotor with a flange on its end. Power cable is sunk inside of the tube and a flange. Bearing with one of end electroconductive washers is mounted on the tube between flange and stator of the electric motor.;EFFECT: provided saving of working substance of jet engines within satellite position control system.;1 dwg
机译:技术领域:本发明涉及卫星位置控制系统的机电致动器。用于人造地球卫星的机载控制力矩的动力陀螺仪设备部件包含电动机,该电动机具有在其轴线上与电动机的转子同轴的圆柱形飞轮。本发明的方面在于,飞轮完全覆盖电动机的定子并且设置有平行于电动机轴线的凹槽。这些凹槽包含与端部导电垫圈互连并在地磁场中减速旋转的导电杆。电动机结表示固定在电动机定子上并与转子同轴且末端带有法兰的管。电源线沉入管子和法兰的内部。带有一个端部导电垫圈的轴承安装在电动机的法兰和定子之间的管上。效果:在卫星位置控制系统中节省了喷气发动机的工作物质。1 dwg

著录项

  • 公开/公告号RU2343419C1

    专利类型

  • 公开/公告日2009-01-10

    原文格式PDF

  • 申请/专利权人 MANTASHJAN PAVEL NIKOLAEVICH;

    申请/专利号RU20070118470

  • 发明设计人 MANTASHJAN PAVEL NIKOLAEVICH;

    申请日2007-05-17

  • 分类号G01C21/18;

  • 国家 RU

  • 入库时间 2022-08-21 19:10:47

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