首页> 外国专利> Improved system for controlling thrust vector aerospace, 2004.

Improved system for controlling thrust vector aerospace, 2004.

机译:改进的用于控制推力矢量航空航天的系统,2004年。

摘要

The invention relates to a control system of the thrust vector for aerospace and controlling a vehicle propelled by a motor of the type of reaction. The control system of the thrust vector improved simultaneously rotate and move laterally to the reaction motor 16 with respect to the longitudinal axis 14 of the vehicle. This complex movement of the jet engine generates control of the moments of sufficiently large, which makes it possible to the motor to the reaction of being very closely related to the center of gravity of the vehicle 10 12. It follows that the vehicle can be shorter and that the structure which is typically necessary to position the jet engine by a pivot point located further back is eliminated.
机译:本发明涉及用于航空航天的推力矢量的控制系统,并控制由反作用类型的电动机驱动的车辆。改进的推力矢量的控制系统同时旋转并相对于车辆的纵轴14相对于反作用电动机16横向移动。喷气发动机的这种复杂的运动产生了足够大的力矩的控制,这使得电动机能够做出与车辆10 12的重心非常紧密相关的反应。由此可以使车辆更短并且消除了通常通过位于更靠后的枢轴点来定位喷气发动机所需的结构。

著录项

  • 公开/公告号FR2626318A1

    专利类型

  • 公开/公告日1989-07-28

    原文格式PDF

  • 申请/专利权人 TRW INC;

    申请/专利号FR19890000956

  • 发明设计人 RIMVYDAS ALEXANDER KAMINSKAS;

    申请日1989-01-26

  • 分类号B64C15/02;B64G1/00;B64G1/26;B64G1/40;F02K9/84;

  • 国家 FR

  • 入库时间 2022-08-22 06:30:00

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