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STATOREACTOR FOR TELEGUID MISSILES

机译:远传导弹的法定代表人

摘要

Statoreactor for guided missiles. /P P Statoreactor for guided missiles with deflection of the thrust jet, in particular supersonic, in which the thrust nozzle comprises, connected to its extended end, an enlarged extension beyond the expansion ratio corresponding to the pressure surrounding and in which, for the deflection of the jet, control pulses acting each time in the direction of the desired deflection are delivered at the level of the control openings distributed in the peripheral direction of the nozzle. /P P The control openings 24B, 28A opening into a marginal zone of the outlet end 10 of the nozzle are connected to an injection system 14 supplying them with compressed gas or with fluid acting as ordered.
机译:制导导弹的静电反应器。

用于制导导弹并具有推力射流偏斜的静变反应器,尤其是超音速射流,其中推力喷嘴的延伸端连接有一个扩大的延伸部分,该延伸部分超过了对应于周围压力的膨胀比,并且对于喷嘴的偏转,每次在期望的偏转方向上起作用的控制脉冲在分布在喷嘴的圆周方向上的控制开口的高度处被传递。

开口到喷嘴出口端10边缘区域的控制孔24B,28A连接到注入系统14,向其供应压缩气体或按顺序作用的流体。

著录项

  • 公开/公告号FR2453279A1

    专利类型

  • 公开/公告日1980-10-31

    原文格式PDF

  • 申请/专利号FR19800006536

  • 发明设计人

    申请日1980-03-24

  • 分类号F02K9/80;

  • 国家 FR

  • 入库时间 2022-08-22 17:18:16

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