首页> 外国专利> Combined supersonic/hypersonic combustion ramjet has air injector system for reflection of supersonic intake air

Combined supersonic/hypersonic combustion ramjet has air injector system for reflection of supersonic intake air

机译:超音速/超人性燃烧冲压喷气发动机具有空气喷射器系统,可反射超音速进气

摘要

The system has a high pressure compressor, which feeds compressed intake air into a combustion chamber. A small nozzle generates an injector jet to suck fresh air into larger jet system. This is a combined combustion ramjet, which works with dynamic pressure effect at high speeds. The jet system is mainly formed by a tube, with an adjustable constriction at the front end. The injection nozzles are placed at this point, so that the combustion ramjet can also burn fuel. The air intake is formed so that the air is deflected through 45 deg , to pass through the constriction.
机译:该系统具有高压压缩机,该压缩机将压缩的进气导入燃烧室。小喷嘴产生喷射器射流,将新鲜空气吸入较大的射流系统。这是一种组合式燃烧冲压发动机,可在高速下发挥动态压力作用。喷射系统主要由管子组成,在前端有可调节的收缩。喷嘴位于此位置,因此燃烧冲压发动机也可以燃烧燃料。形成进气口,以使空气偏转45度,以通过缩颈。

著录项

  • 公开/公告号DE19932093A1

    专利类型

  • 公开/公告日2001-01-11

    原文格式PDF

  • 申请/专利权人 ITTNER GERHARD;

    申请/专利号DE1999132093

  • 发明设计人 ITTNER GERHARD;

    申请日1999-07-09

  • 分类号F02K7/10;

  • 国家 DE

  • 入库时间 2022-08-22 01:10:24

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