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Steady detonation combustor and steady detonation wave generation method

机译:稳态爆震燃烧器及稳态爆波产生方法

摘要

A steady-state detonation combustor and a steady-state detonation wave generating method, in which a stabilized detonation wave can be generated by generating a hypersonic and unburned premixed gas. An rich premixed gas whose gas fuel is rich is combusted in a rich premixed gas combustion chamber ( 11 ) to generate a fist high-temperature and high-pressure burned gas, while at the same time, a lean premixed gas whose oxygen is rich is combusted in a lean premixed gas combustion chamber ( 12 ) to generate a second high-temperature and high-pressure burned gas, and subsequently, after each high-temperature and high-pressure burned gas is accelerated to hypersonic speed and at the same time mixed together through an interpenetrating nozzle ( 40 ), a premixed gas obtained by the mixture and containing the gas fuel and the oxygen which are unreacted is impinged on a steady-state detonation stabilizer ( 60 ), so that a stabilized detonation wave is generated.
机译:稳态爆震燃烧器和稳态爆震波产生方法,其中可以通过产生高超音速和未燃烧的预混合气体来产生稳定的爆震波。气体燃料浓的浓预混合气在浓预混合气燃烧室(11)中燃烧,产生第一高温高压燃烧气体,同时,富氧的稀薄预混合气被富集。在稀薄的预混合气体燃烧室(12)中燃烧以产生第二种高温高压燃烧气体,随后,在每种高温高压燃烧气体被加速至高超声速并同时混合之后通过互穿喷嘴(40)一起,将由混合物获得的并且包含未反应的气体燃料和氧气的预混合气体撞击在稳态爆震稳定器(60)上,从而产生稳定的爆震波。

著录项

  • 公开/公告号JP3981743B2

    专利类型

  • 公开/公告日2007-09-26

    原文格式PDF

  • 申请/专利号JP20030586471

  • 发明设计人 笠原 次郎;

    申请日2002-04-19

  • 分类号F23R3/42;F23R3/20;F23R7;F02C5;F02C7/264;F02C7/266;F02K9/95;F02K7/02;

  • 国家 JP

  • 入库时间 2022-08-21 21:10:53

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