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Shock-stabilized supersonic flame-jet method and apparatus

机译:冲击稳定的超音速火焰喷射方法和装置

摘要

A supersonic flame jet device includes a body having an entry portion (22) of relatively small cross-sectional area, an expanding supersonic nozzle section (23) and a cylindrical duct (21) of extended length connected in series with each other. In using the device, an oxidant (24) at high pressure is introduced into the entry passage (22) wherein the flow is increased to sonic velocity. The sonic velocity flow of the oxidant (24) is then introduced into the passage (23) of expanding cross-section in the direction of the gas flow while introducing a fuel (25) to be burned into the flow of the oxidant (24). The velocity of flow of the oxidant, or the oxidant and the fuel, is then increased to supersonic velocity prior to entry into the extended duct (23) of constant cross-sectional area where a shock (40) is produced to stabilize flame reactions along the extended duct length (21) whereby a supersonic flame jet will exit the extended duct.
机译:一种超音速火焰喷射装置,包括:主体,其具有相对较小的横截面积的入口部分; 22;扩张的超音速喷嘴部分(23);以及彼此串联连接的延伸长度的圆柱形管道(21)。在使用该装置时,将高压氧化剂(24)引入进入通道(22),在该通道中流量增加到声速。然后将氧化剂(24)的声速流引入沿气体流动方向扩展的横截面的通道(23),同时将待燃烧的燃料(25)引入氧化剂(24)的流中。 。然后,在进入具有恒定横截面面积的延伸管道(23)之前,将氧化剂或氧化剂和燃料的流速提高到超音速,在该管道中会产生冲击(40)来稳定沿火焰的反应延伸的管道长度(21),从而超音速火焰喷射器将离开延伸的管道。

著录项

  • 公开/公告号EP0734782A3

    专利类型

  • 公开/公告日1997-04-23

    原文格式PDF

  • 申请/专利权人 DRACO;

    申请/专利号EP19960104822

  • 发明设计人 BROWNING JAMES A.;

    申请日1996-03-26

  • 分类号B05B7/20;

  • 国家 EP

  • 入库时间 2022-08-22 03:20:17

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