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Pulse detonation igniter for pulse detonation chambers

机译:脉冲爆震室的脉冲爆震点火器

摘要

A pulse detonation engine has a pulse ignition system, a plurality of detonation chambers (15), an oxygen source (33), and a fuel source (35). The oxygen source and the fuel source supply oxygen and fuel, respectively, to both the pulse ignition system and to the detonation chambers. The pulse ignition system creates detonation waves by igniting a first series of fuel mixtures inside a plurality of igniter tubes (39) equal to the number of detonation chambers (15). One detonation wave is delivered by each igniter tube into each detonation chamber for igniting a second series of fuel mixtures inside the detonation chambers. The detonation waves increase in magnitude as they travel through the detonation chambers before exiting the rearward ends of the detonation chambers. After detonation, the detonation engine is purged of residual gases by a ventilation system (81) and the process is repeated sequentially as described.
机译:脉冲爆震发动机具有脉冲点火系统,多个爆震室(15),氧气源(33)和燃料源(35)。氧气源和燃料源分别向脉冲点火系统和爆震室供应氧气和燃料。脉冲点火系统通过点燃多个点火器管(39)内的第一系列燃料混合物来产生爆炸波,所述多个点火器管等于爆炸室(15)的数量。每个点火器管将一个起爆波传送到每个起爆室中,以点燃起爆室内的第二系列燃料混合物。爆炸波在离开爆炸室的后端之前穿过爆炸室时,其强度会增加。引爆之后,引爆发动机通过通风系统(81)清除残留气体,并按顺序依次重复该过程。

著录项

  • 公开/公告号US5937635A

    专利类型

  • 公开/公告日1999-08-17

    原文格式PDF

  • 申请/专利权人 LOCKHEED MARTIN CORPORATION;

    申请/专利号US19960757855

  • 发明设计人 DON D. WINFREE;LOUIS G. HUNTER JR.;

    申请日1996-11-27

  • 分类号F02C5/02;

  • 国家 US

  • 入库时间 2022-08-22 02:07:34

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