| 气动谐振管点火技术研究 |
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| 引用本文： | 梁国柱,马彬,张国舟,程显辰,张振鹏.气动谐振管点火技术研究[J].推进技术,2001,22(4):286-289. |
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| 作者姓名： | 梁国柱 马彬 张国舟 程显辰 张振鹏 |
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| 作者单位： | 北京航空航天大学宇航学院 |
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| 基金项目： | 国家"八六三”基金资助项目(863-2-3-4-7). |
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| 摘 要： | 为了发展液体火箭发动机的气动谐振管非电点火新技术,提出了一种新颖的组合喷嘴混气谐振加热方案,并介绍了所研制的氦气谐振热表面点火器和同轴氢氧谐振火炬点火器,给出了气动谐振管点火器工程设计的一般原则和相关参数的选择。
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| 关 键 词： | 液体推进剂 火箭发动机 点火系统 气动谐振管 非电点火技术 氦气谐振热表面点火器 同轴氢氧谐振火炬点火器 气动参数 |
| 文章编号： | 1001-4055(2001)04-0286-04 |
| 修稿时间： | 2000年12月14 |
Investigation on gas dynamic resonance tube ignition method |
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| Liang Guozhu,Ma Bing,Zhang GuoZhou,Cheng XianChen and Zhang zhengPeng.Investigation on gas dynamic resonance tube ignition method[J].Journal of Propulsion Technology,2001,22(4):286-289. |
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| Authors: | Liang Guozhu Ma Bing Zhang GuoZhou Cheng XianChen and Zhang zhengPeng |
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| Institution: | School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083;School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083;School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083;School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083;School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083 |
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| Abstract: | To develop the new technology of gas dynamic resonance tube non electric ignition for liquid rocket engines,a new conceptual scheme of combined nozzle mixing gas resonance heating was proposed. The gaseous helium resonance surface heating igniter and the co axial gaseous oxygen hydrogen resonance torch igniter were described. And the general engineering design criteria for the resonance tube igniter were proposed. |
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| Keywords: | Liquid propellant rocket engine Ignition Ignition system Aerodynamic heating |
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