| 冲压发动机模型燃烧室低压燃烧性能试验 |
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| 引用本文： | 牛志刚,费立群,冯守义,何小民.冲压发动机模型燃烧室低压燃烧性能试验[J].推进技术,2011,32(4):509-511,524. |
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| 作者姓名： | 牛志刚 费立群 冯守义 何小民 |
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| 作者单位： | 1. 中国航天科工集团三十一研究所高超声速冲压发动机技术重点实验室,北京100074／中国航天科工集团三十一研究所,北京100074
2. 南京航空航天大学能源与动力学院,江苏南京,210016 |
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| 摘 要： | 低压不利于燃烧,从化学动力学角度分析,压力降低导致空气密度降低,化学反应速率降低。用冲压发动机模型燃烧室进行了低压燃烧试验,结果显示：进口压力pin从0.094 MPa变至0.065 MPa,燃烧效率由大变小;压力降低到0.065 MPa时,燃烧室燃烧性能急剧恶化,燃烧极不稳定,随时可能因压力波动或油气参数变化而熄火。无传焰槽时燃烧效率随压力的变化规律与有传焰槽的一致,但燃烧效率相对低一些。
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| 关 键 词： | 冲压喷气发动机 燃烧室 低压 |
| 收稿时间： | 2011/1/20 0:00:00 |
| 修稿时间： | 2011/6/19 0:00:00 |
Experiment on combustion performance of a ramjet prototype combustor in low pressure condition |
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| NIU Zhi-gang,FEI Li-qun,FENG Shou-yi and HE Xiao-min.Experiment on combustion performance of a ramjet prototype combustor in low pressure condition[J].Journal of Propulsion Technology,2011,32(4):509-511,524. |
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| Authors: | NIU Zhi-gang FEI Li-qun FENG Shou-yi and HE Xiao-min |
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| Institution: | NIU Zhi-gang1.2,FEI Li-qun1,2,FENG Shou-yi1,HE Xiao-min3(1.Science and Technology on Scramjet Lab.,The 31st Research Inst.of CASIC,Beijing 100074,China,2.The 31st Research Institute of CASIC,3.Coll.of Energy and Power,Nanjing Univ.of Aeronautics and Astronautics,Nanjing 210016,China) |
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| Abstract: | Low pressure is an adverse condition for combustion.On the basis of chemical dynamics,decreasing pressure leads to decreasing density of air and decreasing rate of chemical reaction.Experiments in a ram jet prototype combustor were carried out.The results demonstrated that while the inlet pressure of the combustor pin varied from 0.094 to 0.065MPa,the combustion efficiency decreased;when the pressure pin decreased to 0.065MPa,the combustor performance deteriorated rapidly,and the combustion became so unstea... |
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| Keywords: | Combustion chamber Ramjet engine Low pressure |
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