| 新型高密度燃料性能研究 |
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| 引用本文： | 叶丹阳,曹新发,韦伟.新型高密度燃料性能研究[J].火箭推进,2011,37(4):50-53. |
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| 作者姓名： | 叶丹阳 曹新发 韦伟 |
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| 作者单位： | 中国航天科技集团公司四院四十二所,湖北襄阳,441003 |
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| 摘 要： | 研究了新型高密度碳氢化合物HD-2与航空煤油的复配。通过对不同配比的燃料的密度、黏度、闪点、燃烧热值的测定比较，研究了复配燃料的基本性能；通过火箭一冲压组合发动机（RBCC）航空煤油点火燃烧性能实验，研究了不同HD-2添加含量的复配燃料的燃烧性能。基本性能测试实验和点火燃烧性能实验的结果表明：添加HD-2高密度碳氢化合...
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| 关 键 词： | HD-2 复配燃料 点火性能 发动机推力 |
Properties of new high-density fuel |
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| YE Dan-yang,CAO Xin-fa,WEI Wei.Properties of new high-density fuel[J].Journal of Rocket Propulsion,2011,37(4):50-53. |
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| Authors: | YE Dan-yang CAO Xin-fa WEI Wei |
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| Institution: | YE Dan-yang,CAO Xin-fa,WEI Wei(The 42nd Institute,the Fourth Academy,CASC,Xiangyang 441003,China) |
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| Abstract: | The formulation of new high-density hydrocarbon fuel HD-2 and aero kerosene(RP-3) is studied.Density,viscosity,flash point and combustive calorific value of the complex fuel were measured and compared.The ignition and combustion performances of complex fuels with different HD-2 ratio were investigated by performance experiments on RBCC engine.The results show that HD-2 can remarkably improve ignition and combustion properties of RP-3,and increase the thrust of RBCC engine. |
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| Keywords: | HD-2 complex fuel ignition performance engine propulsion |
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