| 小型涡轮发动机红外隐身技术 |
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| 引用本文： | 李俊萍,刘永远,关胜如,等.小型涡轮发动机红外隐身技术[J].战术导弹技术,2014(3):90-94,109. |
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| 作者姓名： | 李俊萍 刘永远 关胜如 等 |
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| 作者单位： | [1]北京动力机械研究所,北京100074; [2]空军驻京丰地区军事代表室,北京100074 |
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| 摘 要： | 对红外隐身技术在小型涡轮发动机上的可行性进行了分析,适合小型涡轮发动机红外隐身技术有:采用涡扇发动机、异型喷管、壁面冷却技术等。对小型涡轮发动机红外隐身设计需要突破的低损失高效掺混技术、壁面冷却设计技术、红外隐身效能评估等技术进行了论述,以实现集气动、红外、结构一体化隐身喷管设计。最后对小型涡轮发动机红外隐身技术发展趋势进行了阐述。
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| 关 键 词： | 涡轮发动机 红外隐身技术 一体化隐身设计 |
Infrared Stealth Technology of the Small Turbine Engine |
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| Affiliation: | Li Junpm , Liu Yongyuan, Guan Shengru , Xu Lingzhi , Wang Hanquan ( Beijing Power Machinery Institute, Beijing 100074, China; Air Force Military Representative Office in Beijing Fengtai Region, Beijing 100074, China) |
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| Abstract: | The feasibility of infrared stealth technology in small turbine engine are analyzed. Infrared stealth technology suitable for small turbine engine include the turbofan engine, special shaped nozzle and wall cooling technology. The small turbine engine infrared stealth design need to improve the low loss high efficient mixing technology, wall cooling design technology, infrared stealth technology of effective- ness evaluation, and realize the set of pneumatic, infrared, structure integration stealth nozzle design. Fi- nally the development trend of infrared stealth technology is elaborated. |
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| Keywords: | turbine engine infrared stealth technology integration stealth design |
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