| 推重比15一级发动机关键技术及分析 |
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| 引用本文： | 王占学,刘增文,蔡元虎,李斌.推重比15一级发动机关键技术及分析[J].航空发动机,2010,36(1):58-62. |
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| 作者姓名： | 王占学 刘增文 蔡元虎 李斌 |
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| 作者单位： | 1. 西北工业大学动力与能源学院,西安,710072
2. 沈阳发动机设计研究所,沈阳,110015 |
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| 摘 要： | 全面阐述和分析了推重比15一级涡扇发动机总体、风扇和压气机、燃烧室、涡轮、加力燃烧室、喷管等设计技术。
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| 关 键 词： | 航空发动机 高推重比 设计 |
1. School of Engine and Energy, Northwestern Polytechnical University, Xl'an 710072, China;2.Shenyang Aeroengine Research Institute, Shenyang 110015, China |
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| Authors: | WANG Zhan-xueI LIU Zeng-wen CAI Yuan-huj LI Bin |
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| Institution: | 1. School of Engine and Energy, Northwestern Polytechnical Umversity, Xi＇an 710072, China;2. Shenyang Aeroengine Research Institute, Shenyang 110015, China) |
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| Abstract: | The design technologies for general, fan, compressor, combustor, turbine, afterburner and nozzle of turbofan engine with thrust to weight ratio up to level of 15 were entirely illustrated and analyzed. |
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| Keywords: | aeroengine high thrust to weight ratio design |
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