| 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： | 中国航空工业发展中心,北京,100029 |
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| 摘 要： | 围绕下一代窄体客机发动机，介绍了目前国外飞机和发动机生产商方案选择的一些思路，叙述了传统涡扇发动机、齿轮传动涡扇发动机和开式转子发动机的最新进展，预测了发展趋势。
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| 关 键 词： | 开式转子发动机 齿轮传动涡扇发动机 窄体客机 |
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: | HU Xiao-yu (Aviation Industries Development Research Center of China, Beijing100029, China) |
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| Abstract: | Some considerations of foreign aircrqft and engine manufactures on next generation narrow aircraft engine were presented. The latest developments of traditional turbofan engine, geared turbofan engine and open rotor engine are described. The development trend of next generation narrow aircraft engine was forecasted. |
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| Keywords: | open rotor engine geared turbofan engine narrow aircraft |
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