| 中国大涵道比涡扇发动机整机试验验证规划研究 |
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| 引用本文： | 王海.中国大涵道比涡扇发动机整机试验验证规划研究[J].航空发动机,2019,45(6):97-102. |
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| 作者姓名： | 王海 |
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| 作者单位： | 中国人民解放军93128部队,北京,100076 |
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| 基金项目： | 国防工程重点研究项目资助 |
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| 摘 要： | 为满足中国军用运输机和民用大飞机用大涵道比涡扇发动机的研制需求,加速提升中国试验技术能力,根据国外先进大涵道比涡扇发动机整机试验取得的成果,分析并明确了大涵道比涡扇发动机整机试验验证依据,制定了未来中国大涵道比涡扇发动机整机试验验证规划,系统地论证了不同类别整机试验的关注点,总结了中国开展大涵道比涡扇发动机整机试验需突破的关键技术,为开展其整机试验理清思路。
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| 关 键 词： | 大涵道比涡扇发动机 整机试验 验证规划 关键技术 |
Demonstration Program Study of Overall Engine Test on High Bypass Ratio Turbofan Engine in China |
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| Authors: | WANG Hai |
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| Affiliation: | PLA 93128 Unit, Beijing 100076, China |
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| Abstract: | In order to meet the development demand of high bypass ratio turbofan engine for Chinese military transport aircraft and
civil large aircraft, and to accelerate and improve the test technical ability in China, the test demonstration basis of high bypass ratio
turbofan engine was analyzed and clarified according to the test results of foreign advanced high bypass ratio turbofan engine. The
demonstration program of overall engine test of the high bypass ratio turbofan engine in the future was set up. The focus of different kinds of
overall engine test was demonstrated systematically. The key technologies needed to break through of overall engine test of the high bypass
ratio turbofan engine in China was summarized, and the train of thought for the overall engine test was put forward. |
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