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
中国大涵道比涡扇发动机整机试验验证规划研究
Demonstration Program Study of Overall Engine Test on High Bypass Ratio Turbofan Engine in China
  
DOI:
中文关键词:  大涵道比涡扇发动机  整机试验  验证规划  关键技术
英文关键词:high bypass ratio turbofan engine  overall engine test  demonstration program  key technologies
基金项目:国防工程重点研究项目资助
作者单位E-mail
王海 中国人民解放军93128 部队北京100076 ymhh2001@163.com 
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中文摘要:
      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。
英文摘要:
      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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