王宝坤,林山,张帅,唐震,李诗军.大涵道比涡扇发动机侧风试验方法研究[J].航空发动机,2020,46(1):70-74
大涵道比涡扇发动机侧风试验方法研究
Study on Crosswind Test Method of High Bypass Ratio Turbofan
  
DOI:
中文关键词:  侧风试验  大涵道比涡扇发动机  侧风风向  进气畸变  稳定性  航空发动机
英文关键词:crosswind test  high bypass ratio turbofan  crosswind direction  inlet distortion  stability  aeroengine
基金项目:航空动力基础研究项目资助
作者单位E-mail
王宝坤,林山,张帅,唐震,李诗军 中国航发沈阳发动机研究所沈阳110015 693659286@qq.com 
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中文摘要:
      侧风条件对大涵道比涡扇发动机性能稳定性有重要影响。为开展大涵道比涡扇发动机侧风试验,分析了侧风试验标准 要求及侧风发生装置的工作原理与调试标定方法,进行了大涵道比涡扇发动机侧风试验研究,制定了侧风试验数据分析方法。开发 了1 种用于模拟侧风环境的试验装置,并提出了1 种风速标定方法和开展侧风试验的程序。结果表明:该试验装置可有效实现航 空发动机侧风试验环境,该标定方法可得到侧风试验装置工作状态与试验所需风速之间的映射关系,具有重要的工程指导意义。
英文摘要:
      The crosswind conditions have an important influence on the performance stability of the high bypass ratio turbofan. In order to carry out the crosswind test of high bypass ratio turbofan,the requirements of crosswind test standard were analyzed. The working principle and debugging calibration method of the crosswind generator were studied. The study of the crosswind test of high bypass ratio turbofan was carried out and the data analysis method of crosswind test was developed. A test device for simulating crosswind environment was developed,and a method for calibrating the wind speed and a program for carrying out the crosswind test were put forward. The results show that the test device can effectively realize the aeroengine crosswind test environment,and the calibration method can obtain the mapping relation between the working state of the crosswind test device and the test wind speed required,and has the important engineering guiding significance.
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