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某型涡扇发动机进口温度畸变的稳定性评定试验技术研究

Stability Assessment Test Technology of a Turbofan Engine Inlet Temperature Distortion

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【作者】 张天飞叶巍陆德雨赵晓斌王进

【Author】 ZHANG Tian-fei~1,YE Wei~2,LU De-yu~2,ZHAO Xiao-bin~3,WANG-Jin~3(1.Beijing Institute of Technology,Beijing100081,China;2.China Gas Turbine Establishment,Chengdu610500,China;3.Air Force Eighth Research Institute, Beijing100076,China)

【机构】 北京理工大学机电工程学院中国燃气涡轮研究院空军第八研究所空军第八研究所 北京100081四川成都610500北京100076北京100076

【摘要】 介绍了温度畸变发生器的组成及工作原理。通过开展某型涡扇发动机与温度畸变发生器的联合畸变试验,确定了发动机各工作状态下的临界热扰动值,获得了该型发动机的温度畸变敏感系数,建立了适用于工程实际的发动机温度畸变方法。试验证明,温度畸变发生器的建立是成功的,是全面开展发动机稳定性评定的有力工具,对我国制定航空发动机进口温度畸变规范有重要意义。

【Abstract】 This paper discusses the constitution and principle of temperature distortion generator.Based on the inlet temperature distortion experiments of a turbofan-engine,the critical thermal agitation values under each engine operating condition were ascertained,the distortion sensitivity coefficients of the engine were determined,and a practical technical aero-engine stability assessment method for inlet temperature distortion was presented.It is proved that the temperature distortion generator is a useful tool for aero-engine stability assessment.The successful development of a temperature distortion generator will have significant effects on the formulating of our country’s assessment criterion of aero-engine inlet temperature distortion.

  • 【文献出处】 航空动力学报 ,Journal of Aerospace Power , 编辑部邮箱 ,2003年06期
  • 【分类号】V235
  • 【被引频次】2
  • 【下载频次】171
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