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摘要:
Turbocharging is an efficient approach for addressing power reduction and oil consumption increase in aviation piston engines during high-altitude flights.However,a turbocharger significantly increases the complexity of a power system,and its considerably complex matching relation with the engine results in a coupling of failure modes.Conventional analytical methods are hard to identify failure-inducing factors.Consequently,safety issues are becoming increasingly prominent.This study focuses on methods for identifying failure-inducing factors.A whole-machine system model is established and validated through experimentation.The response surface method is employed to further abstract the system simulation model to a surrogate model (average error: ~3 %) in order to reduce the computational cost while ensuring accuracy.On this basis,an improved Correspondence Analysis (CA)-Polar Angle (PA)-based Classification (PAC) is proposed to identify the key factors affecting the failure mode of turbochargers.This identification method is based on the row profile coordinates G varying with the numerical deviations of the key factors,and is capable of effectively identifying the key factors affecting the failure.In a validation example,this method identifies the diameter of the exhaust valve (e2) as the primary factor affecting the safety margin for each work boundary.
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篇名 Identification of key factors affecting the failure of aviation piston engine turbochargers based on an improved correspondence analysis-polar angle-based classification
来源期刊 中国航空学报(英文版) 学科
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年,卷(期) 2021,(5) 所属期刊栏目
研究方向 页码范围 466-484
页数 19页 分类号
字数 语种 英文
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中国航空学报(英文版)
月刊
1000-9361
11-1732/V
大16开
北京学院路37号西小楼
80-675
1988
eng
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2997
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