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双转子发动机转差引起的叶片尾流激振
引用本文:赵福星,史海秋,杨兴宇.双转子发动机转差引起的叶片尾流激振[J].航空动力学报,2008,23(6):1098-1101.
作者姓名:赵福星  史海秋  杨兴宇
作者单位:北京航空工程技术研究中心,北京,100076
摘    要:介绍了双转子结构发动机在飞行使用中高、低压转子转速差随转速的变化特点,提出了转差可能在高、低压转子交界处的动叶间引起尾流激振的观点,并通过计算实例对转差引起的叶片尾流激振特点作了简要描述.与导向器的尾流激振比较,转差引起的叶片尾流激振有着易激起危险的低阶振型、共振转速范围宽和激振强度低的特点.

关 键 词:航空、航天推进系统  转差  尾流激振  双转子发动机
文章编号:1000-8055(2008)06-1098-04
收稿时间:2007/6/15 0:00:00
修稿时间:2007年6月15日

Blade wake excitation caused by twin-shaft engine speed difference
ZHAO Fu-xing,SHI Hai-qiu and YANG Xing-yu.Blade wake excitation caused by twin-shaft engine speed difference[J].Journal of Aerospace Power,2008,23(6):1098-1101.
Authors:ZHAO Fu-xing  SHI Hai-qiu and YANG Xing-yu
Institution:Beijing Aeronautical Technology Research Center, Beijing 100076, China;Beijing Aeronautical Technology Research Center, Beijing 100076, China;Beijing Aeronautical Technology Research Center, Beijing 100076, China
Abstract:This paper proposed the features of speed difference's change along with high pressure or low pressure rotor speed when twin-shaft engine was used in flight.A point of view was presented that speed difference is likely to arouse wake excitation between high pressure and low pressure rotor blade.The features of blade wake excitation caused by speed difference were briefly described through numerical examples.As compared with vane wake excitation,the blade wake excitation caused by speed difference features low stage vibration mode of high hazard exposure,wide resonance speed range and low excitation intensity.
Keywords:aerospace propulsion system  speed difference  wake excitation  twin-shaft engine
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