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涡轴发动机动力涡轮转子高速动平衡技术研究
引用本文:邓旺群,高德平.涡轴发动机动力涡轮转子高速动平衡技术研究[J].航空动力学报,2003,18(5):669-675.
作者姓名:邓旺群  高德平
作者单位:南京航空航天大学能源与动力学院,江苏南京210016
基金项目:国家航空预研资助项目(24.8.3)
摘    要:针对动力涡轮转子空心、薄壁、大长径比、带弹性支承和挤压油膜阻尼器、内置测扭基准轴的结构特点,提出了一种改进的"多转速、多平面、分步平衡"的方法,设计了一组精密平衡卡箍,建立了一套涡轴发动机动力涡轮转子高速动平衡的平衡步骤和平衡工艺,给出了动力涡轮转子的平衡判定准则,在全转速范围内进行了动力涡轮转子的高速动平衡,最高平衡转速大于20,000r/min。所建立的平衡方法和工艺已应用于某型涡轴发动机动力涡轮转子的高速动平衡,效果良好。 

关 键 词:航空、航天推进系统    涡轴发动机    高速动平衡    动力涡轮转子    平衡卡箍    弯曲临界转速
文章编号:1000-8055(2003)05-0669-07
收稿时间:2002/11/18 0:00:00
修稿时间:2002年11月18

High Speed Dynamic Balance Technique of a Power Turbine Rotor of a Turbine Shaft Engine
DENG Wang qun and GAO De ping.High Speed Dynamic Balance Technique of a Power Turbine Rotor of a Turbine Shaft Engine[J].Journal of Aerospace Power,2003,18(5):669-675.
Authors:DENG Wang qun and GAO De ping
Institution:Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
Abstract:High speed dynamic balance of power turbine rotor which generally runs over the second bending critical speed is a key technique in developing turbine shaft engine.This paper presents an improved multispeed,multiplane and step by step balance precedure developed to balance a power turbine rotor with a long slender hollow shaft,elastic supports and squeeze film dampers,and inherent torque tube.A group of precise balance collars are designed for adding trial masses.A set of balance steps and balance technologies are summarized.Criteria for evaluating the quality are established which involve the limits of both vibration displacement of shaft and vibration acceleration of supports.The procedure is carried out throughout the whole operating speed range and the highest balance speed is over 20,000 rpm.It has been successfully applied to balancing the power turbine rotor in practice.
Keywords:aerospace propulsion system  turbine shaft engine  high speed dynamic balance  power turbine rotor  balance collar  bending critical speed  
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