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轮盘径向破裂转速计算方法分析及修正
引用本文:冯引利,何云,陈伟,刘红彬.轮盘径向破裂转速计算方法分析及修正[J].航空动力学报,2014,29(11):2729-2734.
作者姓名:冯引利  何云  陈伟  刘红彬
作者单位:南京航空航天大学 能源与动力学院, 南京 210016;中国航空工业集团公司 中国燃气涡轮研究院, 成都 610500;中国航空工业集团公司 中国燃气涡轮研究院, 成都 610500;南京航空航天大学 能源与动力学院, 南京 210016;中国航空工业集团公司 中国燃气涡轮研究院, 成都 610500
摘    要:分析了轮盘径向破裂转速理论计算方法及常用平均径向应力计算方法的含义及其特点.且依据理论计算方法的含义,提出了基于有限元计算结果的轮盘径向破裂转速计算修正方法.通过实例应用,证明了相对于理论方法计算结果,修正方法较常用平均径向应力方法计算精度更高,其计算精度由6.6%提高到0.5%以内,且修正方法较理论方法使用更方便、工程适用性更强.

关 键 词:轮盘  径向破裂转速  平均径向应力  修正方法  有限元
收稿时间:7/9/2013 12:00:00 AM

Analysis and correction of computational methods on disk radial burst speed
FENG Yin-li,HE Yun,CHEN Wei and LIU Hong-bin.Analysis and correction of computational methods on disk radial burst speed[J].Journal of Aerospace Power,2014,29(11):2729-2734.
Authors:FENG Yin-li  HE Yun  CHEN Wei and LIU Hong-bin
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;China Gas Turbine Establishment, Aviation Industry Corporation of China, Chengdu 610500, China;China Gas Turbine Establishment, Aviation Industry Corporation of China, Chengdu 610500, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;China Gas Turbine Establishment, Aviation Industry Corporation of China, Chengdu 610500, China
Abstract:The meanings and characteristics of theoretical computation method and average radial stress computation method for disk radial burst speed were analyzed. According to the meanings of theoretical computation method, the correction method for disk radial burst speed was put forward on the basd of finite element computational results. By application example, relative to theoretical method's computation result indicates that the correction method has higher calculation precision than the average radial stress method.The calculation precision is improved from 6.6% to less 0.5%. The correction method is more convenient and applicable than theoretical method.
Keywords:disk  radial burst speed  average radial stress  correction method  finite element
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