高压涡轮盘的热弹性应力分析

THE THERMAL-ELASTIC STRESS ANALYSIS OF HIGH PRESSURE TURBINE PLATE

  • 摘要: 本文利用大型通用有限元程序ALGOR某型发动机的高压涡轮盘及其榫齿进行了三维热弹性应力分析,对如何处理轮盘和叶片之间的连接进行了研究,并在有限元计算中应用了边界元法,从而得到了盘及榫齿的热弹性应力分布,并已应用于实际的发动机结构设计中。

     

    Abstract: ALGOR. a familiar finite element program, was employed to conduct three-dimesion thermal-elastic stress analysis of an engine's high pressure turbine polate and its tenon tooth The thermal-elastic stress distributions of plate and its tenon tooth were obtained and applied to the design of the engine . Boundary elements were used when calculating.

     

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