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压气机轮盘简化结构强度的数值仿真分析
引用本文:付为刚,姚裕隆,裴少坤,陈俊杰.压气机轮盘简化结构强度的数值仿真分析[J].内燃机与配件,2021(6).
作者姓名:付为刚  姚裕隆  裴少坤  陈俊杰
作者单位:中国民用航空飞行学院航空工程学院
基金项目:中国民用航空飞行学院青年基金项目(XM2753)。
摘    要:背景:压气机轮盘是发动机的重要组件,工作环境的应力条件复杂,其结构性能对发动机工作将产生很大的影响。目的:针对发动机轮盘进行受力分析,有利于进行轮盘结构优化设计,进而提高发动机推重比。方法:本文采用理论分析与有限元仿真相结合,基于对称假设下的轮盘简化结构强度给出径向与周向最大应力的理论解。同时,运用有限元软件ANSYS获得对应的数值仿真解。结论:经理论解与仿真解对比分析表明,本文提供的方法可用于压气机轮盘简化结构强度的求解分析。

关 键 词:压气机轮盘  强度  数值仿真  有限元法

Numerical Simulation on Simplified Structural Strength of Engine Compressor Disk
FU Wei-gang,YAO Yu-long,PEI Shao-kun,CHEN Jun-jie.Numerical Simulation on Simplified Structural Strength of Engine Compressor Disk[J].Internal Combustion Engine & Parts,2021(6).
Authors:FU Wei-gang  YAO Yu-long  PEI Shao-kun  CHEN Jun-jie
Affiliation:(Civil Aviation Flight University of China,Aviation Engineering Institute,Guanghan 618300,China)
Abstract:Background:the compressor disk is an important component of the engine,the stress condition of the working environment is complex,its structure and performance will have a great impact on the engine.The purpose of this paper is to analyze the force on the engine disk,which is conducive to the optimization design of the disk structure,and then improve the thrust-weight ratio of the engine.The method of this paper:in this paper,theoretical analysis and finite element simulation are combined,and the theoretical solutions of radial and circumferential maximum stress are given based on the simplified structural strength of the disk under the assumption of symmetry.At the same time,the corresponding numerical simulation solution is obtained by using the finite element software ANSYS.The conclusion of this paper:the comparison between theoretical solution and simulation solution shows that the method presented in this paper can be used to solve and analyze the simplified structure strength of compressor disk.
Keywords:compressor disk  strength  numerical simulation  finite element
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