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火焰筒局部蠕变屈曲分析方法
引用本文:洪杰,高金海,马艳红,王建军. 火焰筒局部蠕变屈曲分析方法[J]. 航空动力学报, 2010, 25(2): 388-395
作者姓名:洪杰  高金海  马艳红  王建军
作者单位:北京航空航天大学能源与动力工程学院,北京,100191;北京航空航天大学能源与动力工程学院,北京,100191;北京航空航天大学能源与动力工程学院,北京,100191;北京航空航天大学能源与动力工程学院,北京,100191
基金项目:新世纪优秀人才支持计划 
摘    要:准确考虑火焰筒温度场和应力场的局部特性,提出局部蠕变屈曲概念,并给出一套局部蠕变屈曲分析方法.基于Hoff理论建立蠕变屈曲理论模型,结合理论和试验数据验证有限元方法处理蠕变屈曲问题的可行性.考虑蠕变屈曲失稳要素,结合静力结果确定蠕变屈曲危险部位,将子模型技术引入非线性/热弹塑性/蠕变有限元程序中,结合曲率极大点判据,确定危险部位蠕变屈曲临界时间.方法将改善传统方法中的平均温度、平均压应力和平面应变假设,提高了计算精度. 

关 键 词:火焰筒  局部蠕变屈曲  有限元法  子模型技术  临界时间
收稿时间:2009-02-14
修稿时间:2009-06-09

Local creep buckling analysis method of combustor liner
HONG Jie,GAO Jin-hai,MA Yan-hong and WANG Jian-jun. Local creep buckling analysis method of combustor liner[J]. Journal of Aerospace Power, 2010, 25(2): 388-395
Authors:HONG Jie  GAO Jin-hai  MA Yan-hong  WANG Jian-jun
Affiliation:School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Abstract:In consideration of the local feature of combustor liner temperature field and stress field,a concept of local creep buckling was presented in this paper along with an engineering analysis method.Firstly,the theoretical model of creep buckling was established based on Hoff theory.Secondly,the feasibility of using finite element method(FEM) to analyze creep buckling was validated by theoretical and test data.Thirdly,a statics analysis with thermal-mechanical loads was performed,and then the dangerous place of combustor liner local creep buckling was captured considering creep buckling instability factors.Finally,sub-model technique was used in nonlinear thermal elastic-plastic/creep finite element analysis to capture the critical time of local creep buckling with curvature local maximum point criterion.It could be concluded that,as compared with traditional method,the hypothesis of average temperature,average compressive stress and plane strain could be improved in this paper,thus the computational accuracy was enhanced greatly.The work of this paper is significant on the application of structure design of combustor liner.
Keywords:combustor liner  local creep buckling  finite element method  sub-model technique  critical time
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