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Distributed collaborative extremum response surface method for mechanical dynamic assembly reliability analysis
  • ISSN号:1671-833X
  • 期刊名称:《航空制造技术》
  • 时间:0
  • 分类:O171[理学—数学;理学—基础数学] TB114.3[理学—概率论与数理统计;理学—数学;理学—应用数学;一般工业技术]
  • 作者机构:[1]School of Jet Propulsion, Beihang University, Beijing 100191, China
  • 相关基金:Project(51175017) supported by the National Natural Science Foundation of China; Project(YWF-12-RBYJ-008) supported by the Innovation Foundation of Beihang University for PhD Graduates, China; Proj ect(20111102110011) supported by the Research Fund for the Doctoral Program of Higher Education of China
中文摘要:

To make the dynamic assembly reliability analysis more effective for complex machinery of multi-object multi-discipline(MOMD),distributed collaborative extremum response surface method(DCERSM)was proposed based on extremum response surface method(ERSM).Firstly,the basic theories of the ERSM and DCERSM were investigated,and the strengths of DCERSM were proved theoretically.Secondly,the mathematical model of the DCERSM was established based upon extremum response surface function(ERSF).Finally,this model was applied to the reliability analysis of blade-tip radial running clearance(BTRRC)of an aeroengine high pressure turbine(HPT)to verify its advantages.The results show that the DCERSM can not only reshape the possibility of the reliability analysis for the complex turbo machinery,but also greatly improve the computational speed,save the computational time and improve the computational efficiency while keeping the accuracy.Thus,the DCERSM is verified to be feasible and effective in the dynamic assembly reliability(DAR)analysis of complex machinery.Moreover,this method offers an useful insight for designing and optimizing the dynamic reliability of complex machinery.

英文摘要:

To make the dynamic assembly reliability analysis more effective for complex machinery of multi-object multi-discipline (MOMD),distributed collaborative extremum response surface method (DCERSM) was proposed based on extremum response surface method (ERSM).Firstly,the basic theories of the ERSM and DCERSM were investigated,and the strengths of DCERSM were proved theoretically.Secondly,the mathematical model of the DCERSM was established based upon extremum response surface function (ERSF).Finally,this model was applied to the reliability analysis of blade-tip radial running clearance (BTRRC) of an aeroengine high pressure turbine (HPT) to verify its advantages.The results show that the DCERSM can not only reshape the possibility of the reliability analysis for the complex turbo machinery,but also greatly improve the computational speed,save the computational time and improve the computational efficiency while keeping the accuracy.Thus,the DCERSM is verified to be feasible and effective in the dynamic assembly reliability (DAR) analysis of complex machinery.Moreover,this method offers an useful insight for designing and optimizing the dynamic reliability of complex machinery.

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期刊信息
  • 《航空制造技术》
  • 中国科技核心期刊
  • 主管单位:中国航空工业集团公司
  • 主办单位:北京航空制造工程研究所
  • 主编:刘柱
  • 地址:北京市朝阳区八里桥北东军庄1号
  • 邮编:100024
  • 邮箱:lzm@amte.net.cn
  • 电话:010-85700465
  • 国际标准刊号:ISSN:1671-833X
  • 国内统一刊号:ISSN:11-4387/V
  • 邮发代号:82-26
  • 获奖情况:
  • 中文核心期刊,中国科技论文统计用刊,中国期刊方阵“双百”期刊
  • 国内外数据库收录:
  • 中国中国科技核心期刊,中国北大核心期刊(2011版)
  • 被引量:10629