σ*2=σep2(1+ACαER(Aσep2σ02)n-1) ]]> whereA=inelastic anisotropic correction term,; <math overflow="scroll"><mtable><mtr><mtd><mrow><mi>A</mi><mo>=</mo><mi /><mo>⁢</mo><mrow><mfrac><mn>1</mn><mn>2</mn></mfrac><mo>[</mo><mrow><msup><mrow><mi>F</mi><mo>⁡</mo><mrow><mo>(</mo><mrow><msub><mi>D</mi><mi>yy</mi></msub><mo>-</mo><msub><mi>D</mi><mi>zz</mi></msub></mrow><mo>)</mo></mrow></mrow><mn>2</mn></msup><mo>+</mo><msup><mrow><mi>G</mi><mo>⁡</mo><mrow><mo>(</mo><mrow><msub><mi>D</mi><mi>zz</mi></msub><mo>-</mo><msub><mi>D</mi><mi>xx</mi></msub></mrow><mo>)</mo></mrow></mrow><mn>2</mn></msup><mo>+</mo></mrow></mrow></mrow></mtd></mtr><mtr><mtd><mrow><mi /><mo>⁢</mo><mrow><mrow><mi>H</mi><mo>⁢</mo><msup><mrow><mo>(</mo><mrow><msub><mi>D</mi><mi>xx</mi></msub><mo>-</mo><msub><mi>D</mi><mi>yy</mi></msub></mrow><mo>)</mo></mrow><mn>2</mn></msup></mrow><mo>+</mo><mrow><mn>2</mn><mo>⁢</mo><mi>L</mi><mo>⁢</mo><mstyle><mspace width="0.3em" height="0.3ex" /></mstyle><mo>⁢</mo><msubsup><mi>D</mi><mi>yz</mi><mn>2</mn></msubsup></mrow><mo>+</mo><mrow><mn>2</mn><mo>⁢</mo><mstyle><mspace width="0.3em" height="0.3ex" /></mstyle><mo>⁢</mo><msubsup><mi>MD</mi><mrow><mi>z</mi><mo>⁢</mo><mstyle><mspace width="0.3em" height="0.3ex" /></mstyle><mo>⁢</mo><mi>x</mi></mrow><mn>2</mn></msubsup></mrow><mo>+</mo><mrow><mn>2</mn><mo>⁢</mo><mstyle><mspace width="0.3em" height="0.3ex" /></mstyle><mo>⁢</mo><msubsup><mi>ND</mi><mrow><mi>x</mi><mo>⁢</mo><mstyle><mspace width="0.3em" height="0.3ex" /></mstyle><mo>⁢</mo><mi>y</mi></mrow><mn>2</mn></msubsup></mrow></mrow><mo>]</mo></mrow></mtd></mtr></mtable></math>  where F, G, H, L, M and N are the Hill constants, C=elastic anisotropic correction term, C=DE−1D σ*=determined linear stress, σ ep=estimated inelastic stress, D=direction vector of the elastic and inelastic stresses E −1=inverse stiffness matrix, ER=reference stiffness, σ0=reference stress, and σ α, n=material constants. "/> Method of determining the elastoplastic behavior of components consisting of anisotropic material and use of the method
首页> 外国专利> Method of determining the elastoplastic behavior of components consisting of anisotropic material and use of the method

Method of determining the elastoplastic behavior of components consisting of anisotropic material and use of the method

机译:确定由各向异性材料组成的组件的弹塑性行为的方法和该方法的用途

摘要

A method of determining the elastoplastic behavior of components, in particular of gas turbine plants, at high temperatures. First of all, the linear-elastic behavior is determined and the inelastic behavior is taken into account on the basis of the linear-elastic results by using the Neuber rule, the anisotropic characteristics of the components, as occur in particular through the use of single-crystalline materials, are taken into account in a simple manner by using a modified anistropic Neuber rule in the form; <math overflow="scroll"><mrow><msup><mi>σ</mi><mrow><mo>*</mo><mn>2</mn></mrow></msup><mo>=</mo><mrow><msubsup><mi>σ</mi><mi>ep</mi><mn>2</mn></msubsup><mo>⁡</mo><mrow><mo>(</mo><mrow><mn>1</mn><mo>+</mo><mrow><mfrac><mrow><mi>A</mi><mo>⁢</mo><mstyle><mspace width="0.3em" height="0.3ex" /></mstyle></mrow><mi>C</mi></mfrac><mo>⁢</mo><mfrac><mi>α</mi><msub><mi>E</mi><mi>R</mi></msub></mfrac><mo>⁢</mo><msup><mrow><mo>(</mo><mfrac><mrow><mi>A</mi><mo>⁢</mo><mstyle><mspace width="0.3em" height="0.3ex" /></mstyle><mo>⁢</mo><msubsup><mi>σ</mi><mi>ep</mi><mn>2</mn></msubsup></mrow><msubsup><mi>σ</mi><mn>0</mn><mn>2</mn></msubsup></mfrac><mo>)</mo></mrow><mrow><mi>n</mi><mo>-</mo><mn>1</mn></mrow></msup></mrow></mrow><mo>)</mo></mrow></mrow></mrow></math> whereA=inelastic anisotropic correction term,; <math overflow="scroll"><mtable><mtr><mtd><mrow><mi>A</mi><mo>=</mo><mi /><mo>⁢</mo><mrow><mfrac><mn>1</mn><mn>2</mn></mfrac><mo>[</mo><mrow><msup><mrow><mi>F</mi><mo>⁡</mo><mrow><mo>(</mo><mrow><msub><mi>D</mi><mi>yy</mi></msub><mo>-</mo><msub><mi>D</mi><mi>zz</mi></msub></mrow><mo>)</mo></mrow></mrow><mn>2</mn></msup><mo>+</mo><msup><mrow><mi>G</mi><mo>⁡</mo><mrow><mo>(</mo><mrow><msub><mi>D</mi><mi>zz</mi></msub><mo>-</mo><msub><mi>D</mi><mi>xx</mi></msub></mrow><mo>)</mo></mrow></mrow><mn>2</mn></msup><mo>+</mo></mrow></mrow></mrow></mtd></mtr><mtr><mtd><mrow><mi /><mo>⁢</mo><mrow><mrow><mi>H</mi><mo>⁢</mo><msup><mrow><mo>(</mo><mrow><msub><mi>D</mi><mi>xx</mi></msub><mo>-</mo><msub><mi>D</mi><mi>yy</mi></msub></mrow><mo>)</mo></mrow><mn>2</mn></msup></mrow><mo>+</mo><mrow><mn>2</mn><mo>⁢</mo><mi>L</mi><mo>⁢</mo><mstyle><mspace width="0.3em" height="0.3ex" /></mstyle><mo>⁢</mo><msubsup><mi>D</mi><mi>yz</mi><mn>2</mn></msubsup></mrow><mo>+</mo><mrow><mn>2</mn><mo>⁢</mo><mstyle><mspace width="0.3em" height="0.3ex" /></mstyle><mo>⁢</mo><msubsup><mi>MD</mi><mrow><mi>z</mi><mo>⁢</mo><mstyle><mspace width="0.3em" height="0.3ex" /></mstyle><mo>⁢</mo><mi>x</mi></mrow><mn>2</mn></msubsup></mrow><mo>+</mo><mrow><mn>2</mn><mo>⁢</mo><mstyle><mspace width="0.3em" height="0.3ex" /></mstyle><mo>⁢</mo><msubsup><mi>ND</mi><mrow><mi>x</mi><mo>⁢</mo><mstyle><mspace width="0.3em" height="0.3ex" /></mstyle><mo>⁢</mo><mi>y</mi></mrow><mn>2</mn></msubsup></mrow></mrow><mo>]</mo></mrow></mtd></mtr></mtable></math>  where F, G, H, L, M and N are the Hill constants, C=elastic anisotropic correction term, C=DE−1D σ*=determined linear stress, σ ep=estimated inelastic stress, D=direction vector of the elastic and inelastic stresses E −1=inverse stiffness matrix, ER=reference stiffness, σ0=reference stress, and σ α, n=material constants.
机译:一种确定部件,特别是燃气轮机设备,在高温下的弹塑性行为的方法。首先,通过使用Neuber规则,尤其是通过使用单个零件而出现的部件的各向异性特性,在线弹性结果的基础上确定线弹性行为并考虑非弹性行为-通过使用以下形式的改进的各向异性Neuber规则,以简单的方式考虑晶体材料; <![CDATA [<数学溢出=“ scroll”> σ * 2 < / mrow> = σ ep 2 < mo>⁡ 1 + A C α E R A σ ep 2 < / msubsup> σ 0 2 n - 1 ]]> 哪里 A =非弹性各向异性校正项, ; <![CDATA [<数学溢出=“ scroll”> A = 1 2 [ < mi> F D yy - D zz < / mrow> 2 + G D zz - D xx 2 + < / mo> H D xx - D yy < / mrow> 2 + 2 L D yz 2 + 2 MD z x 2 + 2 ⁢< / mo> ND x y < / mi> 2 ] ]]> 其中F,G,H,L,M和N是希尔常数, C =弹性各向异性校正项,C = D E −1 D σ * =确定的线性应力, σ ep =估计的非弹性应力, D =弹性应力和非弹性应力的方向向量 E −1 =反刚度矩阵, E R =参考刚度, σ 0 =参考应力和σ α,n =材料常数。

著录项

  • 公开/公告号US7050912B2

    专利类型

  • 公开/公告日2006-05-23

    原文格式PDF

  • 申请/专利权人 OTTO BERNHARDI;ROLAND MUECKE;

    申请/专利号US20040935167

  • 发明设计人 OTTO BERNHARDI;ROLAND MUECKE;

    申请日2004-09-08

  • 分类号G01L1;G01L3;G01L5;G06F19;

  • 国家 US

  • 入库时间 2022-08-21 21:42:22

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