σ*2=σep2+σep2⁢D_·E——ER·D_⁢ ⁢σv*2σ*2⁢ ⁢α⁡(σep2σ02⁢ ⁢σv*2σ*2)n-1 ]]>;where; &sgr;*=determined linear stress,;&sgr;*v=determined linear Hill's comparative stress,; &sgr; ep=estimated inelastic stress,; D=directional vector of the elastic and inelastic stresses,; E −1=inverse stiffness matrix;ER=reference stiffness,;&sgr;0=reference stress, and;&agr;,n=constant."/> Method for determining the elasto-plastic behavior of components consisting of anisotropic material, and application of the process
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Method for determining the elasto-plastic behavior of components consisting of anisotropic material, and application of the process

机译:确定由各向异性材料组成的部件的弹塑性行为的方法及其应用

摘要

In a method for determining the elasto-plastic behavior of components consisting of anisotropic material, in particular of gas turbine installations, at high temperatures, in which method, first of all, the linear-elastic behavior is determined and, on the basis of the linear-elastic results, the inelastic behavior is also taken into account by applying Neuber's rule, the anisotropic properties of the components, as occur in particular on account of the use of single crystal materials, are taken into account in a simple manner by using a modified anisotropic Neuber's rule of the form <math><mrow><msup><mi>&amp;sigma;</mi><mrow><mo>*</mo><mn>2</mn></mrow></msup><mo>=</mo><mrow><msubsup><mi>&amp;sigma;</mi><mi>ep</mi><mn>2</mn></msubsup><mo>+</mo><mrow><msubsup><mi>&amp;sigma;</mi><mi>ep</mi><mn>2</mn></msubsup><mo>&amp;it;</mo><mrow><munder><mi>D</mi><mi>_</mi></munder><mo>&amp;CenterDot;</mo><mfrac><munder><munder><mi>E</mi><mi>&amp;mdash;</mi></munder><mi>&amp;mdash;</mi></munder><msub><mi>E</mi><mi>R</mi></msub></mfrac><mo>&amp;CenterDot;</mo><munder><mi>D</mi><mi>_</mi></munder></mrow><mo>&amp;it;</mo><mstyle><mtext>&amp;emsp;</mtext></mstyle><mo>&amp;it;</mo><mfrac><msubsup><mi>&amp;sigma;</mi><mi>v</mi><mrow><mo>*</mo><mn>2</mn></mrow></msubsup><msup><mi>&amp;sigma;</mi><mrow><mo>*</mo><mn>2</mn></mrow></msup></mfrac><mo>&amp;it;</mo><mstyle><mtext>&amp;emsp;</mtext></mstyle><mo>&amp;it;</mo><msup><mrow><mi>&amp;alpha;</mi><mo>&amp;af;</mo><mrow><mo>(</mo><mrow><mfrac><msubsup><mi>&amp;sigma;</mi><mi>ep</mi><mn>2</mn></msubsup><msubsup><mi>&amp;sigma;</mi><mn>0</mn><mn>2</mn></msubsup></mfrac><mo>&amp;it;</mo><mstyle><mtext>&amp;emsp;</mtext></mstyle><mo>&amp;it;</mo><mfrac><msubsup><mi>&amp;sigma;</mi><mi>v</mi><mrow><mo>*</mo><mn>2</mn></mrow></msubsup><msup><mi>&amp;sigma;</mi><mrow><mo>*</mo><mn>2</mn></mrow></msup></mfrac></mrow><mo>)</mo></mrow></mrow><mrow><mi>n</mi><mo>-</mo><mn>1</mn></mrow></msup></mrow></mrow></mrow></math> ;where; &sgr;*&equals;determined linear stress,;&sgr;*v&equals;determined linear Hill's comparative stress,; &sgr; ep&equals;estimated inelastic stress,; D&equals;directional vector of the elastic and inelastic stresses,; E &minus;1&equals;inverse stiffness matrix;ER&equals;reference stiffness,;&sgr;0&equals;reference stress, and;&agr;,n&equals;constant.
机译:在一种用于确定由各向异性的材料,尤其是燃气轮机设备组成的部件在高温下的弹塑性行为的方法中,首先确定线性弹性行为,并在此基础上确定线性弹性行为。线性弹性结果,还可以通过应用Neuber规则来考虑非弹性行为,特别是通过使用单晶材料来考虑组件的各向异性特性,方法是使用格式为 <![CDATA [ &sigma; * 2 = &sigma; ep 2 + 和sigma; ep 2 &it; < > D _ &CenterDot; E &mdash; &mdash; E R < / mfrac> &CenterDot; D _ &it; &emsp; &it; &sigma; v < mo> * 2 &sigma; * 2 &it; &emsp; &it; &alpha; &af; &sigma; < / mi> ep 2 &sigma; 0 2 &it; &emsp; &it; < mi>&sigma; v * 2 &sigma ; * 2 n - 1 ]]> ;其中; &sgr; *等于确定的线性应力;&sgr; * v 等于确定的线性Hill的比较应力, &sgr; ep &equals;估计的非弹性应力, D 等于弹性和非弹性应力的方向向量, E &minus; 1 &equals;逆刚度矩阵; E R &equals;参考刚度;;&sgr; 0 &equals;参考应力和;&agr; ,n等于常数。

著录项

  • 公开/公告号US6715364B2

    专利类型

  • 公开/公告日2004-04-06

    原文格式PDF

  • 申请/专利权人 ALSTOM TECHNOLOGY LTD;

    申请/专利号US20020119937

  • 发明设计人 OTTO BERNHARDI;ROLAND MUECKE;

    申请日2002-04-11

  • 分类号G01D70/20;

  • 国家 US

  • 入库时间 2022-08-21 23:13:00

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