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Fatigue crack propagation in single crystal CMSX-2 at elevated temperature.

机译:高温下单晶CMSX-2中的疲劳裂纹扩展。

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摘要

Fatigue Crack Propagation (FCP) tests were carried out on single crystal CMSX-2 as part of an investigation of the mechanisms of crack advance under conditions of fatigue loading in modern Ni-base superalloys intended for use in single crystal form. FCP tests were conducted at two temperatures, 25C and 700C, two environments, (laboratory air and high vacuum) and two crystallographic orientations. The morphology of the fracture surfaces was examined using scanning electron microscopy (SEM). Two primary modes of cracking were observed crystallographic crack propagation and gamma prime precipitate avoidance. Those areas of the crack surface associated with precipitate avoidance showed a 'wavy' morphology associated with the residual dendritic macrostructure. Increasing temperature was shown to decrease the amount of crystallographic cracking. Tests conducted at high temperature in laboratory air showed less crystallographic crack growth than those tested in vacuum. Transmission electron microscopy (TEM) was used to characterize the deformation mechanisms associated with each mode of cracking. Dislocations were found to travel in well-defined slip bands which passed through both the matrix and the precipitates in those areas associated with crystallographic crack propagation. Dislocations were found to segregate to the channels of gamma matrix between the precipitates for those regions associated with gamma prime avoidance crack morphologies.A three dimensional finite element analysis (FEA) was used to determine the stress fields ahead of the crack tips for several crack morphologies. Those regions on the crack surface which exhibited crystallographic cracking were found to have high values of the shear stress resolved in the direction of the Burgers vector and low normal stresses to the plane containing the Burgers vector. Those regions which exhibited gamma prime precipitate avoidance cracking morphologies were found to have low values of the shear stress resolved in the direction of the Burgers vector and high normal stresses to the faces of the gamma prime precipitates. The decrease in the amount of crystallographic cracking at high temperature appeared to result from the increasing hardness of the gamma prime precipitates with increasing temperature.
机译:对单晶CMSX-2进行了疲劳裂纹扩展(FCP)测试,作为研究疲劳强度条件下打算用于单晶形式的现代镍基高温合金中裂纹扩展机制的一部分。 FCP测试是在25°C和700°C的两种温度,两种环境(实验室空气和高真空)和两种晶体学取向下进行的。使用扫描电子显微镜(SEM)检查断裂表面的形态。观察到裂纹的两种主要模式,即晶体学裂纹扩展和避免γ′沉淀。与避免析出有关的裂纹表面区域显示出与残余树枝状宏观结构有关的“波浪”形貌。显示出升高的温度减少了结晶裂纹的数量。与在真空中测试的结果相比,在实验室空气中高温下进行的测试显示出较少的晶体裂纹扩展。透射电子显微镜(TEM)用于表征与每种裂纹模式相关的变形机制。发现位错在明确的滑移带中传播,滑移带穿过基体和与晶体学裂纹扩展有关的区域中的沉淀物。对于那些与避免γ初生裂纹形态有关的区域,发现位错偏析在析出物之间的γ矩阵通道上。三维有限元分析(FEA)用于确定几种裂纹形态在裂纹尖端之前的应力场。 。发现在裂纹表面上表现出晶体学开裂的那些区域具有在Burgers矢量的方向上分解的高剪切应力值和对包含Burgers矢量的平面的低法向应力。发现那些表现出避免γ′初析的裂纹形态的区域在Burgers矢量的方向上具有较低的剪切应力值,而γ′初析的表面具有较高的法向应力。高温下结晶裂纹数量的减少似乎是由于随着温度升高而γ初生沉淀物的硬度增加所致。

著录项

  • 作者

    Antolovich, Bruce F.;

  • 作者单位

    Georgia Institute of Technology.;

  • 授予单位 Georgia Institute of Technology.;
  • 学科 Engineering Mechanical.Engineering Materials Science.Engineering Metallurgy.
  • 学位 Ph.D.
  • 年度 1993
  • 页码 159 p.
  • 总页数 159
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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