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An investigation of the failure mechanisms in high temperature materials subjected to isothermal and anisothermal fatigue and creep conditions

机译:等温,等温疲劳和蠕变条件下高温材料破坏机理的研究

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摘要

Many engineering components are subjected to conditions which have a detrimental effect on the materials from which they are made. Such components are used, for example, within high temperature regions of aeroengines (e.g. turbine discs) and power plant (e.g. steam pipes) and such conditions can include periods of isothermal and/or thermo-mechanical cyclic loading which may cause fatigue, excessive plasticity and creep. The combination of conditions to which the materials are subjected can have a strong influence on the failure mechanisms induced within the material.\ud\udThis study is concerned with the identification of the failure mechanisms which occur in RR1000 (a Nickel-based superalloy used in aeroengine turbine discs) tested under both isothermal and anisothermal cyclic conditions. The various types of test conditions applied to the specimens (e.g. waveforms which contain high temperature tensile conditions or alternatively low temperature tensile conditions) and the related failure mechanisms (e.g. intergranular, transgranular or mixed cracking), have been identified. Comparisons of the predictions of failure lives with experimental data from tested specimens, subjected to various test conditions, are also presented.
机译:许多工程组件所处的条件会对制造它们的材料产生不利影响。这样的部件例如在航空发动机(例如涡轮盘)和发电厂(例如蒸汽管)的高温区域内使用,并且这样的条件可能包括等温和/或热机械循环载荷,这可能会导致疲劳,过度可塑性和蠕变。材料所处的条件组合可能会对材料内部引起的失效机理产生强烈影响。\ ud \ ud本研究与RR1000(一种镍基高温合金,用于RR1000)中的失效机理的鉴定有关。航空发动机涡轮盘)在等温和等温循环条件下进行了测试。已经确定了施加到样品上的各种类型的测试条件(例如包含高温拉伸条件或低温拉伸条件的波形)和相关的破坏机理(例如晶间,晶间或混合裂纹)。还介绍了失效寿命的预测与来自经受各种测试条件的被测样品的实验数据的比较。

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