首页|TiAl合金高温疲劳裂纹扩展表征及力学行为研究

TiAl合金高温疲劳裂纹扩展表征及力学行为研究

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鉴于TiAl合金在负应力比条件下的裂纹扩展试验数据缺失,本研究旨在丰富其力学性能数据库.为此,特地设计了一种适用于TiAl合金负应力比裂纹扩展试验的中心拉伸试样,同时开发了 1200℃高温疲劳板材加热炉,以及采用直流电位法测量疲劳裂纹长度的试验技术.通过疲劳试验机对试样进行加载,结合直流电位法,成功获取了TiAl合金在 600、800℃下的负应力比疲劳裂纹扩展数据.实验结果揭示,TiAl合金的疲劳裂纹扩展速率随试验温度的升高而加快;在相同的温度和应力强度因子幅度下,应力比的提高同样加速TiAl合金的疲劳裂纹扩展.进一步观察TiAl合金的断口形貌,呈现出典型的解理特征.
Study on High Temperature Fatigue Crack Propagation and Mechanical Behavior of TiAl Alloy
The aim of this study is to enrich the mechanical properties database of TiAl alloy due to the lack of crack propagation test data under negative stress ratio.Therefore,a central tensile specimen suitable for the negative stress ratio crack propagation test of TiAl alloy was designed.At the same time,a 1200℃ high temperature fatigue plate heating furnace was developed,and a test technique for measuring fatigue crack length by DC potential method was developed.The fatigue crack propagation data of TiAl alloy at 600 ℃ and 800 ℃ were successfully obtained by loading specimens by fatigue testing machine,combined with DC potential method.The experimental results show that the fatigue crack propagation rate of TiAl alloy increases with the increase of test temperature.At the same temperature and stress intensity factor amplitude,the increase of stress ratio also accelerates the fatigue crack propagation of TiAl alloy.The fracture morphology of TiAl alloy was further observed,showing typical cleavage characteristics.

TiAl alloycrack propagationhigh temperaturedirect current potential method

王亮、刘帅、陈新、杨洋

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航空材料检测与评价北京市重点试验室,北京 100095

材料检测与评价航空科技重点试验室,北京 100095

中国航空发动机集团材料检测与评价重点试验室,北京 100095

先进高温结构材料重点试验室,北京 100095

中国航发北京航空材料研究院,北京 100095

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TiAl合金 裂纹扩展 高温 直流电位法

2024

失效分析与预防
南昌航空大学 北京航空材料研究院

失效分析与预防

影响因子:0.352
ISSN:1673-6214
年,卷(期):2024.19(6)