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1)  thermal fatigue
热疲劳
1.
Study of failure mode and failure mechanisms on thermal fatigue of plasma sprayed thermal barrier coatings;
等离子涂层热疲劳失效模式及失效机理研究
2.
Changes of morphology and composition of carbides in H13 steel after thermal fatigue;
H13钢热疲劳后碳化物形态和组分的变化
3.
Effect of heat treatment conditions on the thermal fatigue properties of WC/steel composites;
热处理条件对WC/钢复合材料热疲劳性能的影响
2)  heat fatigue
热疲劳
1.
Investigation of improvement of heat fatigue resistance of steel 3Cr24Ni7;
提高 3Cr24Ni7 钢热疲劳性的研究
2.
Three invalid patterns which resulted from the improper heat treatment were heat fatigue,thermal wear,two invalid patterns appeared concurrence,the invalid patterns were mainly studied,and the solved approaches were put forward.
重点研究了由于热处理不当引起的三种失效:热疲劳、热磨损、以及两者失效同时发生,并提出了解决的途径。
3.
The heat fatigue of the coat of supporting steel back of the powder metalurgical friction material and rotator material was studied in this article.
研究了粉末冶金摩擦材料及对偶材料支承钢背镀层的热疲劳行为。
3)  Hot Fatigue
热疲劳
1.
The propagation rules of hot fatigue of H13 used for die casting dies were studiedthrough simulating the work conditions of die casting dies.
依据模拟压铸铝合金模具的工作条件,研究了压铸模具钢H13的热疲劳裂纹的扩展规律。
4)  Creep-Fatigue/Thermal-Fatigue
蠕变疲劳/热疲劳
5)  cold-hot fatigue
冷热疲劳
1.
CoCrMoSi coating was deposited on CrZrCu with HVOF,and its cold-hot fatigue and war resistance were studied,analyzed and compared with NiCo plated coating widely applied in metallurgy industry.
采用光学显微镜、SEM及EDS等方法,对涂层的冷热疲劳性能和抗磨损性能进行了分析研究,并与当前冶金行业大量使用的电镀NiCo镀层进行对比。
2.
Co based alloy coating was deposited on the narrow side CrZrCu plate of the slab continuous caster with HVOF and the cold-hot fatigue was compared with Co-Ni plating coating.
结果表明:450℃下进行冷热疲劳试验,Co基合金涂层经过113次后,涂层还保持完好无损,未出现任何缺陷,而电镀镀层只能承受37。
6)  thermal fatigue
冷热疲劳
1.
Microstructure and thermal fatigue mechanical properties of cast cobalt-base su peralloy K640S were investigated during a number of recycles.
对铸造钴基高温合金K640S进行10次返回处理,研究了母合金和几种不同返回次数返回料的冷热疲劳性能,并进行了金相观察·结果表明:加热到815℃,然后水冷到25℃,保温5min,冷却5s,循环70次时,7返、10返合金首先出现微裂纹·随着循环次数的增加,返回料比新料疲劳裂纹生长快·循环200次时,无论新料还是返回料裂纹长度都达到2mm·随着返回次数的增加,合金中气体及夹杂物质量分数随之增加,枝晶组织越来越发达
补充资料:热疲劳
分子式:
CAS号:

性质:当容器或构件由于其温度的反复变化而引起其金属材料的疲劳现象称为热疲劳。

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