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Creep Properties of Directionally Solidified Ti-46Al-1.5Mo-0.2C Alloys Using a Seeding Technique

机译:定向晶种定向凝固Ti-46Al-1.5Mo-0.2C合金的蠕变性能

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摘要

Creep properties of directionally solidified Ti-46Al-1.5Mo-0.2C alloys with well aligned lamellar microstructure have been dramatically improved. The ingots were manufactured by seeding technique directional solidification. Directionally solidified Ti-46Al-1.5Mo-0.2C alloys showed excellent creep properties. However, the creep resistance decreased as the angle between lamellar orientation and loading axis increased. It is found that the control of the lamellar orientation is most important to improve the creep resistance of TiAl alloys. In the results of TEM analysis of creep specimen before and after creep test, it was found that no carbides were formed before creep test. But, after creep test, carbides were formed in gamma lath, gamma / gamma interfaces, gamma / alpha_2 interfaces and dislocations. In the case of creep test at 750 deg C, the quantity of carbides found in dislocations decreased as the load level increased. It was thought that superior thermal stability of Ti-46Al-1.5Mo-0.2C alloy suppressed the dynamic recrystallization and the coarsening of the lamellar microstructure, and the excellent creep resistance was maintained for long time due to this thermal stability.
机译:具有良好排列的层状微结构的定向凝固Ti-46Al-1.5Mo-0.2C合金的蠕变性能已得到显着改善。通过定向凝固的晶种技术制造铸锭。定向凝固的Ti-46Al-1.5Mo-0.2C合金表现出优异的蠕变性能。但是,随着层状取向和加载轴之间的夹角增加,抗蠕变性降低。发现层状取向的控制对于提高TiAl合金的抗蠕变性最重要。在蠕变试验之前和之后的蠕变样品的TEM分析结果中,发现蠕变试验之前没有形成碳化物。但是,经过蠕变测试后,在伽马板条,伽马/伽马界面,伽马/α_2界面和位错中形成了碳化物。在750摄氏度下进行蠕变测试的情况下,位错中发现的碳化物数量随负载水平的增加而减少。认为Ti-46Al-1.5Mo-0.2C合金的优异的热稳定性抑制了动态再结晶和层状组织的粗化,并且由于该热稳定性而长时间保持了优异的耐蠕变性。

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