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Microstructure and Texture Variations in High Temperature Titanium Alloy Ti65 Sheets with Different Rolling Modes and Heat Treatments

机译:不同轧制方式和热处理的高温钛合金Ti65板材的组织和织构变化

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摘要

Ti65 alloy (Ti-5.8Al-4.0Sn-3.5Zr-0.5Mo-0.4Si-0.3Nb-1.0Ta-0.8W-0.05C) is the newly developed high temperature titanium alloy optimized from Ti60 alloys. The long-term service temperature of the alloy is as high as 650 °C, which is unattainable with the previous high temperature titanium alloy. It has excellent strength and excellent creep resistance, and has great application prospects in the aerospace industry. In the current study, the evolution of microstructure and texture of Ti65 alloy sheets developed by unidirectional rolling (UDR) and cross rolling (CR) followed by solution and aging treatment was investigated. The microstructure of the UDR sample consists of equiaxed , lamellar and few elongated , and the texture is the combination of minor B-type and major T-type texture, with the main component of basal {0001} fiber texture and , respectively. Due to more active slip system resulted by transformed direction, the microstructure of the CR sample consists of more elongated , and the <0001> texture characterized as R-type texture forms in addition to B/T-type texture. With aging temperature increasing, the microstructures for both transform to duplex microstructure, and the thicknesses of lamellar increase. B-type texture becomes stronger, while T/R-type texture are weakened, which is caused by the combination of recrystallization, spheroidization, and variant selection. An abnormal increasing of T/R-type texture but constant B-type texture happens in the CR-600 sample, which is related to high recrystallization fraction. It is expected that the research results can provide useful references for the rolling of high temperature titanium alloy sheets and the precise control of microstructure/texture.
机译:Ti65合金(Ti-5.8Al-4.0Sn-3.5Zr-0.5Mo-0.4Si-0.3Nb-1.0Ta-0.8W-0.05C)是从Ti60合金优化而来的最新开发的高温钛合金。合金的长期使用温度高达650°C,这是以前的高温钛合金无法达到的。它具有优异的强度和优异的抗蠕变性,在航空航天工业中具有广阔的应用前景。在当前的研究中,研究了通过单向轧制(UDR)和交叉轧制(CR)然后固溶和时效处理发展的Ti65合金薄板的组织和织构演变。 UDR样品的微观结构由等轴,层状和少量拉长组成,织构是次要B型织构和主要T型织构的结合,主要成分是基础{0001}纤维织构和。由于方向转变导致滑动系统更加活跃,因此CR样品的微观结构由更多的拉长组成,除B / T型织构外,<0001>织构为R型织构。随着时效温度的升高,两者的微观结构均转变为双相微观结构,且层状厚度增加。 B型织构变强,而T / R型织构变弱,这是由于重结晶,球化和变体选择的组合所致。 CR / 600样品中出现T / R型织构异常增加而B型织构不变的现象,这与高再结晶率有关。预期该研究结果可为高温钛合金薄板的轧制和组织/组织的精确控制提供有用的参考。

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