Ti60合金板材的室温强度与其显微组织和织构的关



Boyer R R.An overview on the use of titanium in the aerospace industry[J]. Mater. Sci. Eng., 1996, 213A: 103

DOI:10.1016/0921-5093(96)10233-1 URL

Titanium and titanium alloys are excellent candidates for aerospace applications owing to their high strength to weight ratio and excellent corrosion resistance. Titanium usage is, however, strongly limited by its higher cost relative to competing materials, primarily aluminum alloys and steels. Hence the advantages of using titanium must be balanced against this added cost. The titanium alloys used for aerospace applications, some of the characteristics of these alloys, the rationale for utilizing them, and some specific applications of different types of actual usage, and constraints, are discussed as an expansion of previous reviews of 尾 alloy applications. [1,2]

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[2]  

Banerjee D, Williams J C.Perspectives on titanium science and technology[J]. Acta Mater., 2013, 61: 844

DOI:10.1016/j.actamat.2012.10.043 URL

The basic framework and - conceptual understanding of the metallurgy of Ti alloys is strong and this has enabled the use of titanium and its alloys in safety-critical structures such as those in aircraft and aircraft engines. Nevertheless, a focus on cost-effectiveness and the compression of product development time by effectively integrating design with manufacturing in these applications, as well as those emerging in bioengineering, has driven research in recent decades towards a greater predictive capability through the use of computational materials engineering tools. Therefore this paper focuses on the complexity and variety of fundamental phenomena in this material system with a focus on phase transformations and mechanical behaviour in order to delineate the challenges that lie ahead in achieving these goals.

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王清江, 刘建荣, 杨锐. 高温钛合金的现状与前景[J]. 航空材料学报, 2014, 34(4): 1

Wang Q J, Liu J R, Yang R.High temperature titanium alloys: status and perspective[J]. J. Aeronaut. Mater., 2014, 34(4): 1

DOI:10.11868/j.issn.1005-5053.2014.4.001 Magsci

简要回顾国内外固溶强化型高温钛合金材料的发展历史,分析英、美、俄等国的高温钛合金研究与应用情况及发展趋势。介绍国内自主研制、使用温度在550~650℃范围内的三种钛合金新材料及其相关技术发展,对国内高温钛合金材料进行初步梳理。参考国外高温钛合金研究、应用经验及发展趋势,结合国内实际情况,对国内高温钛合金材料体系的建立及完善提出具体建议,并展望国内高温钛合金近期研究重点和未来发展方向。

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金和喜, 魏克湘, 李建明等. 航空用钛合金研究进展[J]. 中国有色金属学报, 2015, 25: 280

Jin H X, Wei K X, Li J M, et al.Research development of titanium alloy in aerospace industry[J]. Chin. J. Nonfer. Metals, 2015, 25: 280

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Li M Q, Lin Y Y.Grain refinement in near alpha Ti60 titanium alloy by the thermohydrogenation treatment[J]. Int. J. Hydrogen Energy, 2007, 32: 626

DOI:10.1016/j.ijhydene.2006.06.040 URL

The Ti60 titanium alloy, as one of high-temperature titanium alloys, has good creep resistance against high temperature, excellent thermostability at the servicing temperature of 600 C. The microstructure and the phases are investigated through Optical microscopy (OM), Scanning electron microscopy (SEM) and X-ray diffraction analysis (XRD) after thermohydrogenation treatment of the Ti60 titanium alloy. The grains have been refined significantly through the thermohydrogenation treatment, and the occurrence and disappearance of the hydride phase is a main mechanism of grain refinement in the thermohydrogenation treatment of Ti60 titanium alloy.

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Jia W J, Zeng W D, Zhou Y G, et al.High-temperature deformation behavior of Ti60 titanium alloy[J]. Mater. Sci. Eng., 2011, 528A: 4068

DOI:10.1016/j.msea.2011.01.113 URL

Isothermal compressions of near-alpha Ti60 alloy were carried out on a Gleeble-3800 simulator in the temperature range of 960–1110 °C and strain rate range of 0.001–10.0 s 611. The high-temperature deformation behavior was characterized based on an analysis of the stress–strain behavior, kinetics and processing map. The flow stress behavior revealed greater flow softening in the two-phase field compared with that of single-phase field. In two-phase field, flow softening was caused by break-up and globularization of lamellar α as well as deformation heating during deformation. While in the single-phase field, flow softening was caused by dynamic recovery and recrystallization. Using hyperbolic–sine relationships for the flow stress data, the apparent activation energy was determined to be 653 kJ/mol and 183 kJ/mol for two-phase field and single-phase field, respectively. The processing map exhibited two instability fields: 960–980 °C at 0.3–10 s 611 and 990–1110 °C at 0.58–10 s 611. These fields should be avoided due to the flow localization during the deformation of Ti60 alloy.

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Sun F, Li J S, Kou H C, et al.β phase transformation kinetics in Ti60 alloy during continuous cooling[J]. J. Alloy. Compd., 2013, 576: 108

DOI:10.1016/j.jallcom.2013.04.117 URL


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