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热处理制度对TA15合金组织与性能的影响 被引量:14

Effect of heat-treatment on microstructure and properties of TA15 alloy
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摘要 研究了不同热处理制度对TA15钛合金显微组织和性能的影响。结果表明:两相区热处理时,获得了双态和等轴组织;β相区热处理,获得了魏氏组织,冷却速率决定了α片层和α集束的尺寸。魏氏组织的拉伸强度水平与双态/轴组织相当,断裂韧度较高,疲劳裂纹扩展速率较低,塑性有所降低。β相区空冷所得魏氏组织,具有中等强度水平,但断裂韧度较高,抗疲劳裂纹扩展性能最好。 The effects of heat-treatment on microstructure and properties of TA15 alloy were studied. The results show that the Widmanstaten microstructure formed by heating TA15 alloy in β phase region exhibits similar strength, higher fracture toughness and fatigue crack propagation resistance, compared with that of the equiaxed a and (α + β) TA15 alloy formed by heating the alloy in α + β phase region and then cooling using different cooling rate. The width of α lamellae and α colonies depends on the cooling rate. The TA15 alloy with Widmanstaten microstructure obtained by heating it in β phase region and then cooling in air exhibits middle tensile strength, higher fracture toughness and fatigue crack propagation resistance.
出处 《材料热处理学报》 EI CAS CSCD 北大核心 2008年第6期82-85,共4页 Transactions of Materials and Heat Treatment
关键词 TA15钛合金 热处理 显微组织 断裂韧度 疲劳裂纹扩展 TA15 alloy heat-treatment mierostructure fracture toughness fatigue crack propagation
作者简介 李士凯(1978-),男,洛阳船舶材料研究所,博士,从事钛合金研究,电话:0379-67256041,E-mail:LSK786150@163.com。
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参考文献6

  • 1鲍莉索娃.钛合金金相学[M].陈石卿,译.北京:国防工业出版社,1980.
  • 2闵新华,朱益藩,罗月新.变形量对Ti-6Al-2Zr-1Mo-1V合金组织和性能的影响[J].金属学报,2002,38(z1):181-182. 被引量:2
  • 3C莱茵斯,M皮特尔斯编,陈阵华等译.钛与钛合金[M].北京:化学工业出版社,2005
  • 4Filip R, Kubiak K, Ziaja W. The effect of microstructure on the mechanical properties of two-phase Titanium alloys [ J]. Journal of Materials Processing Technology, 2003, 133:84 - 89.
  • 5Lutjering G. Influence of processing on microstructure and mechanical properties of (α+β) titanium alloys[J]. Material Science and Engineering A, 1998, 243 : 32 - 45.
  • 6张旺峰,曹春晓,李兴无,马济民,朱知寿.加载方式与初生α相对钛合金裂纹扩展行为的影响[J].钛工业进展,2004,21(4):26-29. 被引量:7

二级参考文献15

  • 1Eylon D, Hall J A, Pierce C M et al. Microstructure and Mechanical Properties Relationships in the Ti-11Alloy at Room and Elevated Temperatures [ J ]. Metall TransA, 1990, 21A (6): 1733-1744
  • 2Yu-Zhentao, Zhou Lian, Deng Ju, Gu Haicheng. Investigation on monotonic and Cyclic Stress-strain Characteristics of Ti-2Al-2.5Zr [ J ]. Mat Sci Eng A,2000, A280:195-197
  • 3Zhang Z F, Gu H C, Tan X L. Low-cycle Fatigue Behaviors of Commercial-purity Titanium [J ]. Mat Sci Eng, 1998, A252:85-90
  • 4Brun M, Shakhanova G. Titanium Alloy Structure and Parameters Defining Its Diversity [J]. Titanium ScientificTechnicalJournal, 1993, 1:24-29
  • 5Wanhill R J H. Ambient Temperature Crack Growth in Titanium Alloys and Its Significance for Aircraft Structures [J]. Aeronautical Journal, 1977, 81:68-82
  • 6Jafee R I, Burte H M. Titanium Science and Technology [C]. New York-London: Plenum Press, 1973:1257- 1270, 1731- 1744, 553-572
  • 7Scmiatin S L, Thomas J F et al. Processing-microstructure Relationships for Ti-6Al-2Sn-4Zr-2Mo-0.1Si [J]. Metall Trans A, 1983, 14A: 2363-2374
  • 8Brun M, Shakhanova G. Principles of Titanium Alloys'Structure Control with the Purpose of Increasing Their Mechanical Properties [C]. The Minerals, Metals & Materials Society, 1997:193-199
  • 9Bratukhin A G, Anoshkin N F, Moiseev V N et al.Application of Titanium Alloys for Production of Aircraft Structures [J]. Titanium Scientific Technical Journal,1993, 1:77-81
  • 10Hines J A, lutjering G. Propagation of Microcracks at stress Amplitudes Below The Conventional Fatigue limit in Ti-6Al-4V [J]. Fatigue Fract Eng Mater stuct,1999, 22, 657-665

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