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Ti_3AlC_2掺杂SPS法制备Ti_2AlC/TiAl基复合材料的研究 被引量:2

Ti_2AlC/TiAl Composites with Doped Ti_3AlC_2 by SPS
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摘要 通过2TiC-Ti-1.2Al体系的原位热压反应制备Ti_3AlC_2陶瓷,然后以59.2Ti-30.8Al-10Ti_3AlC_2(质量分数,下同,%)为反应体系,采用放电等离子烧结技术制备Ti_2AlC/Ti Al基复合材料。借助XRD、SEM分析产物的相组成和微观结构,并测量其室温力学性能。结果表明:原位热压烧结产物由Ti_3AlC_2和TiC相组成,Ti_3AlC_2呈典型的层状结构,TiC颗粒分布在其间;SPS法制备的Ti_2AlC/Ti Al基复合材料主要由Ti Al、Ti_3Al和Ti_2AlC相组成,Ti_2AlC增强相主要分布于基体晶界处,发挥了晶界/晶内内生型强化相的增强作用。力学性能测试表明:Ti_2AlC/Ti Al基复合材料的密度、维氏硬度、断裂韧性和抗弯强度分别为3.85 g/cm^3、5.37 GPa、7.17 MPa·m^(1/2)和494.85 MPa,穿晶、沿晶及层状撕裂等混合断裂特征对改善性能发挥了重要作用。 Ti_3AlC_2 ceramics were fabricated by in-situ reaction in the 2TiC-Ti-1.2Al system.The Ti_2AlC/Ti Al composites were prepared by spark plasma sintering in the 59.2Ti-30.8Al-10Ti_3AlC_2(wt%)system.The phase composition and microstructure of the products were analyzed by XRD and SEM,respectively.The room temperature mechanical properties were also measured.The results reveal that the in-situ heat pressed Ti_3AlC_2 materials are composed of Ti_3AlC_2 and TiC phases.Ti_3AlC_2 ceramics present layered structure and TiC particles distribute around the grain boundaries.The Ti_2AlC/Ti Al composites prepared by SPS are mainly composed of Ti Al,Ti_3Al and Ti_2AlC phases.Ti_2AlC reinforcements are mainly distributed in the matrix grain boundaries,which exhibit the grain-boundary strengthening or intracrystalline strengthening effect.The density,Vickers hardness,fracture toughness and flexural strength of the Ti_2AlC/Ti Al composites are 3.85 g/cm^3,5.37 GPa,7.17 MPa·m^(1/2) and 494.85 MPa,respectively.The fracture features such as transgranular,intergranular and lamellar tearing play an important role in improving the performance of the composites.
机构地区 陕西理工大学
出处 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2017年第S1期1-4,共4页 Rare Metal Materials and Engineering
基金 国家自然科学基金面上项目(51671116) 陕西省自然科学基础研究计划重点项目(2016JZ016) 陕西省教育厅自然科学重点科学研究计划项目(16JS018) 陕西省青年科技新星科技计划项目(2014KJXX-75) 陕西理工大学科研计划项目(SLGQD16-04)
关键词 TI3ALC2 Ti2AlC/TiAl基复合材料 放电等离子烧结技术 力学性能 Ti_3AlC_2 Ti_2AlC/TiAl composites spark plasma sintering mechanical properties
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  • 1张宁,林均品,王艳丽,陈国良.合金元素Y对高铌TiAl高温合金长期抗氧化性的影响[J].航空材料学报,2006,26(6):42-45. 被引量:11
  • 2师昌绪,仲增墉.中国高温合金40年[J].金属学报,1997,33(1):1-8. 被引量:80
  • 3Gahn S Michael, Morris Robert W. Integrated High Performance Turbine Engine Technology (IHPTET) Program Brochure [ EB/ OL]. 2002. http://www, pr. afrl. af. mil/divisions/prt/ihptet/ ihptet_broehure, pdf. 被引量:1
  • 4China Aeronautical Materials Handbook Editorial Board (中国航空材料手册编委会). China Aeronautical Materials Handbook ( 中国航空材料手册) [M]. Beijing: Aviation Industry Press, 2006. 被引量:1
  • 5Lutjering G, Williams J C. Titanium [ M ]. New York: Springer-Verlag Berlin Heidelberg Press, 2003 : 27 - 70. 被引量:1
  • 6Valentin N Moiseyev. Titanium Alloys: Ruasian Aircraft and Aerospace Applicatiorrs [ M ] , New York : Taylor & Francis Group, 2006. 被引量:1
  • 7Christoph Leyens, Manfred Peters. Titanium atwl Titanium Alloys [M]. Weinheim: Wiley-VCH Verlag GmbH & Co. KGaA, 2003. 被引量:1
  • 8Blackburn M J, Smith M P. R&D on Composition and Processing of Titanium Aluminide Alloys for Turbine Engines [ R ]. Ohio: U. S. Air Force Wright Aeronautical Laboratories 1982. 被引量:1
  • 9Blackburn M J, Smith M P. Titanium Alloys of the TiAl Type: US, Patent d 294 615 [ P] . 1981 -10-13. 被引量:1
  • 10Huang S C. Method of Processing Titanium. Aluminum Alloys Modified by Chromium and Niobium: US, 5076858 [ P]. 1991 -12 -31. 被引量:1

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