The tensile and fracture toughness properties of a (TiBw + TiCp)/Ti-3.5Al-5Mo-6V-3Cr-2Sn-0.5Fe composites after heat treatment

被引:19
作者
Yang Jianhui [1 ,2 ]
Xiao Shulong [2 ]
Chen, Yuyong [1 ,2 ]
Xu Lijuan [2 ]
Wang Xiaopeng [2 ]
Zhang Dongdong [1 ,2 ]
机构
[1] Harbin Inst Technol, State Key Lab Adv Welding & Joining, Harbin 150001, Heilongjiang, Peoples R China
[2] Harbin Inst Technol, Sch Mat Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 2018年 / 729卷
关键词
Titanium matrix composite; Mechanical property; Microstructure; (TiBw plus TiCp) reinforcement; TITANIUM MATRIX COMPOSITES; HEAT-TREATMENT; MECHANICAL-PROPERTIES; AEROSPACE INDUSTRY; FATIGUE BEHAVIOR; ALLOY; MICROSTRUCTURE; STRENGTH; TIB; ALPHA;
D O I
10.1016/j.msea.2018.05.009
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
This study investigated the tensile and fracture toughness properties of a new (TiBw + TiCp)/Ti-3.5Al-5Mo-6V-3Cr-2Sn-0.5Fe composite subjected to solution treatment at 800 degrees C for 1 h with air cooling followed by aging at 440 degrees C, 480 degrees C, and 520 degrees C for 8 h with air cooling. The composite grains were coarse with distinct boundaries after the solution treatment. As the temperature was increased, alpha(p) merged in triangle boundaries and alpha(s) became finer. The basket two-parallel alpha(s) phase comprised many substructures, which generated many dislocations. Finer alpha(s) corresponded to higher strength and fracture toughness. The ultimate tensile strength and yield strength after the solution treatment decreased by 12.5% and 11.3%, respectively. However, the strength significantly improved after aging heat treatment. The highest ultimate tensile strength of 1521 MPa with a 7.2% elongation was reached after aging at 440 degrees C. The ultimate K-IC value was 65 MPa m(1/2) after aging at 480 degrees C. The (TiBw + TiCp) reinforcements formed a streamline along the deformation direction, which enhanced the strength and fatigue toughness. The reinforcements improves the fracture toughness by hindering crack propagation to extend the expansion path and increase the amount of absorbed impact energy.
引用
收藏
页码:21 / 28
页数:8
相关论文
共 41 条
[1]  
BANIA PJ, 1994, JOM-J MIN MET MAT S, V46, P16, DOI 10.1007/BF03220742
[2]   Influence of phase transformation kinetics on the formation of α in a β-quenched Ti-5A1-5Mo-5V-3Cr-1Zr alloy [J].
Barriobero-Vila, Pere ;
Requena, Guillermo ;
Schwarz, Sabine ;
Warchomicka, Fernando ;
Buslaps, Thomas .
ACTA MATERIALIA, 2015, 95 :90-101
[3]   Influence of β grain size on tensile behavior and ductile fracture toughness of titanium alloy Ti-10V-2Fe-3Al [J].
Bhattacharjee, A. ;
Varma, V. K. ;
Kamat, S. V. ;
Gogia, A. K. ;
Bhargava, S. .
METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 2006, 37A (05) :1423-1433
[4]   The use of β titanium alloys in the aerospace industry [J].
Boyer, RR ;
Briggs, RD .
JOURNAL OF MATERIALS ENGINEERING AND PERFORMANCE, 2005, 14 (06) :681-685
[5]   An overview on the use of titanium in the aerospace industry [J].
Boyer, RR .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1996, 213 (1-2) :103-114
[6]   Research on development of in situ titanium matrix composites and in situ reaction thermodynamics of the reaction systems [J].
Cai, Lifang ;
Zhang, Yongzhong ;
Shi, Likai ;
Yang, Haoqiang ;
Xi, Mingzhe .
JOURNAL OF UNIVERSITY OF SCIENCE AND TECHNOLOGY BEIJING, 2006, 13 (06) :551-557
[7]   Influence of thermomechanical processing and heat treatment on microstructure, tensile properties and fracture toughness of Ti-1100-0.1B alloy [J].
Chandravanshi, V. K. ;
Bhattacharjee, A. ;
Kamat, S. V. ;
Nandy, T. K. .
JOURNAL OF ALLOYS AND COMPOUNDS, 2014, 589 :336-345
[8]   Effect of boron on microstructure and mechanical properties of thermomechanically processed near alpha titanium alloy Ti-1100 [J].
Chandravanshi, V. K. ;
Sarkar, R. ;
Kamat, S. V. ;
Nandy, T. K. .
JOURNAL OF ALLOYS AND COMPOUNDS, 2011, 509 (18) :5506-5514
[9]   Effects of Thermomechanical Processing and Heat Treatment on the Tensile and Creep Properties of Boron-Modified Near Alpha Titanium Alloy Ti-1100 [J].
Chandravanshi, Vivek ;
Sarkar, R. ;
Kamat, S. V. ;
Nandy, T. K. .
METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 2013, 44A (01) :201-211
[10]   The effect of processing on the 455°C tensile and fatigue behavior of boron-modified Ti-6Al-4V [J].
Chen, W. ;
Boehlert, C. J. ;
Payzant, E. A. ;
Howe, J. Y. .
INTERNATIONAL JOURNAL OF FATIGUE, 2010, 32 (03) :627-638