Effect of High-Pressure Aging Treatment on Microstructure and Properties of Cu-51.15W-0.24Cr Alloy

被引:0
|
作者
Gu Tao [1 ,2 ]
Zhang Shuaixin [1 ]
Zhao Yuhong [1 ]
Fu Dongxing [2 ]
Zhang Zhibin [3 ]
Liu Jianhua [4 ]
Hou Hua [1 ]
机构
[1] North Univ China, Sch Mat Sci & Engn, Taiyuan 030051, Peoples R China
[2] GRIPM Adv Mat Co Ltd, Gen Res Inst Nonferrous Met, Beijing 100088, Peoples R China
[3] Acad Mil Sci PLA China, Natl Innovat Inst Def Technol, Beijing 100071, Peoples R China
[4] Yanshan Univ, Coll Mat Sci & Engn, Key Lab Metastable Mat Sci & Technol, Qinhuangdao 066004, Hebei, Peoples R China
基金
中国国家自然科学基金; 山西省青年科学基金;
关键词
Cu-51.15W-0.24Cr alloy; high-pressure aging treatment; hardness; thermal diffusivity; resistivity; HEAT-TREATMENT; ELECTRICAL-CONDUCTIVITY; STRENGTHENING MECHANISM; THERMAL-EXPANSION; CU COMPOSITE; EVOLUTION; FABRICATION; TUNGSTEN;
D O I
暂无
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Aiming at solving the problem of poor strength, low conductivity and thermal conductivity of Cu-W alloys, high pressure aging treatment was conducted to reinforce Cu-51.15W-0.24Cr alloy. The microstructure, hardness, thermal conductivity and conductivity of the alloy after high pressure aging treatment and normal pressure aging treatment were compared. The results show that high pressure aging treatment can increase the compactness of Cu48.61W51.15Cr0.24 alloy, eventually resulting in more dispersed distribution and finer grain size of Cr phase during the aging treatment, and improving the hardness and thermal conductivity of the alloy. After solution treatment at 960 degrees C for 1 h and aging at 500 degrees C for 1 h under a pressure of 3 GPa, the hardness, thermal diffusivity and resistivity are determined to be 1540 MPa, 0.5236 cm(2).s(-1) and 4.458x10(4) Omega.m, respectively, which are 17.56% and 10.74% higher than and 4.85% lower than those of alloy under normal pressure, respectively. Therefore, high pressure aging treatment can be an effective way to improve mechanical properties and to reduce resistivity of Cu-51.15W-0.24Cr alloy.
引用
收藏
页码:4224 / 4229
页数:6
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