Preparation of NiTip/Al composites with controllable phase transformation and damping behavior by friction stir processing

被引:4
|
作者
Wu, Xiao [1 ,2 ]
Jiang, Hongjie [1 ,2 ]
Li, Wangyun [3 ]
Liu, Chongyu [1 ]
Huang, Hongfeng [1 ]
Liu, Shuhui [2 ]
Wei, Lili [2 ]
机构
[1] Guilin Univ Technol, Sch Mat Sci & Engn, Guilin 541004, Peoples R China
[2] Guilin Univ Technol, Key Lab New Proc Technol Nonferrous Met & Mat, Minist Educ, Guilin 541004, Peoples R China
[3] Guilin Univ Elect Technol, Sch Mech & Elect Engn, Guilin 541004, Peoples R China
基金
中国国家自然科学基金;
关键词
NiTi particle; aluminum matrix composites; phase transformation; damping behavior; friction stir processing; DYNAMIC YOUNGS MODULUS; MECHANICAL-PROPERTIES; MATRIX COMPOSITES; THERMAL-EXPANSION; AGING TREATMENT; HIGH-STRENGTH; CAPACITY; ALLOY; MICROSTRUCTURE; TEMPERATURE;
D O I
10.1007/s11431-023-2487-y
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The NiTip/1060Al composites were prepared using a pre-aging and friction stir method (FSP) to enhance the low-temperature damping performance of the aluminum alloy and accommodate various service temperatures. The bonding between NiTi particles and the 1060Al matrix is well established after FSP, and no new phases are formed in the composites. The phase-transformation peak temperature of NiTip/1060Al composites gradually shifts to lower temperatures with increased aging temperature of NiTi particles. At room temperature, the 550 degrees C-NiTip/1060Al composite exhibits superior damping performance, with an internal friction value 144% higher than that of the FSP-1060Al alloy. However, at -91 degrees C, the 650 degrees C-NiTip/1060Al composite demonstrates better damping performance, with an internal friction value 158% higher than that of the FSP-1060Al alloy. The NiTip/1060Al composites exhibit the internal friction peak of NiTi phase-transformation in the temperature range from -91 degrees C to 60 degrees C. This characteristic results in significantly better damping performance compared to the FSP-1060Al alloy and other high-damping aluminum matrix composites.
引用
收藏
页码:597 / 607
页数:11
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