Microstructure and High-Temperature Mechanical Properties of a Superalloy Joint Deposited with CoCrMo and CoCrW Welding Wires

被引:1
|
作者
Huang, Shuai [1 ]
Wang, Tianyuan [1 ]
Miao, Jian [1 ]
Chen, Xing [1 ]
Zhang, Guohui [1 ]
Chen, Bingqing [1 ]
Zhou, Biao [1 ]
机构
[1] Beijing Inst Aeronaut Mat, Printing Res & Engn Technol Ctr 3D, Beijing 100095, Peoples R China
关键词
single crystal superalloy; overlay welding; welding wire; high-temperature tensile; LASER; BEHAVIOR; ALLOYS; RESISTANCE; EVOLUTION;
D O I
10.3390/coatings14070892
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The preparation of a single crystal superalloy surface overlay welding coating to improve its high-temperature mechanical properties is of great significance for prolonging the service life of blades. This work selected two types of welding wire alloys, CoCrMo and CoCrW, to prepare coatings on the surface of a single crystal superalloy. A comparative study was conducted on their mechanical properties, such as tension, compression, fatigue, durability, and wear at a high temperature of 900 degree celsius, aiming to reveal the high-temperature mechanical properties of the two types of welding coatings. Results showed that the average high-temperature tensile strength of the CoCrMo welded specimen was smaller than that of the CoCrW welded specimen; the average high-temperature duration of CoCrMo welded specimens at 150 MPa was lower than the average duration of CoCrW welded specimens; the high-temperature fatigue life of CoCrMo welded specimens at 220 MPa was 7.186 x 105; and the average high-temperature wear rate of CoCrMo sample was 3.64 x 10-6 mm3<middle dot>N-1<middle dot>m-1. The CoCrW alloy was more wear resistant than CoCrMo. The hardness of CoCrMo welded joints gradually increased from the substrate to the heat-affected zone and then to the fusion zone, and was much higher in the fusion zone than in the CoCrW alloy.
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页数:16
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