Investigation of microstructures and high-temperature tensile behavior of heat treated GTD222 nickel-based superalloy prepared by selective laser melting

被引:1
|
作者
Lv, Yuting [1 ]
Dong, Hao [1 ]
Lang, Xianwei [1 ]
Zhang, Qiang [1 ]
Deng, Wentang [1 ]
Jiang, Di [1 ]
Wang, Rui [2 ,3 ,4 ]
Wei, Guijiang [5 ]
机构
[1] Shandong Univ Sci & Technol, Coll Mech & Elect Engn, Qingdao 266590, Shandong, Peoples R China
[2] Gaona Aero Mat Co Ltd, Beijing, Peoples R China
[3] Cent Iron & Steel Res Inst, Beijing Key Lab Adv High Temp Mat, Beijing, Peoples R China
[4] Shanghai Jiao Tong Univ, Shanghai Key Lab Adv High Temp Mat & Precis Formin, 800 Dongchuan Rd, Shanghai 200240, Peoples R China
[5] Youjiang Med Univ Nationalities, Affiliated Hosp, Baise 533000, Guangxi, Peoples R China
基金
美国国家科学基金会;
关键词
GTD222; superalloy; Selective laser melting; Heat treatment; High -temperature tensile; ELECTRICAL CONTACT MATERIALS; ARC-EROSION BEHAVIOR; LOMER-COTTRELL LOCKS; MECHANICAL-PROPERTIES; DEFORMATION; EVOLUTION; CREEP;
D O I
10.1016/j.jmrt.2023.12.046
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this study, various heat treatment methods including direct aging and solution aging were performed on the selective laser melted (SLMed) GTD222 nickel-based superalloy, and the microstructures and high-temperature tensile behavior of the superalloys were systematically investigated. The results indicate that, in comparison to the as-deposited superalloy, both direct aging and solution aging lead to a significant enhancement in high -temperature strength and ductility. The directly aged superalloy exhibits a higher yield strength, while the solution-aged ones displays superior elongation. Specifically, at a tensile temperature of 760 degrees C, the superalloy subjected to a solution treatment at 1240 degrees C demonstrates the most favorable tensile properties, boasting a tensile strength of 835 MPa, an elongation rate of 6.5 %, and a reduction in area of 13 %. This study also provides a detailed discussion of the high temperature tensile behavior of the SLMed GTD222 superalloy after heat treatment.
引用
收藏
页码:900 / 910
页数:11
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