|
|
MICROSTRUCTURE AND MECHANICAL PROPERTIES OF K4202 CAST NICKEL BASE SUPERALLOY FABRICATED BY SELECTIVE LASER MELTING |
Wenpu HUANG,Hanchen YU,Jie YIN,Zemin WANG( ),Xiaoyan ZENG |
Wuhan National Laboratory of Optoelectronics, Huazhong University of Science and Technology, Wuhan 430074, China |
|
Cite this article:
Wenpu HUANG,Hanchen YU,Jie YIN,Zemin WANG,Xiaoyan ZENG. MICROSTRUCTURE AND MECHANICAL PROPERTIES OF K4202 CAST NICKEL BASE SUPERALLOY FABRICATED BY SELECTIVE LASER MELTING. Acta Metall Sin, 2016, 52(9): 1089-1095.
|
|
Abstract As a cast nickel base superalloy, K4202 is mainly used in aircraft engines due to its high strengths at elevated temperatures, excellent resistance to hot corrosion and favorable weldability. K4202 alloy is usually fabricated by the conventional casting method and mechanical processing, along with macro-segregation and excessive tool wear. As one of the most promising additive manufacturing technologies, selective laser melting (SLM) is able to manufacture high-performance and complex components. According to the requirement of selective laser melting manufactured metal parts with complex structures in aerospace and other fields, K4202 alloy was used as material for SLM in this research and the forming technology, microstructure and mechanical properties of SLMed and heat-treated samples were studied. The results show that the microstructure of samples formed by SLM is composed of dendrites and isometric crystal. The growing direction of dendrites is nearly perpendicular to melt pool traces in most cases. The dendrite structures disappear completely after solution+ageing heat treatment on account of recrystallization and metal carbide precipitates in grains and at grain boundaries. The precipitates are able to improve the strength of the grain boundary due to the pinning effect. The microstructure has no significant changes after ageing heat treatment, but carbide precipitates at grain boundaries as well. The microhardness of SLM samples is uniform on cross section and vertical section. After solution+ageing and ageing heat treatment, there is a significant improvement on the microhardness. The mechanical properties for as-fabricated samples are superior to those of the cast K4202. Besides, the yield strength and tensile strength increase clearly after heat treatments and the mechanical properties is the highest after ageing heat treatment. This is because of the precipitation of γ' strengthening phases. However, the obvious decrease in the ductility occurs at the same time.
|
Received: 22 December 2015
|
Fund: Supported by High Technology Research and Development Program of China (No.2013AA031606) |
[1] | Wang J M, Shao C, Zhao M H, Cai Q K.Mod Manuf Eng, 2007; (9): 91 | [1] | (王建明, 邵冲, 赵明汉, 才庆魁. 现代制造工程, 2007; (9): 91) | [2] | Costes J P, Guillet Y, Poulachon G, Dessoly M.Int J Mach Tools Manuf, 2007; 47: 1081 | [3] | Qi H, Azer M, Ritter A.Metall Mater Trans, 2009; 40A: 2410 | [4] | Zhang D Y, Niu W, Cao X Y, Liu Z. Mater Sci Eng, 2015; A644: 32 | [5] | Zhang B J, Zhao G P, Zhang W Y, Huang S, Chen S F.Acta Metall Sin, 2015; 51: 1227 | [5] | (张北江, 赵光普, 张文云, 黄烁, 陈石富. 金属学报, 2015; 51: 1227) | [6] | Tian Z J, Gu D D, Shen L D, Xie D Q, Wang D S.Aeron Manuf Technol, 2015; (11): 38 | [6] | (田宗军, 顾冬冬, 沈理达, 谢德巧, 王东生. 航空制造技术, 2015; (11): 38) | [7] | Chen J L, Dong P, Zhang K, He J W, Liang X K.Electromach Mould, 2014; (1): 66 | [7] | (陈济轮, 董鹏, 张昆, 何京文, 梁晓康. 电加工与模具, 2014; (1): 66) | [8] | Cui C X, Hu B M, Zhao L C.Mater Des, 2011; 32: 1684 | [9] | Yadroitsev I, Smurov I.Phys Procedia, 2010; 5: 551 | [10] | Vilaro T.Mater Sci Eng, 2012; A534: 446 | [11] | Kanagarajah P, Brenne F, Niendorf T.Mater Sci Eng, 2013; A588: 188 | [12] | Wei K W, Wang Z M, Zeng X Y.Mater Lett, 2015; 156: 187 | [13] | Zhang H, Zhu H H, Qi T, Hu Z H, Zeng X Y.Mater Sci Eng, 2016; A656: 47 | [14] | Pauly S, L?ber L, Romy P.Mater Today, 2013; 16: 37 | [15] | Chlebus E, Gruber K, Ku?nicka B, Kurzac J, Kurzynowski T.Mater Sci Eng, 2015; A638: 647 | [16] | Shi Y S, Lu Z L, Zhang W X, Huang S H, Chen G Q.Chin Surf Eng, 2006; 19(5+): 150 | [16] | (史玉升, 鲁中良, 章文献, 黄树槐, 陈国清. 中国表面工程, 2006; 19(5+): 150) | [17] | Song B, Dong S J, Coddet P, Liao H L, Coddet C.Mater Des, 2014; 53: 1 | [18] | Wang Z M, Guan K, Gao M, Li X Y, Chen X F, Zeng X Y.J Alloys Compd, 2012; 513: 518 | [19] | Mumtaz K A, Hopkinson N.J Mater Process Technol, 2010; 210: 279 | [20] | Li S, Wei Q S, Shi Y S, Zhu Z C, Zhang D Q.J Mater Sci Technol, 2015; 31: 946 | [21] | Harrison N J, Todd I, Mumtaz K. Acta Mater, 2015; 94: 59 | [22] | Bi G J, Sun C N, Chen H C, Ng F L, Ma C C K.Mater Des, 2014; 60: 401 | [23] | Kunze K, Etter T, Gr?sslin J, Shklover V.Mater Sci Eng, 2015; A620: 213 | [24] | Rickenbacher L, Etter T, Hovel S.Rapid Prototyping J, 2013; 19: 282 | [25] | Huang Q Y, Li H K.Superalloy. Beijing: Metallurgical Industry Press, 2000: 6 | [25] | (黄乾尧, 李汉康. 高温合金. 北京:冶金工业出版社, 2000: 6) | [26] | Liu Q C, Elambasseril J, Sun S J, Leary M, Brandt M, Sharp P K. Adv Mater Res, 2014; 891: 1519 | [27] | Loh L E, Liu Z H, Zhang D Q, Mapar M, Sing S L, Chua C K, Yeong W Y.Virtual Phy Prototyping, 2014; 9: 11 | [28] | He L Z, Zheng Q, Sun X F, Guan H R, Hu Z Q, Tieu A K, Lu C, Zhu H T.Mater Sci Eng, 2005; A397: 297 | [29] | Guo J T.Materials Science and Engineering for Superalloys. Beijing: Science Press, 2008: 322 | [29] | (郭建亭. 高温合金材料学. 北京: 科学出版社, 2008: 322) | [30] | Vilaro T, Colin C, Bartout J D, Nazé L, Sennour M.Mater Sci Eng, 2012; A534: 446 | [31] | Song K, Yu K, Lin X, Chen J, Yang H O, Huang W D.Acta Metall Sin, 2015; 51: 935 | [31] | (宋衎, 喻凯, 林鑫, 陈静, 杨海欧, 黄卫东. 金属学报, 2015; 51: 935) | [32] | Shao C, Li J T, Wu J T, Zhao M H.In: Zhang W ed., Proc 11th China Superalloys Conference, Beijing: Metallurgical Industry Press, 2007: 364 | [32] | (邵冲, 李俊涛, 吴剑涛, 赵明汉. 见: 张卫主编, 第十一届中国高温合金年会论文集, 北京: 冶金工业出版社, 2007: 364) |
|
No Suggested Reading articles found! |
|
|
Viewed |
|
|
|
Full text
|
|
|
|
|
Abstract
|
|
|
|
|
Cited |
|
|
|
|
|
Shared |
|
|
|
|
|
Discussed |
|
|
|
|