DD5单晶高温合金大间隙钎焊的组织演变与界面形成机制*
收稿日期: 2015-12-03
网络出版日期: 2016-04-29
基金资助
*国家自然科学基金项目51401210和51331005以及国家高技术研究发展计划项目2014AA041701资助
MICROSTRUCTURE EVOLUTION AND INTERFACIAL FORMATION MECHANISM OF WIDE GAP BRAZING OF DD5 SINGLE CRYSTAL SUPERALLOY
Received date: 2015-12-03
Online published: 2016-04-29
Supported by
Supported by National Natural Science Foundation of China (Nos.51401210 and 51331005) and High Technology Research and Development Program of China (No.2014AA041701)
采用新型Ni-Co-Cr-W-B+DD99混合粉末钎料焊接DD5单晶高温合金, 分析钎料成分对接头显微组织演变和接头力学性能的影响, 探讨Ni-Co-Cr-W-B钎料/DD99合金粉的界面形成机制与接头形成机理. 结果表明, 在钎焊过程中, Ni-Co-Cr-W-B钎料/DD99合金粉的界面上首先形成了γ-Ni初生相, B偏析并析出细小颗粒状的M3B2 型硼化物, 在冷却过程中残余液相形成块状M3B2相、γ+γ′共晶相和γ-Ni+Ni3B+CrB共晶相. 提高混合粉末钎料中DD99合金粉的配比, 可有效抑制焊缝中的硼化物和低熔点共晶相的形成, 提高焊缝成分和组织均匀性. 当DD99合金粉的配比增加至70% (质量分数)时, B可均匀扩散至DD5母材和DD99合金粉中, 未观察到低熔点共晶相, 界面处脆性化合物相显著减少, 接头高温性能提高. 接头经过固溶处理和时效处理后, 在870 ℃的高温拉伸性能可提高至1010 MPa.
孙元 , 刘纪德 , 侯星宇 , 王广磊 , 杨金侠 , 金涛 , 周亦胄 . DD5单晶高温合金大间隙钎焊的组织演变与界面形成机制*[J]. 金属学报, 2016 , 52(7) : 875 -882 . DOI: 10.11900/0412.1961.2015.00622
Ni-based single-crystal superalloy DD5 has excellent high temperature properties, which is the preferred raw material for aero-engine turbine blade in recent year. In this research, DD5 superalloy was brazed by different contents of Ni-Co-Cr-W-B+DD99 mixed powder filler alloy. The microstructure evolution and interfacial formation mechanism of DD5 superalloy brazing joint were analyzed by SEM and EPMA. The mechanical properties of joint after solid solution treatment and aging treatment were tested. The results show that γ-Ni primary phase formed firstly in the Ni-Co-Cr-W-B/DD99 interface during the brazing process, and then B element segregated and precipitated to fine granular M3B2 type boride. The residual liquid phase solidified and formed lastly to the M3B2 phase, γ+γ′ eutectic phase and γ-Ni+Ni3B+CrB eutectic phase during cooling. With increasing the ratio of DD99 in mixed powder filler alloy, the low melting point eutectic phase and borides in the joint decrease and the uniformity of composition and microstructure of joint improve. When the ratio of DD99 increased to 70% (mass fraction) in the mixed powder filler alloy, it can be observed that element of B diffused to DD99 additive powder which result ed in the decrease of low melting point eutectic phases and brittle compounds. The high temperature tensile properties of joint is 1010 MPa at 870 ℃.
| [1] | Zhang X L, Zhou Y Z, Jin T, Sun X F.Acta Metall Sin, 2012; 48: 1229 |
| [1] | (张晓丽, 周亦胄, 金涛, 孙晓峰. 金属学报, 2012; 48: 1229) |
| [2] | Tung S K, Lim L C, Lai M O.Scr Mater, 1996; 34: 763 |
| [3] | Huang X, Miglietti W.J Eng Gas Turb Power, 2012; 134: 010801 |
| [4] | Chen Y, Zhang K, Huang J, Hosseini S R E, Li Z G.Mater Des, 2016; 90: 586 |
| [5] | Zhang D X, Liu D S, Zhu X P.In: Sung W P, Chen R eds., 3rd Int Conf Frontiers of Manufacturing and Design Science, Hong Kong: Trans Tech Publications LTD, 2013: 64 |
| [6] | Liu T, Yan F, Liu S, Li R Y, Wang C M, Hu X Y.Opt Laser Technol, 2016; 80(2): 56 |
| [7] | Chelladurai A M, Gopal K A, Murugan S, Albert S K, Venugopal S, Jayakumar T.Sci Technol Weld Joining, 2015; 20: 578 |
| [8] | Ma T J, Yan M, Yang X W, Li W Y, Chao Y J.Mater Des, 2015; 85: 613 |
| [9] | Du S G, Wang X F, Gao M.Acta Metall Sin, 2015; 51: 951 |
| [9] | (杜随更, 王喜锋, 高漫. 金属学报, 2015; 51: 951) |
| [10] | Cook G O, Sorensen C D.J Mater Sci, 2011; 46: 5305 |
| [11] | Philips N R, Levi C G, Evans A G.Metall Mater Trans, 2008; 39A: 142 |
| [12] | Pill J J, Kang C S.Mater Trans JIM, 1997; 38: 886 |
| [13] | Li W, Jin T, Sun X F, Guo Y, Guan H R, Hu Z Q.Scr Mater, 2003; 48: 1283 |
| [14] | Khakian M, Nategh S, Mirdamadi S.J Alloys Compd, 2015; 653: 386 |
| [15] | Liu A N, Zhai Q Y, Kang W J, Xu J F, Zhang J, Ruan C Y, Wang W.Hot Work Technol, 2014; 43(17): 29 |
| [15] | (刘安娜, 翟秋亚, 康文军, 徐锦锋, 张军, 阮成勇, 王炜. 热加工工艺, 2014; 43(17): 29) |
| [16] | Huang X, Au P.J Eng Gas Turb Power, 2008; 130: 032101 |
| [17] | Henhoeffer T, Huang X, Yand S, Au P, Nagy D.Mater Sci Technol Lond, 2010; 26: 431 |
| [18] | Henhoeffer T, Huang X, Au P.J Eng Gas Turb Power, 2011; 133: 092101 |
| [19] | Guo J T.Material Science and Engineering for Superalloys (II). Beijing: Science Press, 2008: 452 |
| [19] | (郭建亭. 高温合金材料学(中). 北京: 科学出版社, 2008: 452) |
| [20] | Zhuang H S, Lugscheider E. High Temperature Brazing.Beijing: National Defence Industry Press, 1989: 46 |
| [20] | (庄鸿寿, Lugscheider E.高温钎焊. 北京: 国防工业出版社, 1989: 46) |
| [21] | Li X H, Zhong Q P, Cao C X.J Aeron Mater, 2003; 23(12): 10 |
| [21] | (李晓红, 钟群鹏, 曹春晓. 航空材料学报, 2003; 23(12): 10) |
| [22] | Li X H, Xiong H P, Zhang X J.Joining Technologies of Advanced Aeronautical Materials. Beijing: National Defense Industry Press, 2012: 28 |
| [22] | (李晓红, 熊华平, 张学军. 先进航空材料焊接技术. 北京: 国防工业出版社, 2012: 28) |
| [23] | Sheng N C, Liu J D, Jin T, Sun X F, Hu Z Q.Philos Mag, 2014; 94: 1219 |
| [24] | Sheng N C, Liu J D, Jin T, Sun X F, Hu Z Q.J Mater Sci Technol, 2015; 31: 129 |
| [25] | Sheng N C, Liu J D, Jin T, Sun X F, Hu Z Q.Metall Mater Trans, 2013; 44A: 1793 |
| [26] | Liu J D.PhD Dissertation, Institute of Metal Research, Chinese Academy of Sciences, Shenyang, 2007 |
| [26] | (刘纪德. 中国科学院金属研究所博士学位论文, 沈阳, 2007) |
| [27] | Sun Y, Liu J D, Liu Z M, Yang J X, Li J G, Jin T, Sun X F.Acta Metall Sin, 2013; 49: 1581 |
| [27] | (孙元, 刘纪德, 刘忠明, 杨金侠, 李金国, 金涛, 孙晓峰. 金属学报, 2013; 49: 1581) |
/
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|
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