Microstructure and mechanical properties of wide gap brazing joint of the third-generation nickel-based single crystal superalloy
-
摘要: 采用混合粉末钎料钎焊第三代含铼单晶高温合金,其中混合粉末钎料是利用球磨混粉方法将一种镍基粉末钎料和母材成分相同的高温合金粉混合制成。利用SEM和EPMA分析镍基钎料与高温合金粉配比对接头微观组织的影响,并对四种钎料的钎焊接头进行高温持久性能测试。结果表明:采用镍基钎料的焊缝和混合粉末钎料的焊缝中均存在γ-Ni、γ′、γ+γ′共晶、CrB、Ni3B以及M3B2型硼化物,但混合粉末钎料的残留为熔化的球型高温合金;保持焊缝间隙不变,提高混合粉末钎料中高温合金粉末的配比,可以抑制焊缝中M3B2型硼化物和低熔点相的析出,且硼化物的分布变得更均匀,尺寸变得更小,提高了焊缝成分和组织的均匀性;3种接头的高温持久性能均优于纯钎料接头,当提升合金粉的比例由0%至50%时,接头的持久寿命由15 min提升至34 h,但当合金粉比例增加至60%时,接头中产生大量孔洞缺陷,导致持久寿命下降至4 h。Abstract: In this study, the third-generation rhenium containing single crystal superalloy was brazed by mixed powder filler, in which the mixed powder filler was consisted of nickel-based powder filler and the superalloy powder with the same composition of the base metal. SEM and EPMA were used to analyze the influence of the proportion of the third-generation single crystal superalloy powder in the mixed filler on the microstructure of the joint, and the high temperature stress rupture properties of the brazed joint with four kinds of solder were tested. The result indicates that the microstructures and phase compositions of the Ni-based powder filler and mixed powder filler are both consisted of γ-Ni, γ′, CrB, Ni3B and M3B2 type boride, but the residue of the mixed powder filler is molten ball-type superalloy. With the thickness of brazing gap constant and increasing the ratio of the third-generation single crystal superalloy powder in the mixed filler, the precipitation of M3B2 type boride and low-melting point phases in the joint can be inhibited, and the distribution of borides becomes more uniform and the size becomes smaller, thus improving the uniformity of the composition and microstructure of the joint. When the proportion of alloy powder increased from 0% to 50%, the endurance life of the joint increased from 15 min to 34 hours. However, when the proportion of alloy powder increased to 60%, there are a lot of void defects in the joint, resulting in the endurance life of the joint decreased to 4 hours.
-
Key words:
- mixed powder filler /
- wide gap brazing /
- single crystal superalloy /
- microstructure
-
图 4 JSNi-1、JSNi-2、JSNi-3和JSNi-4接头在980 ℃/100 MPa下持久断口形貌及各接头的持久寿命 (a)JSNi-1;(b)JSNi-2;(c)JSNi-3;(d)JSNi-4;(e)各接头的持久寿命
Figure 4. Rupture fracture morphologies of JSNi-1,JSNi-2,JSNi-3 and JSNi-4 joints at 980 ℃/100 MPa and stress rupture life of joints (a)JSNi-1;(b)JSNi-2;(c)JSNi-3;(d)JSNi-4;(e)stress rupture life of joints
表 1 第三代镍基单晶高温合金与镍基钎料的成分(质量分数/%)
Table 1. Compositions of the 3rd generation nickel-based single crystal superalloy and Ni-based filler alloy(mass fraction/%)
Material Co Cr W Mo Al Ti+ Si B Re Ni 3rd single crystal superalloy 8-10 7-9 4-7 0-2 5-7 0.3-2 — 2-5 Bal JSSNi60A 5-10 6-12 2-6 2-5 2-5 0.9-6 0.2-2.0 — Bal 表 2 混合粉末钎料的成分配比
Table 2. Composition ratio of the mixed powder filler alloy
Material Ratio of mixed powder filler alloy (mass fraction/%) JSNi-1 100%JSSNi60A JSNi-2 70%JSSNi60A+30% alloy powder JSNi-3 50%JSSNi60A+50% alloy powder JSNi-4 40%JSSNi60A+60% alloy powder 表 3 JSNi-3钎料钎焊接头组织中各析出相的电子探针(EPMA)成分(原子分数/%)
Table 3. Results of electron microprobe analysis(EPMA)of each phase in joint of JSNi-3 (atomic fraction/%)
Phase B Al Ni Co Cr W Ta Mo Ti Si M3B2 42.1 — 14.6 5.5 17.7 14.9 1.1 3.2 0.9 — CrB 31.5 — 6.3 4.3 40.6 7.6 1.5 6.8 1.4 — Ni3B 13.4 2.1 52.6 8.9 8.6 4.2 — 2 5.6 2.6 γ+γ′ — 9.3 62.4 8.9 10.2 2.1 1.5 — 3.2 2.4 γ-Ni — 7.2 62.9 10.5 12.5 2.8 1.3 — 1.6 1.2 表 4 JSNi-2接头断口成分分析(原子分数/%)
Table 4. Results of EDS of lumps in fracture morphology of JSNi-2 joint(atomic fraction / %)
Position C O Ti Co Cr Ni Ta Mo W Si Al Massive structure 7.06 32.76 0.45 15.85 2.26 6.51 8.75 3.37 22.99 — — Base metal 4.23 21.47 0.48 8.10 10.07 40.01 3.97 1.10 — 2.84 7.73 -
[1] 孙晓峰,金涛,周亦胄,等. 镍基单晶高温合金研究进展[J]. 中国材料进展,2012,31(12):1-2.SUN X F,JIN T,ZHOU Y Z,et al. Research progress of nickel-base single crystal superalloys[J]. Mater China,2012,31(12):1-2. [2] 胡壮麒,刘丽荣,金涛,等. 镍基单晶高温合金的发展[J]. 航空发动机,2005,31(3):1-3. doi: 10.3969/j.issn.1672-3147.2005.03.001HU Z Q,LIU L R,JIN T,et al. Development of nickel-based single crystal superalloys[J]. Aeroengine,2005,31(3):1-3. doi: 10.3969/j.issn.1672-3147.2005.03.001 [3] 马德新. 高温合金叶片单晶凝固技术的新发展[J]. 金属学报,2015,51:1179.MA D X. Development of single crystal solidification technology for production of superalloy turbine blades [J]. Acta Metallurgica Sinica,2015,51:1179. [4] 黄云,李少川,肖贵坚,等. 航空发动机叶片材料及抗疲劳磨削技术现状[J]. 航空材料学报,2021,41(4):17-35. doi: 10.11868/j.issn.1005-5053.2021.000058HUANG Y,LI S C,XIAO G J,et al. Research progress of aero-engine blade materials and anti-fatigue grinding technology[J]. Journal of Aeronautical Materials,2021,41(4):17-35. doi: 10.11868/j.issn.1005-5053.2021.000058 [5] 王刚,张秉刚,冯吉才,等. 镍基高温合金叶片焊接修复技术的研究进展[J]. 焊接,2008(1):20-23. doi: 10.3969/j.issn.1001-1382.2008.01.009WANG G,ZHANG B G,FENG J C,et al. Research progress of welding repairing technology of nickel base superalloy blade[J]. Welding & Joining,2008(1):20-23. doi: 10.3969/j.issn.1001-1382.2008.01.009 [6] 陈操,韩雷,张钰,等. 镍基合金涡轮叶片的服役损伤机理与性能衰减[J]. 航空材料学报,2021,41(4):96-108. doi: 10.11868/j.issn.1005-5053.2020.000201CHEN C,HAN L,ZHANG Y,et al. Service damage mechanism and performance attenuation of nickel-based alloy turbine blades[J]. Journal of Aeronautical Materials,2021,41(4):96-108. doi: 10.11868/j.issn.1005-5053.2020.000201 [7] EGBEWANDE A,CHUKWUKAEME C,OJO O,et al. Joining of superalloy Inconel 600 by diffusion induced isothermal solidification of a liquated insert metal[J]. Materials Characterization,2008,59(8):1051-1058. doi: 10.1016/j.matchar.2007.08.023 [8] 李文,金涛,胡壮麒. 镍基单晶高温合金瞬态液相连接接头的微观结构和结晶学取向[J]. 金属学报,2008,44(12):1474. doi: 10.3321/j.issn:0412-1961.2008.12.012LI W,JIN T,HU Z Q. Microstructure characteristics and crystallographic orientation of transient liquid phase joint of Ni-based single crystal superalloy[J]. Acta Metallurgica Sinica,2008,44(12):1474. doi: 10.3321/j.issn:0412-1961.2008.12.012 [9] 梁海,叶雷,毛唯. 大间隙钎焊用混合粉状高温镍基钎料的润湿性和显微组织[J]. 航空材料学报,2012,32(4):20-25.LIANG H,YE L,MAO W. Wettability and microstructures of high temperature Ni-based mixed filler powders for wide gap brazing[J]. Journal of Aeronautical Materials,2012,32(4):20-25. [10] 潘晖,赵海生. 钴基钎料钎焊K465合金大间隙接头组织与性能[J]. 航空材料学报,2017(3):50-55. doi: 10.11868/j.issn.1005-5053.2016.000205PAN H,ZHAO H S. Microstructure and mechanical properties of wide-gap brazed joints of K465 alloy using cobalt-base brazing alloy[J]. Journal of Aeronautical Materials,2017(3):50-55. doi: 10.11868/j.issn.1005-5053.2016.000205 [11] SUA C Y,LIHA W C,CHOUB C P,et al. Activated diffusion brazed repair for IN738 hot section components of gas turbines[J]. Journal of Materials Processing Technology,2001,115(3):326-332. doi: 10.1016/S0924-0136(01)00831-7 [12] 孙元,刘纪德,侯星宇,等. 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.SUN Y,LIU J D,HOU X Y,et al. Microstructure evolution and interfacial formation mechanism of wide gap brazing of DD5 single crystal superalloy[J]. Acta Metallurgica Sinica,2016,52(7):875-882. [13] 李晓红,钟群鹏,曹春晓. K403与DZ4高温合金的大间隙钎焊[J]. 航空材料学报,2003,23(4):10-15. doi: 10.3969/j.issn.1005-5053.2003.04.003LI X H,ZHONG Q P,CAO C X. Wide-gap brazing between K403 and DZ4 superalloys[J]. Journal of Aeronautical Materials,2003,23(4):10-15. doi: 10.3969/j.issn.1005-5053.2003.04.003 [14] 孙元,刘纪德,刘忠明,等. 钴基钎料钎焊DD5单晶高温合金的接头微观组织演变与力学性能研究[J]. 金属学报,2013,49(12):1581. doi: 10.3724/SP.J.1037.2013.00406SUN Y,LIU J D,LIU Z M,et al. Microstructure evolution and mechanical properties of DD5 single crystal superalloy joint brazed by Co-based filler alloy[J]. Acta Metallurgica Sinica,2013,49(12):1581. doi: 10.3724/SP.J.1037.2013.00406 [15] 孙元,侯星宇,金涛,等. DD5单晶高温合金钎焊接头的微观组织和力学性能分析[J]. 焊接学报,2017,38(1):117.SUN Y,HOU X Y,JIN T,et al. Microstructure and mechanical properties of DD5 single crystal superalloy brazing joint[J]. Transactions of the China Welding Institution,2017,38(1):117. [16] 侯星宇,孙元. 钎焊温度对CMSX-4单晶高温合金接头组织与性能的影响[J]. 焊接,2019(1):40.HOU X Y,SUN Y. Effect of brazing temperature on microstructure and mechanical properties of CMSX-4 single crystal superalloy brazed joint[J]. Welding & Joining,2019(1):40. [17] SUN Y,LIU J,LI B,et al. Microstructure evolution of single crystal superalloy DD5 joints brazed using AWS BNi-2 filler alloy[J]. Materials Research Innovations,2014,18(4):341. [18] 赵旭,孙元,侯星宇,等. 取向偏差对镍基单晶高温合金钎焊接头组织与力学性能的影响[J]. 金属学报,2020,56(2):46-56.ZHAO X,SUN Y,HOU X Y,et al. Effect of orientation deviation on microstructure and mechanical properties of nickel-based single crystal superalloy brazing joints[J]. Acta Metallurgica Sinica,2020,56(2):46-56. -