材料研究学报  2010, Vol. 24 Issue (6): 649-654

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热处理制度对GH706高温合金持久性能的影响

信昕1, 孙文儒1, 冯贞伟2, 祁峰1, 李晓光2, 杨洪才3, 胡壮麒1

1.中国科学院金属研究所 沈阳 110016 2.沈阳黎明发动机(集团)责任有限公司 沈阳 110043 3.东北大学材料与冶金学院 沈阳 110004

Effects of Heat Treatment on Stress Rupture Properties of GH706 Superalloy

XIN Xin1, SUN Wenru1, FENG Zhenwei2, QI Feng1, LI Xiaoguang2, YANG Hongcai3, HU Zhuangqi1

1.Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016 2.Shenyang Liming Aero-Engine Group Corporation. Shenyang 110043 3.School of Materials and Metallurgy, Northeastern University, Shenyang 110004

信昕 孙文儒 冯贞伟 祁峰 李晓光 杨洪才 胡壮麒. 热处理制度对GH706高温合金持久性能的影响[J]. 材料研究学报, 2010, 24(6): 649-654.
, , , , , , . Effects of Heat Treatment on Stress Rupture Properties of GH706 Superalloy[J]. Chin J Mater Res, 2010, 24(6): 649-654.

摘要 参考文献 相关文章 Metrics 全文: PDF(917 KB)   摘要: 不同热处理制度对GH706高温合金持久性能影响的研究结果表明, 固溶加低温时效的两段热处理使合金中析出的η相呈胞状紧密排列于晶界, 强化晶界,获得较长的持久寿命。增加稳定化处理的三段热处理合金, 晶界η相以长针状析出, 并在其周围形成γ'、γ''相贫化区, 贫化区强度较低, 弱化了晶界, 使得裂纹易于萌生, 且易于连通形成扩展通道, 降低了持久寿命。直接时效(DA)处理的合金中η相在晶界呈短棒状分散排列, 可以起到强化晶界的作用, 而η相间的无析出区可以钝化裂纹的萌生和扩展, 从而获得最长的持久寿命和最高的持久塑性。 关键词 ： 金属材料,  GH706高温合金,  热处理,  η相,  持久性能     Abstract：The stress rupture properties of GH706 superalloy at diffierent heat treatments are studied in precent work. For two-step treated GH706 alloy, cellular $ particles precipitate closely at the grain boundaries, strengthening grain boundaries, leading to the prolongation of the stress rupture life. In three-step alloy treated, the needle-like η phases are formed at the grain boundaries, which enlarge the area of the depleted zone of the γ' and γ'' strengthening phases. This zone characterizes with poor strength, which deteriorates grain boundaries. Cracks are prone to initate at γ' and γ'' depleted zone, then the cracks are easily to propagate. Consequently, the stress rupture life is reduced. For direct aging (DA) treated alloy, the rod-like η particles precipitate loosely at the grain boundaries, which makes grain boundary strengthening. The free precipitated phase zone is formed between η particles, which can passivates crack initiation and propagation. This may lead to the longest stress rupture life and the best rupture elongation of the DA GH706 alloy among three kind heat-treated alloys. Key words： metallic materials    GH706 superalloy    heat treatment    &eta    phase    stress rupture properties 收稿日期: 2010-04-09      ZTFLH:  TG14   服务 把本文推荐给朋友 加入引用管理器 E-mail Alert RSS 作者相关文章 信昕 孙文儒 杨洪才 胡壮麒 祁峰 贾丹 李晓光 44.8K 链接本文: https://www.cjmr.org/CN/      或      https://www.cjmr.org/CN/Y2010/V24/I6/649 1. P.W.Schilke, J.J.Pepe, R.C.Schwant, Alloy 706 metallurgy and turbine wheel application, in: Superalloys 718,625,706 and Various Derivatives, E.A.Loria ed., (Warrendale, PA, TMS-AIME, 1994)p.1 2. P.W.Schilke, R.C.Schwant, Alloy 706 use, process optimization, and future directions for GE gas turbine rotor materials, in: Superalloys 718,625,706 and Various Derivatives, E.A.Loria ed., (Warrendale, PA, TMS-AIME, 2001)p.25 3. LONG Zhengdong, The progress of Inconel 706 alloy abroad, Materials Review,5,14(1995) (龙正东，国外Inconel 706合金的研究进展．材料导报, 5,14(1995)) 4. XU Zhichao, QU Bo, XIE Xishan. Direct aging of alloy GH169, Journal of University of Science and Technology Beijing, 13(3) , 239(1991) (徐志超,屈波,谢锡善．GH169合金的DA处理，北京科技大学学报, 13(3)，239（1991）) 5. O.Matsumoto, T.Honjo, Y.Yasumoto, T.Moriyama, T.Tsuchiyama. Grain boundary precipitates and mechanical properties of alloy 706, in: Superalloys 718,625,706 and Various Derivatives, E.A.Loria ed., (Warrendale, PA, TMS-AIME, 1997)p.389 6. T.Takahashi, T.Ishiguro, K.Orita, J.Taira, T.Shibata, S.Nakata. Effects of grain boundary precipitation on creep rupture properties of alloys 706 and 718 turbine disk forgings, in: Superalloys 718,625,706 and Various Derivatives, E.A.Loria ed., (Warrendale, PA, TMS-AIME, 1994)p.557 7. J.H.Moll, G.N.Maniar, D.R.Muzyka. Heat treatment of 706 alloy for optimum 1200℉ stress-rupture properties, Metallurgical Transactions, 2, 2153(1971) 8. LI Xiuyan, ZHANG Jian, RONG Lijian, LI Yiyi. The precipitation mechanism of secondary η phase in a FeNi-based alloy, Chinese Journal of Materials Research, 20(2), 113(2006) (李秀艳,张建,戎利建,李依依．Fe-Ni基合金中次生η相的析出机理，材料研究学报，20(2), 113(2006)) [1] 毛建军, 富童, 潘虎成, 滕常青, 张伟, 谢东升, 吴璐. AlNbMoZrB系难熔高熵合金的Kr离子辐照损伤行为[J]. 材料研究学报, 2023, 37(9): 641-648. [2] 宋莉芳, 闫佳豪, 张佃康, 薛程, 夏慧芸, 牛艳辉. 碱金属掺杂MIL125的CO2 吸附性能[J]. 材料研究学报, 2023, 37(9): 649-654. [3] 赵政翔, 廖露海, 徐芳泓, 张威, 李静媛. 超级奥氏体不锈钢24Cr-22Ni-7Mo-0.4N的热变形行为及其组织演变[J]. 材料研究学报, 2023, 37(9): 655-667. [4] 邵鸿媚, 崔勇, 徐文迪, 张伟, 申晓毅, 翟玉春. 空心球形AlOOH的无模板水热制备和吸附性能[J]. 材料研究学报, 2023, 37(9): 675-684. [5] 幸定琴, 涂坚, 罗森, 周志明. C含量对VCoNi中熵合金微观组织和性能的影响[J]. 材料研究学报, 2023, 37(9): 685-696. [6] 欧阳康昕, 周达, 杨宇帆, 张磊. 含LPSO相Mg-Y-Er-Ni合金的组织和拉伸性能[J]. 材料研究学报, 2023, 37(9): 697-705. [7] 徐利君, 郑策, 冯小辉, 黄秋燕, 李应举, 杨院生. 定向再结晶对热轧态Cu71Al18Mn11合金的组织和超弹性性能的影响[J]. 材料研究学报, 2023, 37(8): 571-580. [8] 熊诗琪, 刘恩泽, 谭政, 宁礼奎, 佟健, 郑志, 李海英. 固溶处理对一种低偏析高温合金组织的影响[J]. 材料研究学报, 2023, 37(8): 603-613. [9] 刘继浩, 迟宏宵, 武会宾, 马党参, 周健, 徐辉霞. 喷射成形M3高速钢热处理过程中组织的演变和硬度偏低问题[J]. 材料研究学报, 2023, 37(8): 625-632. [10] 由宝栋, 朱明伟, 杨鹏举, 何杰. 合金相分离制备多孔金属材料的研究进展[J]. 材料研究学报, 2023, 37(8): 561-570. [11] 任富彦, 欧阳二明. g-C3N4 改性Bi2O3 对盐酸四环素的光催化降解[J]. 材料研究学报, 2023, 37(8): 633-640. [12] 王昊, 崔君军, 赵明久. 镍基高温合金GH3536带箔材的再结晶与晶粒长大行为[J]. 材料研究学报, 2023, 37(7): 535-542. [13] 刘明珠, 樊娆, 张萧宇, 马泽元, 梁城洋, 曹颖, 耿仕通, 李玲. SnO2 作散射层的光阳极膜厚对量子点染料敏化太阳能电池光电性能的影响[J]. 材料研究学报, 2023, 37(7): 554-560. [14] 秦鹤勇, 李振团, 赵光普, 张文云, 张晓敏. 固溶温度对GH4742合金力学性能及γ' 相的影响[J]. 材料研究学报, 2023, 37(7): 502-510. [15] 刘天福, 张滨, 张均锋, 徐强, 宋竹满, 张广平. 缺口应力集中系数对TC4 ELI合金低周疲劳性能的影响[J]. 材料研究学报, 2023, 37(7): 511-522. Viewed Full text Abstract Cited   Shared      Discussed