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材料研究学报  2016, Vol. 30 Issue (6): 465-472    DOI: 10.11901/1005.3093.2016.101
  研究论文 本期目录 | 过刊浏览 |
元素V对镍基柱状晶合金显微组织和高温蠕变性能的影响
于兴福1(), 周金华1, 吴玉超1, 杨月1, 王宇飞2, 满延林2, 黄爱华3
1. 沈阳工业大学材料科学与工程学院 沈阳 110870
2. 沈阳中航动力精密铸造科技有限公司 沈阳 110043
3. 中航商用航空发动机有限责任公司 上海 200241
Effect of V on Microstructure and High Temperature Creep Properties of Diretional Solidified Nickel-base Superalloys
YU Xingfu1,*(), ZHOU Jinhua1, WU Yuchao1, YANG Yue1, WANG Yufei2, MAN Yanlin2, HUANG Aihua3
1. School of Materials Science and Engineering, Shenyang University of Technology, Shenyang 110870, China
2. AVIC Power Shenyang Investment Casting Technology Co. Ltd., Shenyang 110043, China
3. AVIC Commercial Aircraft Engine Co., Ltd., Shanghai 200241, China
引用本文:

于兴福, 周金华, 吴玉超, 杨月, 王宇飞, 满延林, 黄爱华. 元素V对镍基柱状晶合金显微组织和高温蠕变性能的影响[J]. 材料研究学报, 2016, 30(6): 465-472.
Xingfu YU, Jinhua ZHOU, Yuchao WU, Yue YANG, Yufei WANG, Yanlin MAN, Aihua HUANG. Effect of V on Microstructure and High Temperature Creep Properties of Diretional Solidified Nickel-base Superalloys[J]. Chinese Journal of Materials Research, 2016, 30(6): 465-472.

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摘要: 

采用定向凝固炉制备出含有不同V含量的柱状晶合金, 进行了高温蠕变性能测试和微观组织形貌观察, 研究合金化元素V对镍基柱状晶合金微观组织及高温蠕变性能的影响。结果表明: 低V含量的合金中碳化物主要以棒状形式存在, 而高V合金中碳化物主要以块状形式存在, 棒状碳化物中的V含量低于块状碳化物。随V含量的增加, 合金中碳化物由棒状向块状转变, 当V含量达到1.04%(质量分数)时, 碳化物的形貌已经完全转变成块状。铸态合金经固溶处理后, 合金中的碳化物发生溶解, 低V合金中的棒状碳化物溶解较多, 而高V合金中碳化物溶解较少。在980℃/216 MPa和760℃/725 MPa条件下低V柱状晶合金持久寿命较短, 高V合金持久寿命较长, 提高合金中的V含量有利于提高合金的蠕变寿命。高V合金与低V合金相比, 时效和蠕变期间在晶界析出M23C6型碳化物数量少。蠕变期间合金中的裂纹主要在晶内MC型碳化物及晶界析出的M23C6型碳化物处萌生和扩展。

关键词 金属材料V元素作用微观组织镍基合金蠕变    
Abstract

The effect of alloying element V on the microstructure and high temperature creep properties of a diretional solidified nickel-base superalloy was researched by varying the amount of V addition. The alloy composition was set in a controlled fixedness except for element V, and then the effect of V can be assessed. The alloys were directionally solidified by utilizing Bridgeman casting process and followed by appropriate post heat treatment. The microstructure and high temperature creep properties of the prepared alloys were then characterized. The results shown that, with lower amount of V addition, the alloying V existed mainly in acicular type carbides rather than in blocky type carbides; while for the higher addition of V, the shape of vanadium carbides in the alloys transition from acicular type to blocky type. When the V content reaches 1.04 % in the alloy, the shape of carbides has been transformed into blocky type completely. After solid solution treatment, the carbides in the alloy were dissolved partly, and the acicular carbides in the alloy with lower V content dissolved much more than the blocky carbides in high V content alloy. Under the condition of 980℃/216 MPa and 760℃/725 MPa, the stress rupture life is shorter for the alloy with lower V content, but loger for that with higher V content. The amount of M23C6 type carbide precipitated at grain boundaries in the alloy with higher V content is less than that with lower V content during creep test and aging heat treatment. During creep test, cracks initiate and grow mainly at the MC type carbide within grains or the M23C6 type carbides precipitated at the grain boundaries. Therefore, the increase of V content is of benefit for the improvement of creep life of the alloy.

Key wordsmetallic materials    effect of vanadium    microstructure    nickel-base alloy    creep
收稿日期: 2016-02-25     
ZTFLH:  TG146.1  
作者简介: 本文联系人: 于兴福
C Cr Al Mo Ti Co V B Ni
Alloy 1 0.147 9.03 5.22 3.05 4.67 10.23 0.62 0.015 Bal.
Alloy 2 0.145 9.01 5.26 3.04 4.67 10.24 0.96 0.016 Bal.
Alloy 3 0.146 9.00 5.28 3.06 4.65 10.23 1.04 0.015 Bal.
表1  定向凝固合金棒的主要化学成分
图1  片状蠕变试样示意图
图2  镍基柱状晶合金中碳化物形貌
图3  合金中γ'相形貌
图4  固溶处理后合金中碳化物形貌
图5  完全热处理后合金中晶界析出的碳化物形貌
图6  碳化物形貌及EDAX能谱分析曲线
图7  铸态合金萃取物的XRD谱
图8  980℃/216 MPa条件下不同V含量合金的蠕变曲线
图9  760℃/725 MPa条件下不同V含量合金的蠕变曲线
Co Cr Ti Al Mo V Ni
Alloy1 Rod like carbide 10.68 9.97 6.94 4.45 4.48 0.56 Bal.
Bulk like carbide 0.09 2.24 57.1 -- 32.8 4.60 Bal.
Matrix 11.03 9.26 4.66 4.36 2.16 0.36 Bal.
Alloy3 Bulk like carbide -- 1.87 66.5 -- 21.8 6.96 Bal.
Matrix 10.60 8.92 4.95 4.76 2.83 0.79 Bal.
表2  合金中各相的化学成分
图10  蠕变期间碳化物的分解
图11  裂纹沿碳化物形成形貌
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