Low Cycle Fatigue Properties of Nickel Base Single Crystal Superalloy at Different Temperatures
摘 要
研究了Ni-Cr-Co-Mo-W-Ta-Nb-Re-Al-Hf-C系镍基单晶高温合金在不同温度(800,980 ℃)下的低周疲劳性能。结果表明:与800 ℃下相比,980 ℃下合金的塑性变形量更大,损伤更严重,疲劳强度更低,寿命更短;2种温度下合金的疲劳断裂均为类解理断裂;800 ℃时,裂纹萌生于疏松组织处,沿{111}平面扩展,瞬断区面积较大,980 ℃时,裂纹萌生于脆性氧化皮处,沿与应力轴垂直的{001}平面扩展,瞬断区面积较小。
Abstract
The low cycle fatigue properties of the Ni-Cr-Co-Mo-W-Ta-Nb-Re-Al-Hf-C series single crystal superalloy at different temperatures (800, 980℃) were studied. The results show that compared with those at 800℃, the plastic deformation of the alloy at 980℃ was greater, the damage was more serious, the fatigue strength was lower, and the life was shorter. The fatigue fractures of the alloys at two temperatures were cleavage-like fractures. At 800℃, the crack initiated at the loose microstructure and propagated along the {111} plane, and the instantaneous fracture area was relatively large. At 980℃, the crack initiated at the brittle oxide scale and propagated along the {001} plane perpendicular to the stress axis, and the instantaneous fracture area was relatively small.
中图分类号 TG132.3 DOI 10.11973/jxgccl202103004
所属栏目 试验研究
基金项目
收稿日期 2020/4/13
修改稿日期 2021/1/5
网络出版日期
作者单位点击查看
备注史振学(1975-),男,山东曲阜人,高级工程师,博士
引用该论文: SHI Zhenxue,HU Yingtao,LIU Shizhong. Low Cycle Fatigue Properties of Nickel Base Single Crystal Superalloy at Different Temperatures[J]. Materials for mechancial engineering, 2021, 45(3): 16~20
史振学,胡颖涛,刘世忠. 不同温度下镍基单晶高温合金的低周疲劳性能[J]. 机械工程材料, 2021, 45(3): 16~20
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参考文献
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【2】史振学,王效光,杨万鹏,等.热暴露温度对单晶高温合金持久性能的影响[J].金属热处理,2018,43(5):1-5. SHI Z X,WANG X G,YANG W P,et al. Effect of thermal exposure temperature on stress rupture properties of single crystal superalloy[J]. Heat Treatment of Metals, 2018, 43(5):1-5.
【3】CARON P,KHAN T.Evolution of Ni-based superalloys for single crystal gas turbine blade applications[J].Aerospace Science and Technology,1999,3(8):513-523.
【4】ARGENCE D,VERNAULT C,DESVALLEES Y,et al. MC-NG:A 4th generation single-crystal superalloy for future aeronautical turbine blades and vanes[C]//Superalloys Ninth International Symposium.[S.l.]:ACM, 2000.
【5】WALSTON S,CETEL A,MACKAY R,et al.Joint development of a fourth generation single crystal superalloy[C]//Superalloys Tenth International Symposium.[S.l.]:ACM, 2004.
【6】谢洪吉. DD6单晶高温合金疲劳性能研究[D]. 北京:北京航空材料研究院,2018. XIE H J. The fatigue properties of DD6 single crytal superallouy[D]. Beijing:Beijing Institute of Aeronautical Materials, 2018.
【7】谢洪吉,李嘉荣,韩梅,等.超温对DD6单晶高温合金组织及高周疲劳性能影响[J].稀有金属材料与工程,2018,47(8):2483-2488. XIE H J, LI J R, HAN M, et al. Effect of over-temperature on microstructure and high cycle fatigue properties of DD6 single crystal superalloy[J]. Rare Metal Materials and Engineering, 2018, 47(8):2483-2488.
【8】MULLER S,ROSLER J,SOMMER C,et al.The influence of load ratio,temperature,orientation and hold time on fatigue crack growth of CMSX-4[C]//Superalloys Ninth International Symposium.[S.l.]:ACM, 2000.
【9】SHI Z X,WANG X G,LIU S Z,et al.Low cycle fatigue properties and microstructure evolution at 760℃ of a single crystal superalloy[J].Progress in Natural Science:Materials International,2015,25(1):78-83.
【10】张志华,于慧臣,李影,等.单晶镍基高温合金在600~760℃下的低循环疲劳行为[J].航空材料学报,2018,38(3):58-64. ZHANG Z H, YU H C, LI Y, et al. Low cycle fatigue behaviors of single crystal nickel-based superalloy at temperatures of 600-760℃[J]. Journal of Aeronautical of Materials, 2018,38(3):58-64.
【11】ZHOU H,RO Y,HARADA H,et al.Deformation microstructures after low-cycle fatigue in a fourth-generation Ni-base SC superalloy TMS-138[J].Materials Science and Engineering:A,2004,381(1/2):20-27.
【12】罗辅欢,卿华,田洪宇,等.一种考虑各向异性的DD6单晶高温合金低周疲劳寿命预测方法[J].燃气涡轮试验与研究,2019,32(6):41-44. LUO F H, QING H, TIAN H Y, et al. A method for predicting low cycle fatigue life of single-crystal high temperature alloy DD6 with anisotropy[J].Gas Turbine Experiment and Research, 2019, 32(6):41-44.
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【14】刘维维,唐定中,李嘉荣,等.抽拉速率对DD6单晶高温合金650℃低周疲劳性能的影响[J].航空材料学报,2012,32(2):8-12. LIU W W, TANG D Z, LI J R, et al. Effects of withdrawing rate on low cycle fatigue properties of single crystal superalloy DD6 at 650℃[J]. Journal of Aeronautical of Materials, 2012, 32(2):8-12.
【15】WAN J S,YUE Z F.A low-cycle fatigue life model of nickel-based single crystal superalloys under multiaxial stress state[J].Materials Science and Engineering:A,2005,392(1/2):145-149.
【16】WASSON A J,FUCHS G E.The effect of carbide morphologies on elevated temperature tensile and fatigue behavior of a modified single crystal Ni-base superalloy[C]//Superalloys Eleventh International Symposium.[S.l.]:ACM, 2008.
【17】史振学,李嘉荣,刘世忠,等.第二代单晶高温合金的低周疲劳行为[J].材料热处理学报,2011,32(5):41-45. SHI Z X, LI J R, LIU S Z, et al. Low cycle fatigue behavior of a second generation single crystal superalloy DD6 at high temperature[J]. Transactions of Materials and Heat treatment, 2011, 32(5):41-45.
【18】钟群鹏,赵子华.断口学[M].北京:高等教育出版社,2006. ZHONG Q P, ZHAO Z H. Fractography[M]. Beijing:Higher Education Press, 2006.
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