参考文献(References):
[1] 杨明辉.航空发动机用高温材料的应用及发展趋势研究[J].中国战略新兴产业,2019 (12):164-165.
[2] ARGENCE D,VEMAULT C,DESVALLCES Y,et al.MC-NG:a 4th generation single-crystal superalloy for future aeronautical turbine blades and vanes[M]// Superalloys 2000.New Jersey:John Wiley & Sons,2000:829-837.
[3] WALSTON S,CETEL A,MACKAY R,et al.Joint development of a fourth generation single crystal superalloy[M]// Superalloys 2004.New Jersey:John Wiley & Sons,2004:15-24.
[4] 孙晶霞.一种镍基单晶高温合金组织稳定性及持久性能的研究[D].沈阳:沈阳工业大学,2019.
[5] 岳全召,刘林,杨文超,等.先进镍基单晶高温合金蠕变行为的研究进展[J].材料导报,2019,33(3):479-489.
[6] 张健,王莉,王栋,等.镍基单晶高温合金的研发进展[J].金属学报,2019,55(9):1077-1094.
[7] SATO A,HARADA H,YOKOKAWA T,et al.The effects of ruthenium on the phase stability of fourth generation Ni-base single crystal superalloys[J].Scripta Materialia,2006,54(9):1679-1684.
[8] CELEL A D,DUHL D N.Second-generation nickel-base single crystal superalloy[M]// Superalloys 1988.New Jersey:John Wiley & Sons,1988:235-244.
[9] 赵乃仁,王志辉,李金国,等.一种镍基单晶高温合金的各向异性研究[J].材料工程,2008(2):58-61.
[10] ANTOLOVICH B F,SAXENA A,ANTOLOVICH S D.Fatigue crack propagation in single-crystal CMSX-2 at elevated temperature[J].Journal of Materials Engineering and Performance,1993,2(4):489-495.
[11] 李嘉荣,史振学,袁海龙,等.单晶高温合金DD6拉伸性能各向异性[J].材料工程,2008 (12):6-10.
[12] 张龙飞,燕平,赵京晨,等.DD407单晶高温合金760 ℃拉伸性能的各向异性[J].钢铁研究学报,2011,23(12):54-59.
[13] 王效光,李嘉荣,喻健,等.DD9单晶高温合金拉伸性能各向异性[J].金属学报,2015,51(10):1253-1260.
[14] 史振学,刘世忠,李嘉荣.一种第四代单晶高温合金不同温度的拉伸性能各向异性[J].航空材料学报,2019,39(4):78-85.
[15] SIEB?RGER D,KNAKE H,GLATZEL U.Temperature dependence of the elastic moduli of the nickel-base superalloy CMSX-4 and its isolated phases[J].Materials Science and Engineering:A,2001,298(1/2):26-33.
[16] 刘金来,叶荔华,周亦胄,等.一种单晶高温合金的弹性性能的各向异性[J].金属学报,2020,56(6):855-862.
[17] SHAH D M,DUHL D N.The effect of orientation,temperature and gamma prime size on the yield strength of a single crystal nickel base superalloy[M]//Superalloys 1984.New Jersey:John Wiley & Sons,1984:105-114.
[18] YANG W P,LI J R,LIU S Z,et al.Orientation dependence of transverse tensile properties of nickel-based third generation single crystal superalloy DD9 from 760 to 1 100 ℃[J].Transactions of Nonferrous Metals Society of China,2019,29(3):558-568.
[19] DALAL R P,THOMAS C R,DARDI L E.The effect of crystall-ographic orientation on the physical and mechanical properties of an investment cast single crystal nickel-base superalloy[M]// Superalloys 1984.New Jersey:John Wiley & Sons,1984:185-197.
[20] MILLIGAN W W,ANTOLOVICH S D.Yielding and deformation behavior of the single crystal superalloy PWA1480[J].Metallurgical Transactions:A,1987,18(1):85-95.
[21] 张龙飞,燕平,赵京晨,等.DD407单晶高温合金980 ℃/260 MPa持久蠕变的各向异性[J].钢铁研究学报,2011,23(增刊2):333-336.
[22] 王开国,李嘉荣,刘世忠,等.DD6单晶高温合金980 ℃蠕变性能研究[J].材料工程,2004(8):7-11.
[23] WEN Z X,ZHANG D X,LI S W,et al.Anisotropic creep damage and fracture mechanism of nickel-base single crystal super-alloy under multiaxial stress[J].Journal of Alloys and Compounds,2017,692:301-312.
[24] SASS V,GLATZEL U,FELLER-KNIEPMEIER M.Anisotropic creep properties of the nickel-base superalloy CMSX-4[J].Acta Materialia,1996,44(5):1967-1977.
[25] 韩国明,于金江,孙晓峰,等.一种镍基单晶高温合金持久各向异性行为[J].稀有金属材料与工程,2011,40(4):673-676.
[26] 李一飞.一种第三代镍基单晶高温合金蠕变各向异性的研究[D].合肥:中国科学技术大学,2019.
[27] 张中奎,王佰智,刘大顺,等.DD6单晶合金蠕变特性及断裂机理[J].材料科学与工程学报,2012,30(3):375-379.
[28] 夏永发,金玉龙.镍基单晶高温合金γ′颗粒[111]取向加载的粗化趋势[J].东北大学学报(自然科学版),2008,29(7):1053-1056.
[29] AGUDO JáCOME L,N?RTERSH?USER P,SOMSEN C,et al.On the nature of γ′ phase cutting and its effect on high temperature and low stress creep anisotropy of Ni-base single crystal superalloys[J].Acta Materialia,2014,69:246-264.
[30] LI Y F,WANG L,ZHANG G,et al.Anisotropic stress rupture properties of a 3rd-generation nickel-based single-crystal super-alloy at 1 100 ℃/150 MPa[J].Acta Metallurgica Sinica (English Letters),2020,33(3):446-458.
[31] 史振学,刘世忠,赵金乾,等.DD15单晶高温合金持久性能各向异性[J].钢铁研究学报,2021,33(2):168-174.
[32] 陈吉平,丁智平,尹泽勇,等.DD3镍基单晶合金低周疲劳寿命研究[J].机械工程材料,2006,30(4):9-12,16.
[33] 马显锋.用于大型燃气轮机的镍基单晶合金高温低周疲劳性能研究[D].北京:清华大学,2010.
[34] KLINGELH?FFER H,EPISHIN A,LINK T,et al.Low cycle fatigue of the single-crystal nickel-base superalloy CMSX-4:ani-stropy and effect of creep damage[J].Materials Testing,2008,51(5):291-294.
[35] 刘柳.一种镍基单晶高温合金低周疲劳行为的研究[D].沈阳:东北大学,2016.
[36] GABB T P,GAYDA J,MINER R V.Orientation and temperature dependence of some mechanical properties of the single-crystal nickel-base superalloy René N4:part II:low cycle fatigue behavior[J].Metallurgical Transactions:A,1986,17(3):497-505.
[37] CHIERAGATTI R,REMY L.Influence of orientation on the low cycle fatigue of MAR-M 200 single crystals at 650 ℃:II:cyclic stress-strain behaviour[J].Materials Science and Engineering:A,1991,141(1):11-22.
[38] GABB T P,WELSCH G,MINER R V,et al.The low cycle fatigue deformation response of a single-crystal superalloy at 650 ℃[J].Materials Science and Engineering:A,1989,108(1):189-202.
[39] YU J J,SUN Y L,SUN X F,et al.Anisotropy of high cycle fatigue behavior of a Ni-base single crystal superalloy[J].Materials Science and Engineering:A,2013,566:90-95.
[40] 中国金属学会高温材料分会.高温合金手册[M].北京:中国标准出版社,2012.
[41] 史振学,刘世忠,赵金乾,等.晶体取向对第四代单晶高温合金DD15高周疲劳性能的影响[J].航空制造技术,2021,64(1/2):51-56,61.