Effect of different drilling techniques on high-cycle fatigue behavior of nickel-based single-crystal superalloy with film cooling hole

被引:16
作者
Zhang, Zhijin [1 ]
Zhang, Mingqi [1 ]
机构
[1] AVIC Mfg Technol Inst, Dept 102, Beijing 100024, Peoples R China
基金
中国国家自然科学基金;
关键词
single-crystal superalloy; film-cooling hole; high-cycle fatigue (HCF); LIFE PREDICTION; PERFORMANCE;
D O I
10.1515/htmp-2020-0072
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The flat plate specimens of nickel-based single-crystal superalloy with 14 film cooling holes, which made by different drilling techniques, were used to study the high-cycle fatigue (HCF) properties at 980 degrees C in an ambient atmosphere. At the same time, the electrical discharge machining (EDM) specimens with a single hole were also used to study the HCF properties under different temperatures. The hole and fracture micrographs were analyzed by scanning electron microscope. The results indicated that different drilling techniques have a great influence on HCF life. The fatigue limit of the millisecond laser drilling is 353MPa, while the EDM is 359MPa and the electro-stream machining (ESM) is 378MPa. The fatigue life decreases gradually with the temperature increasing. The fatigue limit of EDM specimens with a single hole at 900 degrees C, 980 degrees C, and 1,050 degrees C are 472, 430, and 293MPa, respectively. The destruction of the specimens is a typical multisource rupture, and the fracture morphology includes three parts: the cracks sources around the film cooling hole, the propagation zone along the {001} planes, and instant rupture zone along the {111} planes.
引用
收藏
页码:121 / 130
页数:10
相关论文
共 25 条
  • [1] ASTM, 1996, ANN BOOK ASTM STANDA, V03
  • [2] Boyuan F., 1998, T CSICE, V4, P46
  • [3] China Aviation Industry Corporation, 1996, METAL MAT AXIAL LOAD
  • [4] Ascertaining life cycle inventory data for electrical discharge machining
    Gamage, Janaka R.
    DeSilva, Anjali K. M.
    Harrison, Colin
    Harrison, David
    [J]. RESEARCH AND INNOVATION IN MANUFACTURING: KEY ENABLING TECHNOLOGIES FOR THE FACTORIES OF THE FUTURE - PROCEEDINGS OF THE 48TH CIRP CONFERENCE ON MANUFACTURING SYSTEMS, 2016, 41 : 908 - 913
  • [5] APPLICATION OF FRACTURE MECHANICS TO LIFE PREDICTION OF COOLING HOLE CONFIGURATIONS IN THERMAL-MECHANICAL FATIGUE
    GEMMA, AE
    PHILLIPS, JS
    [J]. ENGINEERING FRACTURE MECHANICS, 1977, 9 (01) : 25 - 36
  • [6] Small-scale specimen testing for fatigue life assessment of service-exposed industrial gas turbine blades
    Hollaender, D.
    Kulawinski, D.
    Weidner, A.
    Thiele, M.
    Biermann, H.
    Gampe, U.
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 2016, 92 : 262 - 271
  • [7] A comparative study on thermomechanical and low cycle fatigue failures of a single crystal nickel-based superalloy
    Hong, H. U.
    Kang, J. G.
    Choi, B. G.
    Kim, I. S.
    Yoo, Y. S.
    Jo, C. Y.
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 2011, 33 (12) : 1592 - 1599
  • [8] EDM Drilling and Shaping of Cooling Holes in Inconel 718 Turbine Blades
    Kliuev, M.
    Boccadoro, M.
    Perez, R.
    Dal Bo, W.
    Stirnimann, J.
    Kuster, F.
    Wegener, K.
    [J]. 18TH CIRP CONFERENCE ON ELECTRO PHYSICAL AND CHEMICAL MACHINING (ISEM XVIII), 2016, 42 : 322 - 327
  • [9] Failure analysis of gas turbine rotor blades
    Kumari, Sweety
    Satyanarayana, D. V. V.
    Srinivas, M.
    [J]. ENGINEERING FAILURE ANALYSIS, 2014, 45 : 234 - 244
  • [10] Effect of film cooling on the aerodynamic performance of an airfoil
    Lanzillotta, Francesco
    Sciacchitano, Andrea
    Rao, Arvind Gangoli
    [J]. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2017, 66 : 108 - 120