High Temperature Fatigue Performance of Electron Beam Powder Bed Fusion Manufactured Alloy 718

被引:3
作者
Kjellsson, Henrik [1 ]
Balachandramurthi, Arun Ramanathan [1 ]
Moverare, Johan [1 ,2 ]
Hansson, Thomas [1 ,3 ]
机构
[1] Univ West, Dept Engn Sci, S-46186 Trollhattan, Sweden
[2] Linkoping Univ, Dept Management & Engn, S-58183 Linkoping, Sweden
[3] GKN Aerosp Sweden AB, S-46181 Trollhattan, Sweden
来源
METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE | 2022年 / 53卷 / 07期
关键词
LOW-CYCLE FATIGUE; NICKEL-BASE SUPERALLOY; CRACK-PROPAGATION; GRAIN-STRUCTURE; HEAT-TREATMENT; BEHAVIOR; TEXTURE; MICROSTRUCTURE; PRECIPITATION; INCONEL-718;
D O I
10.1007/s11661-022-06681-7
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The microstructure and mechanical properties of additively manufactured (AM) parts have been shown to be different from that of cast and wrought counterparts. In this study, electron beam powder bed fusion (EB-PBF) fabricated Alloy 718 was exposed to three different heat treatment routes followed by strain-controlled fatigue testing at 550 degrees C. The fatigue tests were performed with specimens built with their center axis parallel and transverse relative to the build direction. The microstructure showed saturated precipitation of delta-Ni3Nb after repeated solution treatment at 954 degrees C. In contrast, no delta-Ni3Nb precipitates could be observed after a single-step solution treatment at 1025 degrees C. However, the disparity of secondary phases showed no noticeable influence on the fatigue life. A significant difference in fatigue behavior was noted between the parallel and transverse directions. The specimens loaded parallel to the elongated grains showed on average similar to 5x greater life in comparison to the perpendicularly loaded specimens. Compared to corresponding heat-treated material conditions tested at ambient temperature, the specimens showed lower life at high strain amplitude and superior life at low strain amplitude. Moreover, competitive internal and surface failure modes were observed at the lower strain amplitudes while for the higher strain ranges, surface failure modes dominated. (C) The Author(s) 2022
引用
收藏
页码:2496 / 2514
页数:19
相关论文
共 62 条
  • [1] [Anonymous], 2009, STAT ANAL FATIGUE DA, DOI DOI 10.1520/STP29332S,129-129-9
  • [2] [Anonymous], 2014, ASTM F3055-14a
  • [3] [Anonymous], 2012, ASTM STANDARD E606E6
  • [4] Effect of build geometry on the β-grain structure and texture in additive manufacture of Ti-6Al-4V by selective electron beam melting
    Antonysamy, A. A.
    Meyer, J.
    Prangnell, P. B.
    [J]. MATERIALS CHARACTERIZATION, 2013, 84 : 153 - 168
  • [5] Anisotropic fatigue properties of Alloy 718 manufactured by Electron Beam Powder Bed Fusion
    Balachandramurthi, Arun Ramanathan
    Moverare, Johan
    Hansson, Thomas
    Pederson, Robert
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 2020, 141 (141)
  • [6] Microstructural influence on fatigue crack propagation during high cycle fatigue testing of additively manufactured Alloy 718
    Balachandramurthi, Arun Ramanathan
    Moverare, Johan
    Dixit, Nikhil
    Deng, Dunyong
    Pederson, Robert
    [J]. MATERIALS CHARACTERIZATION, 2019, 149 : 82 - 94
  • [7] Additive Manufacturing of Alloy 718 via Electron Beam Melting: Effect of Post-Treatment on the Microstructure and the Mechanical Properties
    Balachandramurthi, Arun Ramanathan
    Moverare, Johan
    Mahade, Satyapal
    Pederson, Robert
    [J]. MATERIALS, 2019, 12 (01):
  • [8] Influence of defects and as-built surface roughness on fatigue properties of additively manufactured Alloy 718
    Balachandramurthi, Arun Ramanathan
    Moverare, Johan
    Dixit, Nikhil
    Pederson, Robert
    [J]. MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2018, 735 : 463 - 474
  • [9] Bhavar V, 2017, SYST INNOV SER, P251
  • [10] Bor H.-Y., 2010, SUPERALLOY 718 DERIV, P678