[1]
Buzolits S R, Kline L A. Bolting alloy fills high-temperature gap [J]. Advanced Materials and Processes, 1995, 147(2): 33.
Google Scholar
[2]
Asgari S. Age-hardening behavior and phase identification in solution-treated AEREX 350 superalloy [J]. Metallurgical and Materials Transactions A, 2006, 37A (7): (2051).
DOI: 10.1007/bf02586125
Google Scholar
[3]
Kermajani M. Influence of double aging on microstructure and yield strength of AEREXTM 350 [J]. Materials Science and Engineering A, 2012, 534: 547.
DOI: 10.1016/j.msea.2011.12.006
Google Scholar
[4]
Jiang H, Yang J, Dong J X, Zhang M C, Yao Z H, Xie X X. Stress Relaxation Behavior Comparison of Typical Nickel-Base Superalloys for Fasteners [A]. Proceedings of the 9th International Symposium on Superalloy 718 Derivatives [C]. Pittsburgh: TMS, 2018. 789.
DOI: 10.1007/978-3-319-89480-5_53
Google Scholar
[5]
Hosseinifar M, Asgari S. Static recrystallization behavior of AEREX350 superalloy [J]. Materials Science and Engineering A, 2010, 527(27-28): 7313.
DOI: 10.1016/j.msea.2010.08.005
Google Scholar
[6]
Samiee M, Asgari S. A TEM investigation on precipitation behavior of AEREX350 superalloy [A]. 11th International Symposium on superalloys. Superalloys 2008 [C]. Champion: TMS, 2008. 549.
DOI: 10.7449/2008/superalloys_2008_549_552
Google Scholar
[7]
Farvizi M, Asgari S. Effects of cold work prior to aging on microstructure of AEREX350TM superalloy [J]. Materials Science and Engineering A, 2008, 480(1-2): 434.
DOI: 10.1016/j.msea.2007.07.052
Google Scholar
[8]
Li K.M, Han G.W, Deng B. Influence of Aging Treatment on Microstructure and Properties of Cold-drawn Alloy GH350 [J]. Acta Aeronauticaet Astronautica Sinica, 2012, 33(6): 1156.
Google Scholar
[9]
Wang X.C, Cao M.J. Research and Development of Cold Drawing Bar of GH350 Alloy Used for Fasteners with High Temperature Property and Ultra High Strength [J]. Special Steel Technology, 2015, 21(4): 13.
Google Scholar
[10]
Zhu H.C, Luo J.M, Zhu Z.S. High temperature compression deformation behavior of TB17 titanium alloy[J]. Journal of Aeronautical Materials, 2019, 39 (3): 44.
Google Scholar
[11]
Ye Z,Gao Y K. Study on residual stress of hot die forging for alloy GH4169 turbine disc based on DEFORM-2D [J]. Fording & Stamping Technology, 2018, 43(3): 1.
Google Scholar
[12]
Pan P, Li Q, Li J.C, Wu B, Zhong H.T. Optimization of hot upsetting forming parameters of A286 superalloy hexagonal headed bolt head for high-speed train [J]. Forging and Stamping Technology, 2020, 45(3): 62.
Google Scholar
[13]
Gao Q.W. Research of Hot Upsetting ProcesS for Exagon Headed Holt of Superalloy GH4698 [D]. Harbin: Harbin Institute of Technology, 2015. 32.
Google Scholar
[14]
Huang J.F, Yan F. Development of Bolt Made of GH159(MP159) High Temperature Alloy [A]. The 2nd China Aeronautical Science and Technology Conference [C]. Beijing, 2015. 217.
Google Scholar
[15]
HU S.S, CHEN Y.H. Effect of electromagnetic riveting loading voltage on adiabatic shear deformation of TA1 rivet [J]. Journal of Plasticity Engineering, 2020, 27 (12): 121.
Google Scholar
[16]
HAO Z.P, JI F.F, FAN Y.H, WANG T. Micro-characteristic of Adiabatic Shear Band in High-speed Machining Inconel718 [J]. Modular Machine Tool & Automatic Manufacturing Technique, 2018, (6): 15.
Google Scholar
[17]
XU X.F, WANG L, CHENG X.W, et.al. Research on high temperature mechanical property and microstructure of Ti6321 titanium alloy [J]. Chinese Journal of Stereology and Image Analysis, 2019, 24(2):118.
Google Scholar