Thermal Deformation Behavior and Constitutive Equation of Highly Alloyed Superalloy Udimet720Li

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Abstract:

Hot compressive deformation of Udimet720Li alloy was carried out on Gleeble-3500 thermal mechanical simulator. The flow stress behavior of Udimet720Li alloy during hot compression was studied in the temperature range of 1100-1160 and at a strain rate of 0.001-1s -1. The results showed that the flow stress was controlled by both strain rate and deforming temperature. The flow stress decreased with the increase of deforming temperature, while increased with the increase of strain rate. The change of flow stress with deformation thermal parameters was revealed from true stress-true strain curves, and constitutive relationship of Udimet720Li alloy was obtained on the base of Arrhenius equations and the deformation activation energy was calculated.

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Materials Science Forum (Volumes 747-748)

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703-708

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February 2013

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© 2013 Trans Tech Publications Ltd. All Rights Reserved

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[1] H.T. Pang , P.A.S. Reed. Effects of microstructure on room temperature fatigue crack initiation and short crack propagation in Udimet 720Li Ni-base superalloy. International Journal of Fatigue 30(2008) 2009-(2020).

DOI: 10.1016/j.ijfatigue.2008.01.001

Google Scholar

[2] Y.S. Na, N.K. Park, R.C. Reed. Sigma morphology and precipitation mechanism in Udimet 720Li. Scripta mater. 43(2000)585-590.

DOI: 10.1016/s1359-6462(00)00441-3

Google Scholar

[3] S.W. Kando. Upcoming BR700 Core Tests to Focus on Endurance. Aviation Week & Space Technology, 6(1993) 53-54.

Google Scholar

[4] J.M. Hyzak. The Microstructural Response of As-HIP P/M U-720 to Thermomechanical Processing. In: S.D. Antolovich(Eds. ), Superalloys 1992, Warrendale, PA: TMS, 1992, pp.93-101.

DOI: 10.7449/1992/superalloys_1992_93_101

Google Scholar

[5] K.A. Green, J.A. Lemsky, R.M. Gasior. Development of Isothermally Forged P/M Udimet 720 for Turbine Disk Applications. In : R.D. Kissinger(Eds). Superalloys 1996, Warrendale, PA: TMS, 1996, pp.697-703.

DOI: 10.7449/1996/superalloys_1996_697_703

Google Scholar

[6] Y. Wang, W.Z. Shao, L. Zhen, B.Y. Zhang. Hot deformation behavior of delta-processed superalloy 718. Materials Science and Engineering A, 528(2011) 3218-3227.

DOI: 10.1016/j.msea.2011.01.013

Google Scholar

[7] J. Luo, M.Q. Li, D.W. Ma. The deformation behavior and processing maps in the isothermal compression of 7A09 aluminum alloy. Materials Science and Engineering A, 532(2012)548-557.

DOI: 10.1016/j.msea.2011.10.120

Google Scholar

[8] B. Liu, Y. Liua, W. Zhang, J.S. Huang. Hot deformation behavior of TiAl alloys prepared by blended elemental powders. Intermetallics, 19(2011)154-159.

DOI: 10.1016/j.intermet.2010.08.024

Google Scholar

[9] Lu Yalin, Li Xingcheng, Li Xiaoping, Zhu Fuxian. Deformation behavior and constitutive equation of AZ31 magnesium alloy at elevated temperature. Foundry Technology, 32(2011) 221-225.

Google Scholar