Fatigue Behavior and Surface Sensitivity of Board-Shaped Sample of Powder Metallurgy FGH 96

Article Preview

Abstract:

Powder metallurgy superalloy (P/M superalloy) was developed following the development of turbine engine disc, and it was usually characterized the mechanical behavior using rod specimen . Up to mow, P/M superalloy has not only been the primary material of turbine disc but also the main material of thin plate components. It is insufficient only to carry out mechanical property of rod-shaped samples. In this paper, the fatigue performance and surface sensitivity of powder metallurgy alloys of two kinds of powder (AA powder and PREP powder) were studied. Tensile fatigue tests were carried out for studying the changing law of tensile fatigue behaviors using plate-shaped and rod-shaped samples with shot peening and without shot peening. The surface sensibility of plate specimens was also analyzed according to the fatigue behaviors and crack initiation sites.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 891-892)

Pages:

1723-1728

Citation:

Online since:

March 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] BARRIE R L, GABB T P, TELESMAN J. Effectiveness of shot peening in suppressing fatigue cracking at non-metallic inclusions in Udimet 720. Materials Science and Engineering, 2008, 474: 71-81.

DOI: 10.1016/j.msea.2007.03.100

Google Scholar

[2] H U Hong, I S Kim, B G Choi, H E Jeong, C Y Jo. Effects of temperature and strain range on fatigue cracking behavior in Hastelloy X. Materials Letters, 2008: 4351-4353.

DOI: 10.1016/j.matlet.2008.07.032

Google Scholar

[3] Sophile dubiez Le Goif, Raphael Couturier, Laure Guetaz, et al. Modelling the plastic deformation during high-temperature creep of a powder-metallurgy coarse-grained superalloy. Materials Science and Engineering 2008. A(483-484): 598-601.

DOI: 10.1016/j.msea.2006.10.186

Google Scholar

[4] LEE K O, BAE K H, LEE S B. Comparison of prediction methods for low-cycle fatigue life of HIP superalloys at elevated temperature for turbopump reliability. Materials Science and Engineering A, 2009, 519: 112-120.

DOI: 10.1016/j.msea.2009.04.044

Google Scholar

[5] HURON E S, BAIN K R, MOURER D P, et al. Development of high temperature capability p/M disk superalloys [C] / REED R C, GREEN K A, CARON P, et al. Superalloys 2008, Pennsylvania: TMS, 2008: 181-189.

DOI: 10.7449/2008/superalloys_2008_181_189

Google Scholar

[6] Pineau A, Antolovich SD. High temperature fatigue of nickel-base superalloys- a review with special emphasis on deformation modes and oxidation. Eng Fail Anal 2009, 16: 2668-2697.

DOI: 10.1016/j.engfailanal.2009.01.010

Google Scholar

[7] Leo Prakash DG, Walsh MJ, Maclachlan D, Korsunsky AM. Crack growth micro-mechanisms in the IN718 alloy under the combined influence of fatigue, creep and oxidation. Int J Fatigue 2009, 31: 1966-(1977).

DOI: 10.1016/j.ijfatigue.2009.01.023

Google Scholar

[8] M.J. Caton, S.K. Jha. Small fatigue crack growth and failure mode transitions in a Ni-base superalloy at elevated temperature. International Journal of Fatigue , 2010, 32: 1461-1472.

DOI: 10.1016/j.ijfatigue.2010.01.015

Google Scholar

[9] A. Shyam, C. J. Torbet, C. J. Szczepanski, S. K. Jha, M. J. Caton, J. M. Larsen, T. M. Pollock, J. W. Jones. Ultrasonic fatigue of a nickel-base turbine disk alloy at room and elevated temperatures. 2004 Materials Science and Technology Conference, 2005: 247.

DOI: 10.7449/2004/superalloys_2004_259_268

Google Scholar

[10] By Hans Fech and David Furrer. Processing of Nickel-base superalloys for turbine enginee disc application. Advanced Engineering materials, 2000, 2, No. 12.

Google Scholar

[11] V. A. Kuzmenko and A. I. Afonin. Energy Dissipation in Metals in High-Frequency Fatigue tests, Ⅱ. UDC 539. 43.

Google Scholar