Low Cycle Fatigue Properties of FGH720Li Superalloy

Article Preview

Abstract:

Low cycle fatigue (LCF) properties of a powder metallurgy(PM) nickel base superalloy FGH720Li were systematically studied in this work, including smooth LCF and notched LCF tested at various temperatures and different stress. The relationship between the fatigue life and applied stress was analyzed both for smooth fatigue and notch fatigue tests. The effects of loading frequency and stress ratio on LCF behavior were also studied. As an important influencing factor of the fatigue life in powder metallurgy superalloy, the effect of inclusions on LCF life was also investigated. The results showed that the fatigue properties of FGH720Li alloy was excellent, when tested at the temperature of 450°C and applied stress of 1230MPa, the fatigue life could exceed 5×104 cycles. When tested at 650°C and 1150MPa, the average fatigue life was still beyond 2×105 cycles.

You might also be interested in these eBooks

Info:

Periodical:

Materials Science Forum (Volume 1035)

Pages:

292-296

Citation:

Online since:

June 2021

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2021 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Zou Jinwen, Wang Wuxiang, Development and Application of PM Superalloy, Journal of Aeronautical Materials, 26(3) (2012) 244-250.

Google Scholar

[2] M. P. Jackson, R. C. Reed, Heat treatment of Udimet720Li: the effect of microstructure on properties, Material Science and Engineering A, 259(1) (1999) 85-97.

Google Scholar

[3] S. E. Kim, M. P. Jackson, R. C. Reed, Quantification of the minor precipitates in Udimet720Li using electrolytic extraction and X-ray diffraction, Material Science and Engineering A, 245(2) (1998) 225-232.

DOI: 10.1016/s0921-5093(97)00728-4

Google Scholar

[4] Liu Yang, Tao Yu, Jia Jian, The microstructure evolution of FGH98 PM superalloy after hot deformation, Powder Metallurgy Industry, 21(2) (2011) 14-19.

Google Scholar

[5] G. Onofiro, G. A. Osinkolu, M. Marchionni, Fatigue crack growth of Udimet 720Li superalloy at elevated temperature, International Journal of Fatigue, 23(2001) 887-895.

DOI: 10.1016/s0142-1123(01)00053-6

Google Scholar

[6] J. Luo, P. Bowen, Statistical aspects of fatigue behavior in a PM Ni-base superalloy Udimet 720, Acta Materialia, 51(2003) 3521-3535.

DOI: 10.1016/s1359-6454(03)00171-x

Google Scholar

[7] 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

[8] China national standardization administration, GB/T 15248-2008 the test method for axial loading constant-amplitude low-cycle fatigue of metallic materials, China Standard Press, Beijing, 2008, 1–17.

Google Scholar

[9] Benjamin Guennec, Akira Ueno, Tatsuo Sakai, Effect of the loading frequency on fatigue properties of JIS S15C low carbon steel and some discussions based on micro-plasticity behavior, International Journal of Fatigue, 66 (2014) 29-38.

DOI: 10.1016/j.ijfatigue.2014.03.005

Google Scholar