Enlarged Zn Content Improves Fatigue Crack Propagation Resistance of Two Al-Zn-Mg-Cu Alloys with Multiple Aging Tempers

Article Preview

Abstract:

Fatigue crack propagation is closely associated to the chemical composition of Al-Zn-Mg-Cu alloys. In this work, two Al-Zn-Mg-Cu alloys with a variation of zinc content was investigated and multiple aging treatments were exerted on them and a same regime was selected for further fatigue analysis by tensile property tests. The corresponding precipitation characteristics and fracture surface were observed. The results showed that the alloy with lower zinc content (LZ alloy) possessed an inferior strength value compared with the alloy with higher zinc content (HZ alloy) under the same three stage aging treatments while the elongation had no obvious difference. In contrast, the LZ alloy had a higher fatigue crack propagation rate than the HZ alloy. The observation of fracture surface also proved it. The precipitation observation demonstrated that both had GP zones and η' phase, which possessed the majority. Quantitative analysis of precipitates exhibited that the HZ alloy had a larger proportion of large size precipitates than the LZ alloy. The mechanism of the interaction between dislocation and precipitate was employed to elaborate the difference.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

15-22

Citation:

Online since:

May 2022

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2022 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] J.T. Burns, J. Boselli. Effect of plate thickness on the environmental fatigue crack growth behavior of AA7085-T7451, Int. J. Fatigue. 2016, 83: 253-268.

DOI: 10.1016/j.ijfatigue.2015.10.020

Google Scholar

[2] T.R.F. Cavalcante, G.S. Pereira, G.Y. Koga, et al. Fatigue crack propagation of aeronautic AA7050-T7451 and AA2050-T84 aluminum alloys in air and saline environments, Int. J. Fatigue. 2022, 154: 106519.

DOI: 10.1016/j.ijfatigue.2021.106519

Google Scholar

[3] K.D. Jiang, Z. Zhang, W.B. Zhu, et al. Influence of V additions on microstructures, tensile and fatigue properties of Al–Zn–Mg alloys, Mater. Scie. Eng. A. 2022, 829: 142184.

DOI: 10.1016/j.msea.2021.142184

Google Scholar

[4] M. Satyanarayana, S. Bathula, A. Kumar. Towards finding an actual fatigue crack growth rate of friction stir processed AA2014 alloy, Mater. Lett. 2021, 305: 130757.

DOI: 10.1016/j.matlet.2021.130757

Google Scholar

[5] J. Lindigkeit, A. Gysler, G. Lütjering. The effect of microstructure on the fatigue crack propagation behavior of an Al-Zn-Mg-Cu alloy, Metal. Trans. A. 1981, 12(9): 1613-1619.

DOI: 10.1007/bf02643567

Google Scholar

[6] T.H. Sanders, E.A. Starke. The relationship of microstructure to monotonic and cyclic straining of two age hardening aluminum alloys, Metal. Trans. A. 1976, 7(9): 1407-1418.

DOI: 10.1007/bf02658827

Google Scholar

[7] S. Zhou, L. Wang, L.Y. Xie, et al. Effect of T7951 secondary aging treatment on crack propagation behavior of 7055 aluminum alloy, Trans. Nonferrous Metals Soc. 2016, 26(4): 938-944.

DOI: 10.1016/s1003-6326(16)64190-0

Google Scholar

[8] J.T. Burns, V.K. Gupta, S.R. Agnew, et al. Effect of low temperature on fatigue crack formation and microstructure-scale propagation in legacy and modern Al–Zn–Mg–Cu alloys, Int. J. Fatigue. 2013, 55(7): 268-275.

DOI: 10.1016/j.ijfatigue.2013.06.025

Google Scholar

[9] K. Wen, B. Xiong, Y. Zhang, et al. Measurement and Theoretical Calculation Confirm the Improvement of T7651 Aging State Influenced Precipitation Characteristics on Fatigue Crack Propagation Resistance in an Al–Zn–Mg–Cu Alloy, Met. Mater. Int. 2021, 27: 779-795.

DOI: 10.1007/s12540-019-00446-5

Google Scholar

[10] H.W. Höppel, L. May, M. Prell, et al. Influence of grain size and precipitation state on the fatigue lives and deformation mechanisms of CP aluminium and AA6082 in the VHCF-regime, Int. J. Fatigue. 2011, 33(1): 10-18.

DOI: 10.1016/j.ijfatigue.2010.04.013

Google Scholar

[11] Y.L. Wang, Q.L. Pan, L.L. Wei, et al. Effect of retrogression and reaging treatment on the microstructure and fatigue crack growth behavior of 7050 aluminum alloy thick plate, Mater. Des. 2014, 55(6): 857-863.

DOI: 10.1016/j.matdes.2013.09.063

Google Scholar

[12] Y. Li, G. Xu, S. Liu, et al. Effect of ageing treatment on fatigue crack growth of die forged Al-5.87Zn-2.07Mg-2.42Cu alloy, Eng. Frac. Mech. 2019, 215: 251-260.

DOI: 10.1016/j.engfracmech.2019.04.023

Google Scholar

[13] R. Yang, Z. Liu, P. Ying, et al. Multistage-aging process effect on formation of GP zones and mechanical properties in Al-Zn-Mg-Cu alloy, Trans. Nonferrous Metals Soc. 2016, 26(5): 1183-1190.

DOI: 10.1016/s1003-6326(16)64221-8

Google Scholar

[14] P. Xia, Z. Liu, S. Bai, et al. Enhanced fatigue crack propagation resistance in a superhigh strength Al–Zn–Mg–Cu alloy by modifying RRA treatment, Mater. Charact. 2016, 118: 438-445.

DOI: 10.1016/j.matchar.2016.06.023

Google Scholar

[15] K. Wen, B. Xiong, Y. Zhang, et al. Over-aging influenced matrix precipitate characteristics improve fatigue crack propagation in a Al-Zn-Mg-Cu alloy, Mater. Sci. Eng. A. 2018, 716: 42-54.

DOI: 10.1016/j.msea.2018.01.040

Google Scholar

[16] J.T. Liu, Y.A. Zhang, X.W. Li, et al. Thermodynamic calculation of high zinc-containing Al-Zn-Mg-Cu alloy, Trans. Nonferrous Metals Soc. 2014, 24(5): 1481-1487.

DOI: 10.1016/s1003-6326(14)63216-7

Google Scholar

[17] G.E. Pellissier, S.M. Purdy. Stereology and Quantitative Metallography, Addison-Wesley Publishing Company, USA, (1972).

Google Scholar