Enlarged Zn, Mg Contents with a same Zn/Mg Ratio Improve Fatigue Crack Propagation Resistance of Al-Zn-Mg-Cu Alloys with T7651 State

Article Preview

Abstract:

The fatigue crack propagation of Al-Zn-Mg-Cu alloys could be influenced by the content of main alloying element. In the present work, two Al-Zn-Mg-Cu alloys with a same Zn/Mg ratio were treated by two stage over-aging aging treatment and typical T7651 states were extracted via mechanical properties. Fatigue crack propagation of the two alloys were tested and the related precipitation characteristics and fracture morphology were observed. The results showed that the alloy with higher Zn, Mg contents possessed a better fatigue crack propagation resistance compared with the alloy with lower Zn, Mg contents. The corresponding fracture morphology also showed the difference of fatigue striation, which provided an additional support. The precipitation observation demonstrated that the both alloys possessed GPII zone, η' phase and η phase while the alloy with higher Zn, Mg contents had a larger average precipitate size and a larger proportion of large size precipitates compared with the alloy with lower Zn, Mg contents. Cut and bypass mechanisms of dislocation-precipitate interactions were used to explain the difference of fatigue crack propagation between the two alloys.

You might also be interested in these eBooks

Info:

Periodical:

Materials Science Forum (Volume 1003)

Pages:

3-10

Citation:

Online since:

July 2020

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2020 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] T. Dursun, C. Soutis. Recent developments in advanced aircraft aluminium alloys, Mater. Des. 2014, 56(4): 862-871.

DOI: 10.1016/j.matdes.2013.12.002

Google Scholar

[2] J.C. Williams, E.A. Starke. Progress in structural materials for aerospace, Acta Mater. 2013, 51(19): 5775-5799.

Google Scholar

[3] A. Heinz, A. Haszler, C. Keidel, et al. Recent development in aluminium alloys for aerospace applications, Mater. Sci. Eng. A. 2000, 280(1): 102-107.

DOI: 10.1016/s0921-5093(99)00674-7

Google Scholar

[4] P.A. Rometsch, Y. Zhang, S. Knight. Heat treatment of 7xxx series aluminium alloys—Some recent developments, Trans. Nonferrous Metals Soc. 2014, 24(7): 2003-2017.

DOI: 10.1016/s1003-6326(14)63306-9

Google Scholar

[5] A. Azarniya, A.K. Taheri, K.K. Taheri. Recent advances in ageing of 7xxx series aluminum alloys: a physical metallurgy perspective, J. Alloy Compd, 2018, 781: 945-983.

DOI: 10.1016/j.jallcom.2018.11.286

Google Scholar

[6] J.E.A. Starke, J.T. Staley. Application of modern aluminum alloys to aircraft, Prog. Aeronaut. Sci. 1996, 32(2-3): 131-172.

Google Scholar

[7] D.G. Harlow, J. Nardiello, J. Payne. The effect of constituent particles in aluminum alloys on fatigue damage evolution: Statistical observations, Int. J. Fatigue. 2010, 32(3): 505-511.

DOI: 10.1016/j.ijfatigue.2009.02.036

Google Scholar

[8] D. Yin, H. Liu, Y. Chen, et al. Effect of grain size on fatigue-crack growth in 2524 aluminium alloy, Int. J. Fatigue. 2016, 84: 9-16.

DOI: 10.1016/j.ijfatigue.2015.11.011

Google Scholar

[9] 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

[10] K. Hockauf, M.F.X. Wagner, T. Halle, et al. Influence of precipitates on low-cycle fatigue and crack growth behavior in an ultrafine-grained aluminum alloy, Acta Mater. 2014, 80: 250-263.

DOI: 10.1016/j.actamat.2014.07.061

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: 857-863.

DOI: 10.1016/j.matdes.2013.09.063

Google Scholar

[12] M. Goto, S.Z. Han, S.H. Lim, et al. Role of microstructure on initiation and propagation of fatigue cracks in precipitate strengthened Cu–Ni–Si alloy, Int. J. Fatigue. 2016, 87: 15-21.

DOI: 10.1016/j.ijfatigue.2016.01.004

Google Scholar

[13] 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

[14] K. Wen, Y. Fan, G. Wang, et al. Aging behavior and fatigue crack propagation of high Zn-containing Al-Zn-Mg-Cu alloys with zinc variation, Prog. Nat. Sci. 2017, 27(2): 217-227.

DOI: 10.1016/j.pnsc.2017.02.002

Google Scholar

[15] J.D. Verhoeven, Fundamentals of Physical Metallurgy, John Wiley, New York, (1975).

Google Scholar