Repairing cracked aluminum plates by aluminum patch using diffusion method

作者: Sobhan Dehghanpour , Alireza Nezamabadi , Mohammadmahdi Attar , Farzan Barati , Mehdi Tajdari

DOI: 10.1007/S12206-019-0914-9

关键词:

摘要: The aim of this work is to scrutinize the importance diffusion bonding temperature, pressure and time on repair a cracked aluminum plate while maximum tensile strength under quasi-static loading has been investigated. method was used connect patches central mode I cracks in thin plates. Here, process repairing pieces made or alloys involved chemical mechanical step remove oxide press patch piece temperature difference at certain time. repaired underwent tolerable amount force obtained different situations. Having assigned five temperatures, 300, 400, 500, 550 600 C, as well four test times 30, 60, 120 180 min pressures 10, 20, 50, 80 110 bar, we utilized fractional factorial design approach perform 40 tests there seen 10 mm initial crack samples. Experimental results showed that optimum connection resulted °C bars within where tolerated by vs. unrepaired increased 92 %. Therefore, having weighed using bonding, suggest type can be proper cheap alternative composite adhesive patches.

参考文章(38)
Amir Abbas, Shirzadi Ghoshouni, Diffusion bonding aluminium alloys and composites : new approaches and modelling University of Cambridge. ,(1998) , 10.17863/CAM.14221
X.-P. Zhang, L. Ye, Y.-W. Mai, G.-F. Quan, W. Wei, Investigation on diffusion bonding characteristics of SiC particulate reinforced aluminium metal matrix composites (Al/SiCp-MMC) Composites Part A-applied Science and Manufacturing. ,vol. 30, pp. 1415- 1421 ,(1999) , 10.1016/S1359-835X(99)00040-8
Nicholas G. Tsouvalis, Lazarus S. Mirisiotis, Dimitris N. Dimou, Experimental and numerical study of the fatigue behaviour of composite patch reinforced cracked steel plates International Journal of Fatigue. ,vol. 31, pp. 1613- 1627 ,(2009) , 10.1016/J.IJFATIGUE.2009.04.006
R. Jones, W.K. Chiu, Composite repairs to cracks in thick metallic components Composite Structures. ,vol. 44, pp. 17- 29 ,(1999) , 10.1016/S0263-8223(98)00108-1
Alan Baker, Nik Rajic, Claire Davis, Towards a practical structural health monitoring technology for patched cracks in aircraft structure Composites Part A-applied Science and Manufacturing. ,vol. 40, pp. 1340- 1352 ,(2009) , 10.1016/J.COMPOSITESA.2008.09.015
H. Nakagawa, C. H. Lee, T. H. North, Modeling of base metal dissolution behavior during transient liquid-phase brazing Metallurgical Transactions A. ,vol. 22, pp. 543- 555 ,(1991) , 10.1007/BF02656822
W. Oudad, B. Bachir Bouiadjra, M. Belhouari, S. Touzain, X. Feaugas, Analysis of the plastic zone size ahead of repaired cracks with bonded composite patch of metallic aircraft structures Computational Materials Science. ,vol. 46, pp. 950- 954 ,(2009) , 10.1016/J.COMMATSCI.2009.04.041
Shu-Xin Li, Shan-Tung Tu, Fu-Zhen Xuan, A probabilistic model for prediction of bonding time in diffusion bonding Materials Science and Engineering A-structural Materials Properties Microstructure and Processing. ,vol. 407, pp. 250- 255 ,(2005) , 10.1016/J.MSEA.2005.07.003
J. Maity, T.K. Pal, R. Maiti, Transient liquid phase diffusion bonding of 6061-15 wt% SiCp in argon environment Journal of Materials Processing Technology. ,vol. 209, pp. 3568- 3580 ,(2009) , 10.1016/J.JMATPROTEC.2008.08.015