扩散法修复裂纹零件铝片几何参数的实验与数值研究

S. Dehghanpour, A. Nezamabadi, Mohammadmahdi Attar, F. Barati, M. Tajdari
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引用次数: 1

摘要

修补断裂的航空结构是恢复其力学性能、强度和延长疲劳寿命的常用方法。这种贴片的性能可以通过比较修复件与未修复件所能承受的最大力来获得。补片的形状、尺寸以及补片的粘结方式对补片的质量有重要影响。因此,在本文中,我们研究了影响贴片和片之间扩散键合的因素。实验和数值研究了垂直于加载方向的10 mm中心裂纹片(I型)上铝片的形状对加载过程的影响。采用复合可旋转居心设计,实验得到了扩散连接的最佳条件,包括连接的压力、时间和温度,并在此条件下,将贴片形状和长径比作为设计变量,得到了正方形、矩形、圆形和椭圆形贴片的设计结果。最后发现,在570℃、70 bar、100 min的压力条件下形成了最佳连接,矩形贴片效率更高,但其程度更符合裂纹。在固定区域,本研究中研究的不同贴片几何形状能够影响修复部件可承受的最大力的80%。此外,在实验结果和数值结果之间有一个可接受的收敛。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental and Numerical Investigation on Geometric Parameters of Aluminum Patches for Repairing Cracked Parts by Diffusion Method
Repairing cracked aerial structures using patches is a common way to restore mechanical properties, strength and extend fatigue life. The performance of such patches can be obtained by comparing the maximum amount of force tolerated by the repaired piece with the unrepaired piece. The shape and dimensions of the patch used to repair the crack and the way the patch is bonded affect the repair quality which are of great importance. Therefore, in this paper, we investigate the factors affecting the diffusion bonding between the patch and the piece. The impact of the shape of the aluminum patch attached on a 10 mm central crack piece and perpendicular to the loading direction (mode I) is studied experimentally and numerically. The optimum conditions for the diffusion connection including the pressure, time and temperature of the connection were obtained experimentally using a composite rotatable centered design and in the connection made under these conditions, the patch shape and aspect ratio was considered as variables of design, and the results were obtained for square, rectangular, circular and elliptical patches. At the end, it was found that the best connection under the pressure conditions of 570 °C, 70 bar and 100 min was formed and the rectangular patch efficiency was greater whereas its extent is more in line with crack than the other modes. At a fixed area, the different patch geometries investigated in this study were able to influence up to 80% of the maximum force tolerated by the repaired parts. Also, there is an acceptable convergence between experimental and numerical results.
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