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Fatigue behaviour of fastener holes in high-strength aluminium plates repaired by cold spray deposition

机译:冷喷涂沉积修复高强度铝板扣件孔的疲劳行为

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摘要

This work examines the fatigue behaviour of additive cold spray (CS) repairs of AA7075 and AA2024 fastener holes. Structural ring repairs around fastener holes were made by machining blend-outs ranging from 1/8 to 1/2 the thickness of the plate, then refilling the section of removed material with CS deposition. The repairs were then tested in a lap shear geometry with the repair on both the free (outside) and the mating (inside) surfaces, as well as in remote uniaxial tension. CS repairs for the inside lap shear AA7075 repair configuration and the outside lap shear AA2024 repair configuration were found to have significantly increased fatigue lives even exceeding the number of cycles to failure of the undamaged, unrepaired control plates. Further, none of the CS repairs caused any detrimental impact on fatigue life, and microhardness results indicate that no thermal damage to the substrate occurred. Some interface cracking was seen in the CS repairs; however, no separation of the repair from the substrate was observed.
机译:这项工作检查了AA7075和AA2024紧固件孔的添加剂冷喷涂(CS)修补的疲劳行为。紧固件孔周围的结构环修复是通过以下方式进行的:在板材厚度的1/8至1/2范围内进行机械加工,然后用CS沉积物重新填充去除的材料部分。然后以搭接剪切几何形状对修补物进行测试,同时在自由(外部)和配合(内部)表面以及远距离的单轴张力下进行修补。发现内部搭接剪AA7075维修配置和外侧搭接剪AA2024维修配置的CS维修具有显着提高的疲劳寿命,甚至超过了未损坏,未经修理的控制板失效的循环次数。此外,CS修复均未对疲劳寿命造成任何不利影响,显微硬度结果表明未对基材产生热损伤。 CS维修中发现一些界面破裂;然而,没有观察到修复物与基材分离。

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