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(Poster Session)FRICTION STIR WELDING OF THIN 7075 T6 SHEETS COATED WITH ANTICORROSIVE LAYER

机译:(海报会话)薄膜搅拌搅拌焊接薄7075 T6板涂层耐防腐蚀层

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The goal of the work is to develop friction stir welding process for joining aluminum 7075 T6 sheets. The thickness of the sheets is 0.8 mm. The sheets are coated with anticorrosive layer. The purpose of the welding process is to produce components of airplanes and helicopters in PZL Mielec. Currently, riveting and resistance spot welding technologies are used for joining of aluminum components. The main challenge in obtaining defect free joints using FSW technology is the anticorrosive layer at the interface between top and bottom sheet. The anticorrosive layer has thickness of about 0.03 mm and is made of aluminum. Additionally, since aluminum has tendency to oxidize, the anticorrosive layer is covered with passive layer of aluminum oxide. The anticorrosive layer decreases the degree of material stir in the bottom sheet and acts as insulation blocking the flow of heat to the bottom sheet. Both these factors contribute to occurrence of wormholes and kissing bond defects in the bottom sheet. Additionally, the anticorrosive layer has tendency to form hooking and thinning defects. Hooking and thinning defects initiate cracks and severely decrease joint strength.The anticorrosive layers can be removed using chemical etching. However, this approach requires developing alternative technology for protecting joints against corrosion. Aluminum joints in aerospace applications are exposed to humidity and thermal cycles which contribute to rapid corrosion development, especially at the interface between joined sheets. The ability to weld sheets covered with anticorrosive layer would greatly facilitate the overall production process.Aluminum sheets are joined using 3-axial CNC milling machines. Monolithic tools made of hot work tool steel are applied. The welding trajectory has the length of 350 mm. In order to assess the quality of a joint 3 sets of tests are performed: microstructure analysis, uni-axial tensile tests and microhardness measurements.The number of tool geometries were tested with respect to their ability to produce defectfree joints. In this paper three types of tools were investigated. The following conclusion can be drawn. The application of tools that don't have axis of symmetry improves material stir in the bottom sheet. The application of double weld pass allows for pushing anticorrosive layer into the joint center, removing hooking and thinning defects and thus increasing joint strength. At the current stage of the research the challenge is to produce joints that have both good material stir in the bottom sheet and are free of thinning and hooking defects.
机译:这项工作的目标是开发摩擦搅拌焊接过程用于接合铝7075 T6片材。片材的厚度为0.8毫米。片材涂覆有耐腐蚀层。焊接过程的目的是产生在PZL Mielec的飞机和直升机的部件。目前,铆接和电阻点焊技术用于铝部件的接合。在使用FSW技术获得无缺陷的关节的主要挑战是在顶部和底部片材之间的界面处的耐腐蚀层。防腐层具有大约0.03毫米的厚度和由铝制成。另外,由于铝具有倾向氧化,耐腐蚀层覆盖有氧化铝的钝化层。耐腐蚀层减少材料搅拌的在所述底部片材的程度和作为绝缘阻挡热源到所述底部片材的流动。这两种因素导致了虫洞发生和在所述底部片材接吻键的缺陷。此外,耐腐蚀层具有容易形成钩和变薄的缺陷。钩住和减薄缺陷引发的裂纹和严重降低关节strength.The防腐层可使用化学蚀刻被去除。然而,这种方法需要开发替代技术,保护关节免受腐蚀。在航空航天应用中的铝接头被暴露于湿气和这有助于迅速腐蚀发展的热循环,特别是在接合片之间的界面。将大大促进整体生产process.Aluminum片材的能力覆盖有防腐层焊片材使用3-轴向数控铣床接合。由热作模具钢的单片工具被应用。焊接轨迹具有350毫米的长度。为了评估的接头3组测试的质量进行:工具的几何形状的微结构分析,单轴向拉伸试验及硬度measurements.The数相对于进行测试,以他们的能力,以产生无缺陷的关节。在本文中三种类型的工具进行了调查。下面可以得出结论。工具不具有对称轴的应用改善了在底部片材材料搅拌。双焊道的应用允许推防腐层进入接头中心,除去钩住和减薄缺陷,从而增加接合强度。在研究的当前阶段面临的挑战是产生在底部板片都好材料搅拌均匀,并免费细化的挂钩缺陷的关节。

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