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Friction forge riveting of AA7075-T6 sheets with large diameter 2117-T3 rivets
Aircraft Engineering and Aerospace Technology ( IF 1.5 ) Pub Date : 2023-09-13 , DOI: 10.1108/aeat-03-2023-0079
Mustafa Soylak , Veysel Erturun

Purpose

The purpose of this paper is to examine the effect of changing some riveting parameters on the riveting quality of a riveted aircraft structure. In this study, riveting was performed by applying friction under pressure.

Design/methodology/approach

During this friction riveting process, a feed of 3 mm/min was applied in the axial direction. Rotation speed values of 2,000, 2,200 and 2,400 rpm were selected. A 3-axis die milling machine was used to achieve the required positioning, pressing force and friction effect. 1.27 mm-thick Al 7075-T6 sheets and 2117-T3 forged rivets were used. The feed rate was applied at 1 mm/min in both tensile shear and cross-tensile tests.

Findings

The feasibility of friction riveting in 2117-T3 rivets was examined, it was shown that it could be done, and the most suitable rotation value for this process was determined.

Originality/value

Clamping force is one of the most important parameters for riveting quality. This study will contribute to a better understanding of the friction-forging riveting process along with the effects of riveting parameters. At the same time, it will lead to more research and expand the application of friction forging riveting to more structural connections.



中文翻译:

AA7075-T6板材与大直径2117-T3铆钉的摩擦锻铆

目的

本文的目的是研究改变一些铆接参数对铆接飞机结构的铆接质量的影响。在这项研究中,铆接是通过在压力下施加摩擦来进行的。

设计/方法论/途径

在此摩擦铆接过程中,轴向进给速度为 3 毫米/分钟。选择的转速值为 2,000、2,200 和 2,400 rpm。采用三轴模具铣床来达到所需的定位、压紧力和摩擦效果。使用 1.27 毫米厚的 Al 7075-T6 板材和 2117-T3 锻造铆钉。在拉伸剪切和交叉拉伸测试中,进给速率均为 1 毫米/分钟。

发现

对2117-T3铆钉进行摩擦铆接的可行性进行了检验,结果表明这是可行的,并确定了该工艺最合适的旋转值。

原创性/价值

夹紧力是铆接质量最重要的参数之一。这项研究将有助于更好地理解摩擦锻造铆接过程以及铆接参数的影响。同时,也将引发更多的研究,将摩擦锻铆的应用拓展到更多的结构连接。

更新日期:2023-09-14
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