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Parametric Analysis of the Mandrel Geometrical Data in a Cold Expansion Process of Small Holes Drilled in Thick Plates

机译:厚板小孔冷扩过程中心轴几何数据的参数分析

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摘要

Cold expansion technology is a cold-forming process widely used in aeronautics to extend the fatigue life of riveted and bolted holes. During this process, an oversized mandrel is pushed through the hole in order to yield it and generate compressive residual stresses contributing to the fatigue life extension of the hole. In this paper, a parametric analysis of the mandrel geometrical data (inlet angle straight zone length and diametric interference) and their influence on the residual stresses was carried out using a finite element method (FEM). The obtained results were compared with the conclusions presented in a previous parametric FEM analysis on the influence of the swage geometry in a swaging cold-forming process of gun barrels. This process could be considered, in a simplified way, as a scale-up of the cold expansion process of small holes, and this investigation demonstrated the influence of the diameter ratio (K) on the relation between the mandrel or swage geometry and the residual stresses obtained after the cold-forming process.
机译:冷膨胀技术是一种广泛用于航空领域的冷成型工艺,可以延长铆钉孔和螺栓孔的疲劳寿命。在此过程中,将过大的心轴推过孔,以使其屈服并产生压缩残余应力,从而有助于延长孔的疲劳寿命。在本文中,使用有限元方法对心轴几何数据(进口角直区长度和直径干涉)及其对残余应力的影响进行了参数分析。将获得的结果与先前的参数有限元分析中提出的关于型锻几何形状在枪管型锻冷成型过程中的影响的结论进行了比较。该过程可以简化地考虑为小孔的冷膨胀过程的放大,并且该研究证明了直径比(K)对心轴或型锻几何形状与残余量之间的关系的影响。冷成型后获得的应力。

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