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Finite element analysis and design of three-dimensional superplastic sheet forming processes.

机译:三维超塑性板材成形过程的有限元分析和设计。

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Superplastic forming is widely accepted as an advanced manufacturing method in the aerospace industry to produce complex components. However, in order to successfully design a superplastic forming process, it is necessary to predict the pressure loading cycle to maintain optimum superplastic conditions during deformation. In this dissertation a three dimensional finite element formulation for the design and analysis of thin sheet superplastic forming is presented. A non-Newtonian viscous model is used to describe the material behavior while principles of shell mechanics are used to model the sheet deformation. The sheet is discretized using a simple 6 noded Kirchhoff shell element which is capable of carrying constant membrane stress and constant moments. Based on the principle of rate of virtual work, the finite element equations have been developed with magnitudes referred to a convective coordinate system. The convective system changes with time and conforms to the shape of the midsurface of the shell. An explicit time stepping scheme is implemented to integrate the motion of the sheet from velocities which are the primary solution variables. The nonlinear equilibrium equations are solved using a Newton-Raphson iterative method. A new pressure prediction scheme, based on the power law constitutive model and membrane kinematic assumptions, has been developed and implemented into the formulation. The contact conditions are imposed by the method of pseudo-equilibrium coupled with a compatibility load step. Simple efficient techniques are employed in determining the occurrence and location of contact. A frictional contact procedure, which introduces the effect of friction through the application of tangential forces at the contact node, is presented. Finally, example problems to demonstrate the applicability of the model to simulate superplastic forming are solved. Simple shapes such as long rectangular pans and cones are superplastically formed and successfully verified with experimental results. The superplastic forming of a realistic industrial component is also presented.
机译:超塑性成形已被广泛接受为航空航天工业中生产复杂零件的先进制造方法。但是,为了成功设计超塑性成形工艺,必须预测压力加载周期,以在变形过程中保持最佳的超塑性条件。本文提出了一种用于薄板超塑性成形设计和分析的三维有限元公式。非牛顿粘性模型用于描述材料行为,而壳力学原理用于对板变形建模。使用简单的6结Kirchhoff壳单元将薄板离散化,该壳单元能够承受恒定的膜应力和恒定的力矩。根据虚功率的原理,开发了以对流坐标系为参考的大小的有限元方程。对流系统随时间变化,并符合壳的中表面形状。实施了显式的时间步进方案,以根据速度(主要解决方案的变量)对薄片的运动进行积分。使用牛顿-拉夫森迭代法求解非线性平衡方程。基于幂律本构模型和膜运动学假设,已经开发了一种新的压力预测方案,并将其实施到公式中。接触条件是通过伪平衡方法和兼容性负载步骤确定的。在确定接触的发生和位置时采用了简单有效的技术。提出了一种摩擦接触程序,该过程通过在接触节点处施加切向力来引入摩擦效果。最后,解决了一些问题,这些问题证明了该模型可用于模拟超塑性成形。简单的形状,如长矩形锅和圆锥形被超塑成型,并通过实验结果成功验证。还介绍了实际工业组件的超塑性成形。

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