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A superplastic forming limit diagram concept for Ti-6A1-4V

机译:Ti-6A1-4V的超塑性成形极限图概念

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The current paper is concerned with the development of a simplified method for predicting failure due to plastic instability during the superplastic forming (SPF) of titanium alloys. The rationale is that a key factor in the process of reliable failure prediction is the incorporation of a mechanisms-based model, which includes microstructural effects, such as static and dynamic grain growth and associated hardening, and which is also independent of the forming strain-rate. Existing methods for predicting plastic instability during conventional metal-forming are discussed along with previous attempts at predicting failure during SPF. It is shown that no easy-to-interpret method, such as the forming limit diagram (FLD) in conventional forming, exists for SPF. Consequently, an SPFLD concept in a major strain (ε_1, minor strain (ε_3), and equivalent strain-rate space (ε_(eq)) is presented on the basis of uniaxial SP ductilities across a range of strain-rates along with the Hill-Swift instability criteria and using finite element-predicted ε_1-ε_3-ε_(eq) paths for key points on the forming blank to predict failure. The predicted results are validated against measured data for Ti-6A1-4V at different strain-rates.
机译:当前的论文涉及一种简化的方法的开发,该方法可以预测由于钛合金的超塑性成形(SPF)过程中的塑性不稳定性而导致的失效。理由是,在可靠的故障预测过程中,关键因素是采用基于机制的模型,该模型包括微观结构效应,例如静态和动态晶粒长大以及相关的硬化,并且与成型应变无关。率。讨论了用于预测常规金属成型过程中塑性不稳定性的现有方法,以及先前用于预测SPF失效的尝试。结果表明,对于SPF,不存在易于理解的方法,例如常规成形中的成形极限图(FLD)。因此,基于跨应变率范围的单轴SP延性以及Hill提出了大应变(ε_1,小应变(ε_3)和等效应变率空间(ε_(eq))中的SPFLD概念。 -快速失稳准则,并使用有限元预测的ε_1-ε_3-ε_(eq)路径作为成形坯料上的关键点来预测失效,并根据不同应变率下Ti-6A1-4V的测量数据验证了预测结果。

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