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Introduction of Enhanced Compressive Residual Stress Profiles in Aerospace Components Using Combined Mechanical Surface Treatments

机译:使用组合机械表面处理引入航空航天部件中增强的压缩残余应力分布

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Mechanical surface treatments such as Shot Peening (SP) and Deep Cold Rolling (DCR) are being used to introduce Compressive Residual Stress (CRS) at the surface and subsurface layers of aerospace components, respectively. This paper investigates the feasibility of a combined introduction of both the surface and sub-surface compressive residual stress on Ti6A14V material through a successive application of the two aforementioned processes, one after the other. CRS profiles between individual processes were compared to that of combination of processes to validate the feasibility. It was found out that shot peening introduces surface compressive residual stress into the already deep cold rolled sample, resulting in both surface and sub-surface compressive residual stresses in the material. However the drawback of such a combination would be the increased surface roughness after shot peening a deep cold rolled sample which can be critical especially in compressor components. Hence, a new technology, Vibro-Peening (VP) may be used as an alternative to SP to introduce surface stress at reduced roughness.
机译:诸如喷丸(SP)和深冷轧(DCR)的机械表面处理分别用于在航空航天部件的表面和地下层的压缩残余应力(CRS)。本文通过连续应用,通过连续应用两个前述过程,研究了Ti6a14V材料的结合引入的可行性。将各个过程之间的CRS简档与过程的组合进行比较,以验证可行性。发现射击喷丸将表面压缩残余应力引入已有深冷轧样品中,导致材料中的表面和亚表面压缩残余应力。然而,这种组合的缺点将是在喷丸灌注后的表面粗糙度增加,这是一种深冷轧制样品,这可能尤其是在压缩机部件中。因此,新技术,vibro-peening(vp)可以用作Sp以在降低粗糙度下引入表面应力的替代方案。

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