Modelling the small punch tensile behaviour of an aerospace alloy

被引:17
作者
Lancaster, R. J. [1 ]
Illsley, H. W. [1 ]
Davies, G. R. [1 ]
Jeffs, S. P. [1 ]
Baxter, G. J. [2 ]
机构
[1] Swansea Univ, Inst Struct Mat, Bay Campus, Swansea SA1 8EN, W Glam, Wales
[2] Rolls Royce Plc, Derby DE24 8BJ, England
基金
英国工程与自然科学研究理事会;
关键词
Small punch; Ti-6Al-4V; Fractography; DEFORM; SINGLE-CRYSTAL SUPERALLOY; DEFORMATION; FRACTURE; DUCTILE; STEELS; TESTS; TEMPERATURE; MECHANISMS;
D O I
10.1080/02670836.2016.1230168
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The small punch (SP) test is a widely accepted methodology for obtaining mechanical property information from limited material quantities. Much research has presented the creep, tensile and fracture responses of numerous materials gathered from small-scale testing approaches. This is of particular interest for alloy down selection of next-generation materials and in situ mechanical assessments. However, to truly understand the evolution of deformation of the miniature disc specimen, an accurate and detailed understanding of the progressive damage is necessary. This paper will utilise the SP test to assess the tensile properties of several Ti-6Al-4V materials across different temperature regimes. Fractographic investigations will establish the contrasting damage mechanisms and finite element modelling through DEFORM software is employed to characterise specimen deformation.
引用
收藏
页码:1065 / 1073
页数:9
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