合金和复合材料的硬化及其衍射和自洽模型检验

Q4 Engineering
Elżbieta Gadalińska, A. Baczmaňski, S. Wronski, M. Wróbel, Christian Scheffzük
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引用次数: 0

摘要

本文介绍了原位拉伸试验中Al/SiC复合材料和2124T6铝合金的衍射应力测量结果。这项工作的主要目的是观察应用两种类型的热处理后的复合材料和用作该复合材料基体的合金在拉伸试验的不同阶段的应力值,以确定硬化过程的类型。将实验结果与Baczmański[1]-[3]开发的自洽模型的计算结果进行了比较,以获得有关被检材料微观力学性能(临界分辨剪切应力τcr和硬化参数H)的信息。这种比较使研究人员能够确定增强材料在复合材料中的作用,以及热处理对材料硬化的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The Hardening in Alloys and Composites and Its Examination with a Diffraction and Self-Consistent Model
Abstract The paper presents the results of diffraction stress measurement in Al/SiC composite and in 2124T6 aluminum alloy during the in situ tensile test. The main aim of the work is to observe the stress values for different stages of tensile test for the composite after applying two types of thermal treatment and for the alloy used as a matrix in this composite, to identify the type of hardening process. The experimental results were compared against the calculations results obtained from the self-consistent model developed by Baczmański [1] - [3] to gain the information about the micromechanical properties (critical resolved shear stress τcr and hardening parameter H) of the examined materials. This comparison allowed researchers to determine the role of reinforcement in the composite as well as the impact of the heat treatment on the hardening of the material.
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来源期刊
Fatigue of Aircraft Structures
Fatigue of Aircraft Structures Engineering-Safety, Risk, Reliability and Quality
CiteScore
0.40
自引率
0.00%
发文量
0
期刊介绍: The publication focuses on problems of aeronautical fatigue and structural integrity. The preferred topics include: full-scale fatigue testing of aircraft and aircraft structural components, fatigue of materials and structures, advanced materials and innovative structural concepts, damage tolerant design of aircraft structure, life extension and management of ageing fleets, structural health monitoring and loads, fatigue crack growth and life prediction methods, NDT inspections, airworthiness considerations.
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