The Application of Acoustic Anisotropy to Evaluation of Material Properties

Q4 Engineering Fatigue of Aircraft Structures Pub Date : 2015-01-01 DOI:10.1515/fas-2015-0001
J. Krysztofik, W. Manaj, G. Socha
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引用次数: 2

Abstract

Abstract Structural properties of materials change under stress, temperature and work environment. These changes are generally unfavorable. They cause a reduction in strength of materials. This has an impact on the safety and service life of machines and constructions. In the chemical and petrochemical industry the destruction of a structure can be activated by chemical substances. In the energy industry, a key element in assisting the destruction is temperature. In aviation, the typical cause of damage is the process of fatigue. Regardless of the differences regarding/concerning the mechanisms of degradation, typical of the sectors of industry, the end result is the emergence of microvoids and microcracks in the material. In the final phase of the process, dominant cracks are formed. The term of measure of material damage, introduced by Kachanov and Rabotnow, can be effectively used also when considering the impact of microdamages on measurable macroscopic acoustic quantities. A damage parameter proposed by Johnson allows to correlate changes in acoustic birefringence of the material with the parameter describing the degree of damage. In this article the authors presented the nondestructive tests results concerning Inconel 718 alloy subjected to damage caused by plastic deformation. This paper focuses on the evaluation of acoustic properties in relation to the degradation of the materials tested.
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声学各向异性在材料性能评价中的应用
材料的结构性能在应力、温度和工作环境下发生变化。这些变化通常是不利的。它们会降低材料的强度。这对机器和建筑物的安全性和使用寿命都有影响。在化学和石化工业中,化学物质可以激活结构的破坏。在能源工业中,协助破坏的一个关键因素是温度。在航空领域,典型的损坏原因是疲劳过程。不管在退化机制方面的差异,典型的工业部门,最终的结果是材料中出现微孔和微裂纹。在该过程的最后阶段,主要裂纹形成。由Kachanov和Rabotnow引入的材料损伤测量术语也可以有效地用于考虑微损伤对可测量的宏观声学量的影响。Johnson提出的损伤参数允许将材料的声学双折射变化与描述损伤程度的参数相关联。本文介绍了因科内尔718合金塑性变形损伤的无损检测结果。本文主要讨论了与被测材料退化有关的声学性能评价。
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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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