高温合金结构对超声波参数的影响

Q4 Engineering Fatigue of Aircraft Structures Pub Date : 2015-12-01 DOI:10.1515/fas-2015-0010
J. Nawrocki, K. Gancarczyk, W. Manaj, R. Albrecht, R. Cygan, K. Krupa
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引用次数: 0

摘要

摘要:本文对航空发动机高低压涡轮中常用的镍基高温合金Inconel 713C铸件进行了分析。这些钢锭是在Rzeszów科技大学航空航天材料研究与开发实验室制造的。采用x射线衍射取向法和超声波传播法对高温合金组织进行了分析。超声技术主要用于叶片壁厚的测量。测量精度由超声波在被测材料中的传播速度决定。本文研究了镍基高温合金组织对超声波传播速度的影响。分析了三种不同的宏观结构:等轴(EQ)、定向凝固(DS)和单晶(SX)。作者将所获得的铸件中的晶体取向偏差确定为[001]结晶学方向偏离了锭体的提取轴或主轴。通过测量,研究人员确定了EQ、DS和SX结构之间波速的显著差异。
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The Effect of Superalloy Structure on Ultrasonic Wave Parameters
Abstract This paper analyses the nickel based superalloy Inconel 713C casts typically used in high and low pressure turbines of aircraft engines. The ingots were manufactured in the Research and Development Laboratory for Aerospace Materials at the Rzeszów University of Technology. The superalloy structures were analysed by the following methods: X-ray diffraction orientation measurement and ultrasonic wave propagation. Ultrasonic techniques are mainly used to measure the blade wall’s thickness. Measurement accuracy is determined by the velocity of the ultrasonic wave in the material tested. This work evaluates the effect of the nickel-based superalloy microstructure on the velocity of the ultrasonic wave propagation. Three different macrostructures: equiax (EQ), directionally solidified (DS) and single crystal (SX) were analysed. The authors determined the crystal misorientation in the obtained casts as the deviation of [001] crystallographic direction from the withdrawal axis or the main axis of the ingots. The measurements performed allowed researchers to identify significant differences in the wave velocity between EQ, DS and SX structures.
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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
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0.00%
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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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