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Crack incubation in shot peened AA7050 and mechanism for fatigue enhancement

机译:喷丸AA7050中的裂纹温育及增强疲劳的机理

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Shot peening is a dynamic cold-working process involving the impingement of peening media onto a substrate surface. Shot peening is commonly used as a surface treatment technique within the aerospace industry during manufacturing to improve fatigue performance of structural components. The compressive residual stress induced during shot peening results in fatigue crack growth retardation, improving the performance of shot-peened components. However, shot peening is a compromise between the benefit of inducing a compressive residual stress and causing detrimental surface damage. Because of the relatively soft nature of AA7050-T7451, shot peening can result in cracking of the constituent precipitate particles, creating an initial damage state. The aim of this paper is to understand the balance and fundamentals of these competing phenomena through a comparative study throughout the fatigue lifecycle of baseline versus shot-peened AA7050-T7451. Microstructure and surface topology characterization and comparison of the baseline and shot-peened AA7050-T7451 has been performed using scanning electron microscopy, electron backscatter diffraction, energy dispersive spectroscopy, and optical profilometry techniques. A residual stress analysis through interrupted fatigue of the baseline and shot-peened AA7050-T7451 was completed using a combination of X-ray diffraction and nanoindentation. The fatigue life performance of the baseline versus shot-peened material has been evaluated, including crack initiation and propagation. Subsurface particles crack upon shot peening but did not incubate into the matrix during fatigue loading, presumably due to the compressive residual stress field. In the baseline samples, the particles were initially intact, but upon fatigue loading, crack nucleation was observed in the particles, and these cracks incubated into the matrix. In damage tolerant analysis, an initial defect size is needed for lifetime assessment, which is often difficult to determine, leading to
机译:喷丸处理是一种动态的冷加工工艺,涉及到将喷丸处理介质撞击到基材表面上。喷丸处理通常在制造过程中用作航空航天工业中的表面处理技术,以改善结构部件的疲劳性能。喷丸处理过程中产生的压缩残余应力会导致疲劳裂纹扩展延迟,从而改善喷丸处理组件的性能。然而,喷丸处​​理是在引起压缩残余应力的益处与造成有害的表面损害之间的折衷方案。由于AA7050-T7451的相对较软的性质,喷丸处理可能导致组成的沉淀颗粒破裂,从而形成初始损坏状态。本文的目的是通过在基线疲劳寿命与喷丸强化AA7050-T7451的整个疲劳寿命周期中进行比较研究,来了解这些竞争现象的平衡和基本原理。使用扫描电子显微镜,电子背散射衍射,能量色散光谱和光学轮廓分析技术对基线和喷丸处理的AA7050-T7451进行了微观结构和表面拓扑表征,并进行了比较。通过使用X射线衍射和纳米压痕相结合的方法,完成了通过基线疲劳破坏和喷丸处理的AA7050-T7451进行的残余应力分析。已评估了基线相对于喷丸处理材料的疲劳寿命性能,包括裂纹的产生和扩展。喷丸处理后,表面下的颗粒会破裂,但在疲劳载荷期间不会浸入基体中,这大概是由于压缩残余应力场造成的。在基线样品中,颗粒最初是完整的,但是在疲劳载荷下,颗粒中观察到裂纹成核,并且这些裂纹被温育到基质中。在损伤容限分析中,需要初始缺陷尺寸来进行寿命评估,这通常很难确定,从而导致

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    School of Aeronautics and Astronautics, Purdue University, 701 W. Stadium Ave, West Lafayette, IN 47907-2045, USA;

    School of Materials Engineering, Purdue University, 701 W. Stadium Ave. West Lafayette, IN 47907-2045, USA;

    School of Materials Engineering, Purdue University, 701 W. Stadium Ave. West Lafayette, IN 47907-2045, USA;

    School of Aeronautics and Astronautics, Purdue University, 701 W. Stadium Ave, West Lafayette, IN 47907-2045, USA,School of Materials Engineering, Purdue University, 701 W. Stadium Ave. West Lafayette, IN 47907-2045, USA;

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