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Experimental and Finite Element Simulation Study of Thermal Relaxation of Residual Stresses in Laser Shock Peened IN718 SPF Superalloy

机译:激光冲击强化IN718 SPF高温合金残余应力热松弛的实验和有限元模拟研究

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An integrated experimental and modeling/simulation approach was developed to investigate and secure a quantified knowledge of the impact of high temperature exposures on the stability of residual stresses in a laser shock peened (LSP) high temperature aero-engine alloy, IN718 SPF (super-plastically formed). Single dimple LSP and overlap LSP treatments were carried out utilizing a Nd:Glass laser (lambda = 1.052 mu m), and subsequent heat treatments on the LSP-treated coupons were conducted at different temperatures between 550 and 700 A degrees C. A 3-D nonlinear finite element (FE) computational model and the rate-dependent Johnson-Cook material model were calibrated using the experimental results of residual stress from the single dimple LSP and thermal relaxation treatments, and were further extended to the overlap LSP treatment case. Both experimental and FE simulations show that: a) a high level of compressive residual stress (similar to 700 MPa at surface) and residual stress depth (similar to 0.4-0.6 mm) were achieved following LSP, and b) the overlap LSP treatment gave higher residual stress and greater depth. The magnitudes of the initial residual stress (and plastic strain), heating temperature and exposure time were identified as the key parameters controlling the thermal relaxation behavior. The stress relaxation mainly occurs initially before 20 min exposure and the extent of relaxation increases with an increase in temperature and a higher m(a)gnitude of the initial as-peened residual stress. In addition, in regions deeper than similar to 300 mu m or after initial thermal exposure where the residual stress was lower than similar to 300 MPa, stress relaxation was found to be negligible. Kinetic analysis of the experimental thermal relaxation data based on Zener-Wert-Avrami model gave an activation enthalpy of 2.87 to 3.77 eV, which is near that reported in the literatures for volume and/or substitutional solute diffusion in Nickel. These results suggest that thermal relaxation of the LSP-induced residual stress occurs by a creep-like mechanism involving recovery, rearrangement and annihilation of dislocations by climb.
机译:开发了一种集成的实验和建模/模拟方法,以研究并获得关于高温暴露对激光冲击喷丸(LSP)高温航空发动机合金IN718 SPF(超高强度合金)中残余应力稳定性的影响的定量知识。塑性成型)。使用Nd:玻璃激光(λ= 1.052μm)进行单凹坑LSP和重叠LSP处理,然后在550至700 A的不同温度下对LSP处理的试样进行后续热处理.A 3-利用单酒窝LSP残余应力和热松弛处理的实验结果,对D非线性有限元(FE)计算模型和依赖于速率的Johnson-Cook材料模型进行了校准,并将其扩展到重叠LSP处理案例。实验和有限元模拟均表明:a)LSP后获得了高水平的压缩残余应力(表面近似700 MPa)和残余应力深度(近似0.4-0.6 mm),并且b)重叠LSP处理得到了更高的残余应力和更大的深度。初始残余应力(和塑性应变),加热温度和暴露时间的大小被确定为控制热松弛行为的关键参数。应力松弛主要发生在暴露20分钟之前,松弛程度随温度的升高和初始残余应力的较高m(a)值而增加。另外,在比大约300微米深的区域或在初始热暴露之后残留应力低于大约300 MPa的区域,发现应力松弛可忽略不计。基于Zener-Wert-Avrami模型的实验热弛豫数据的动力学分析得出活化焓为2.87至3.77 eV,这与文献中有关镍中体积和/或置换溶质扩散的报道相近。这些结果表明,由LSP引起的残余应力的热松弛是通过蠕变样的机制发生的,该机制涉及通过爬升恢复,重排和位错ni灭。

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