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- 저자 : S. Kanmani Subbu (검색결과 2 건)
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R. Seetharam,Pagidi Madhukar,G. Yoganjaneyulu,S. Kanmani Subbu,M. J. Davidson 대한금속·재료학회 2022 METALS AND MATERIALS International Vol.28 No.4
Mathematical models are among the new approaches employed to predict the properties of any material under various conditions. Mathematical models are essential for not only understanding the material properties but also estimating the costof design, product life, and failure criteria of the product. Therefore, in the current investigation, the hot deformation (HD)behaviour and microstructure alteration of deformed AA7150-5 wt% B4Ccomposite was studied through a mathematicalmodel. The new AA7150-5 wt% B4C composite was fabricated through an ultrasonic-probe assisted (20 KHz, 1000 W)stir casting process. The hot compression test was performed on a hydraulic press for various deformation temperatures(623–773 K) and strain rates (0.01–1 s−1). Based on the outcome, it is inferred that the flow stresses and microstructuresof AA7150-5 wt% B4Ccomposite was significantly altered during the hot compression test under various deformationconditions. The constitutive and dynamically recrystallized grain (DRXed) models were developed as a function of variousdeformation conditions of deformed AA7150-5 wt% B4Ccomposite, which was then applied to forecast the flow stress andgrain size behaviour for different deformation conditions. The flow stress and DRXed grain size were obtained through theproposed constitutive and DRXed models are correlated with experimental results, with excellent accuracy. The modelsdeveloped are reliable to predict the AA7150-5 wt% B4Cproperties for various conditions.
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Post-Processing of Laser Additive Manufactured Inconel 718 Using Laser Shock Peening
A. N. Jinoop,S. Kanmani Subbu,C. P. Paul,I. A. Palani 한국정밀공학회 2019 International Journal of Precision Engineering and Vol.20 No.9
The components built using new generation feature based design and manufacturing process, called laser additive manufacturing (LAM) is inherited with tensile residual stress due to rapid heating and cooling during material processing. Laser shock peening (LSP) is an advanced surface engineering process that imparts beneficial compressive residual stresses into materials yielding longer product life by increasing the resistance to many surface-related failures, such as wear. LSP is widely used by various industries including aerospace, power generation, chemical processing, etc. to increase the life of engineering components. This paper reports LSP of LAM built Inconel 718 and the parametric study is conducted by varying peak laser power and number of shots at three different levels. Optimum laser power and number of shots derived using grey relational analysis is found to be 170 mW and 7, respectively for maximum hardness and minimum depth of profile. The investigation show that LSP changed the surface morphology and mechanical properties of the LAM built structure. The surface investigation using optical profilometer and Vickers micro-hardness shows a maximum profile depth of 10 μm and hardness of 360 HV. Residual stress measurement indicates compressive residual stress of 214.9–307.9 MPa on the LAM sample surface after LSP. The wear studies show an improvement by a factor of 1.70 for LSP treated LAM samples as compared to that of as-built condition. This study unwrap avenues for using LSP as property enhancement post-processing technique LAM fabricated structures with geometrical complexities.
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