因科镍合金
表面完整性
材料科学
微观结构
残余应力
压痕硬度
表面粗糙度
冶金
航空航天
合金
表面光洁度
变形(气象学)
复合材料
工程类
航空航天工程
作者
Xiao Jiang Cai,Shengfeng Qin,Qing Long An,Ming Chen
出处
期刊:Advanced Materials Research
日期:2012-04-01
卷期号:500: 51-57
被引量:10
标识
DOI:10.4028/www.scientific.net/amr.500.51
摘要
nconel 718 is a typical difficult-to-machine material, and its high speed end milling process has wide applications in manufacturing parts for aerospace and power industry. Surface integrity of these parts greatly influences the final characteristics. This paper presents an experimental investigation to evaluate surface integrity behaviors of Inconel 718 with finishing cutting parameters in terms of surface topography, surface roughness Ra, residual stresses and subsurface microstructure and microhardness. The results show that high cutting speed is advisable to get better surface topography and roughness. Residual stresses and subsurface microhardness barely increase after 80m/min. Microstructure in surface layer has only slight deformation after high speed milling.
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