کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
7153721 1462488 2018 11 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Surface integrity and fatigue behavior when turning γ-TiAl alloy with optimized PVD-coated carbide inserts
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Surface integrity and fatigue behavior when turning γ-TiAl alloy with optimized PVD-coated carbide inserts
چکیده انگلیسی
This paper presents a comprehensive investigation on the effects of tool and turning parameters on surface integrity and fatigue behavior in turning γ-TiAl alloy. The wear of inserts surface, cutting forces, and surface roughness were studied to optimize PVD-coated carbide inserts. Surface topography, residual stresses, microhardness, and microstructure were analyzed to characterize the surfaces layer under different turning parameters. Surface integrity and fatigue life tests of γ-TiAl alloy were conducted under turning and turning-polishing processes. The results show that compared to CNMG120412-MF4, CNMG120408-SM is more suitable because it obtained low cutting force, surface roughness, and tool wear. With increasing the cutting speed and depth, the depths of the compressive residual stress layer, hardening layer, and plastic deformation layer increased. For turning and turning-polishing specimens, the compressive residual stress was relaxed by less than 20%-30% after 107 cycles. The fatigue life of a turning-polishing specimen with Ra = 0.15 µm has increased 3 times from that of a turning specimen with Ra = 0.43 µm.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Chinese Journal of Aeronautics - Volume 31, Issue 4, April 2018, Pages 826-836
نویسندگان
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