DocumentCode
3528943
Title
Near-dry cutting of difficult-to-cut materials Tool wear characteristics of a cemented carbide tool
Author
Wakabayashi, Tetsushi ; Maeda, Yuji ; Kato, Kazuhiko ; Yazawa, Takanori
Author_Institution
Dept. of Intell. Syst. Design Eng., Toyama Prefectural Univ., Toyama, Japan
fYear
2012
fDate
11-14 Nov. 2012
Firstpage
1
Lastpage
6
Abstract
Titanium alloys and Inconel 718 are used in airplane bodies. Pure titanium alloys are used in medical equipment. Wet cutting, which generates a significant amount of cutting fluid, is adopted for the cutting of these difficult-to-cut materials. When near-dry cutting, which is environmentally friendly, is used instead, it easily damages tools, and the stock removal rate and machining accuracy worsen. Thus, in this study, we attempted to clarify and develop a reduction method to generate a mechanism for the cutting-edge fracture in the cylindrical cutting of difficult-to-cut materials. We also examined the relationship between the cutting distance and cutting tool wear as a coefficient of friction on a rake face and tool wear when cutting of the difficult-to-cut materials.
Keywords
aircraft; cermets; cutting; cutting tools; environmental factors; fracture; mechanical engineering; titanium alloys; wear; Inconel 718; airplane bodies; cemented carbide tool; cutting distance; cutting fluid; cutting-edge fracture; cylindrical cutting tool wear characteristics; difficult-to-cut materials; environmental friendly; machining accuracy; medical equipment; near-dry cutting; rake face friction; reduction method; stock removal rate; wet cutting; Cutting tools; Feeds; Force; Materials; Rough surfaces; Surface roughness; Titanium alloys; Inconel718; cemented carbide tool; cutting tool wear; titanium alloy;
fLanguage
English
Publisher
ieee
Conference_Titel
Renewable Energy Research and Applications (ICRERA), 2012 International Conference on
Conference_Location
Nagasaki
Print_ISBN
978-1-4673-2328-4
Electronic_ISBN
978-1-4673-2329-1
Type
conf
DOI
10.1109/ICRERA.2012.6477387
Filename
6477387
Link To Document