Turning of Inconel 718 using inserts with cooling channels under high pressure jet coolant assistance

Abstract A large amount of cutting heat is generated in the turning process of nickel-base superalloy Inconel 718. This research proposed a new concept of inserts with cooling channels to enhance the heat transfer from the tool to coolant by generating turbulent flow in the flank clearance under the condition of high pressure coolant. Through and blind channels were made from the flank face and their influences on the wear and tool life were investigated in the longitudinal turning of Inconel 718. Energy dispersive spectroscopy analysis and computational fluid dynamics analysis were also conducted in addition to the cutting experiments. As a result, inserts with cooling channels decelerated flank wear rate and reduced the adhesion of workpiece material on the flank faces. The extension of tool life brought by the through channel was about twice larger than that done by ordinary tool in the high pressure jet coolant machining. However, the tool life extension advanced by the blind channel was limited to the turning at a small depth-of-cut. Computational fluid dynamics analysis clearly showed the differences in the coolant flow pattern caused by the through and blind channels, and concluded that their cooling abilities depend on the hydraulic pressure value and gradient, respectively.

[1]  Masashi Yamaguchi,et al.  Suppression of notch wear of a whisker reinforced ceramic tool in air-jet-assisted high-speed machining of Inconel 718 , 2015 .

[2]  Matthew S. Dargusch,et al.  New observations on tool life, cutting forces and chip morphology in cryogenic machining Ti-6Al-4V , 2011 .

[3]  B. Ramamoorthy,et al.  Study on the machinability characteristics of superalloy Inconel 718 during high speed turning , 2009 .

[4]  Dirk Biermann,et al.  Experimental studies and CFD simulation of the internal cooling conditions when drilling Inconel 718 , 2016 .

[5]  M. Bermingham,et al.  A comparison of cryogenic and high pressure emulsion cooling technologies on tool life and chip morphology in Ti-6Al-4V cutting , 2012 .

[6]  Xiaoping Li,et al.  Study of the jet-flow rate of cooling in machining Part 1. Theoretical analysis , 1996 .

[7]  J. P. Solano,et al.  Enhancement of laminar and transitional flow heat transfer in tubes by means of wire coil inserts , 2007 .

[8]  D. Biermann,et al.  Machining of β-titanium-alloy Ti–10V–2Fe–3Al under cryogenic conditions: Cooling with carbon dioxide snow , 2011 .

[9]  Masashi Yamaguchi,et al.  Computational Fluid Dynamic Analysis of Coolant Flow in Turning , 2013 .

[10]  Kadir Bilen,et al.  The investigation of groove geometry effect on heat transfer for internally grooved tubes , 2009 .

[11]  Jan C. Aurich,et al.  CFD based Investigation on Internal Cooling of Twist Drills , 2014 .

[12]  Peter Krajnik,et al.  Investigation of machining performance in high-pressure jet assisted turning of Inconel 718: An experimental study , 2009 .

[13]  Xiaoping Li,et al.  Study of the jet-flow rate of cooling in machining Part 2. Simulation study , 1996 .

[14]  James Wallbank,et al.  Cutting temperature: prediction and measurement methods—a review , 1999 .

[15]  Masashi Yamaguchi,et al.  Air jet assisted machining of nickel-base superalloy , 2012 .

[16]  S. Gangopadhyay,et al.  State-of-the-art in surface integrity in machining of nickel-based super alloys , 2016 .