Tool life and surface integrity aspects when drilling nickel alloy

International Conference on Recent Advances in Materials & Manufacturing Technologies

Kannan, S.^1 ; Pervaiz, S.^2 ; Vincent, S.^3 ; Karthikeyan, R.^3

Department of Mechanical Engineering, American University of Sharjah, P.O. Box 26666, Sharjah, United Arab Emirates^1

Department of Mechanical and Industrial Engineering, Rochester Institute of Technology - Dubai, P.O. Box 341055, Dubai, United Arab Emirates^2

Department of Mechanical Engineering, BITS Pilani, Dubai Campus, Dubai, United Arab Emirates^3

关键词: Circumferential direction;    High temperature strength;    Mechanical and thermal properties;    Nickel- based superalloys;    Operational efficiencies;    Residual stress profiles;    Surface integrity;    Tool life;   

Others  :  https://iopscience.iop.org/article/10.1088/1757-899X/346/1/012042/pdf
DOI  :  10.1088/1757-899X/346/1/012042

来源: IOP

【 摘 要 】

Nickel based super alloys manufactured through powder metallurgy (PM) route are required to increase the operational efficiency of gas turbine engines. They are material of choice for high pressure components due to their superior high temperature strength, excellent corrosion, oxidation and creep resistance. This unique combination of mechanical and thermal properties makes them even more difficult-to-machine. In this paper, the hole making process using coated carbide inserts by drilling and plunge milling for a nickel-based powder metallurgy super alloy has been investigated. Tool life and process capability studies were conducted using optimized process parameters using high pressure coolants. The experimental trials were directed towards an assessment of the tendency for surface malformations and detrimental residual stress profiles. Residual stresses in both the radial and circumferential directions have been evaluated as a function of depth from the machined surface using the target strain gauge / center hole drilling method. Circumferential stresses near workpiece surface and at depth of 512 μm in the starting material was primarily circumferential compression which was measured to be average of -404 MPa. However, the radial stresses near workpiece surface was tensile and transformed to be compressive in nature at depth of 512 μm in the starting material (average: -87 Mpa). The magnitude and the depth below the machined surface in both radial and circumferential directions were primarily tensile in nature which increased with hole number due to a rise of temperature at the tool-workpiece interface with increasing tool wear. These profiles are of critical importance for the selection of cutting strategies to ensure avoidance/minimization of tensile residual stresses that can be detrimental to the fatigue performance of the components. These results clearly show a tendency for the circumferential stresses to be more tensile than the radial stresses. Overall the results indicate that the effect of drilling and milling parameters is most marked in terms of surface quality in the circumferential direction. Material removal rates and tool flank wear must be maintained within the control limits to maintain hole integrity.