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Effect of Tool Wear on Subsurface Deformation

of Nickel-based Superalloy

J M Zhou, V Bushlya, Ru Peng, Sten Johansson, P Avdovic and J-E Stahl

Linköping University Post Print

N.B.: When citing this work, cite the original article.

Original Publication:

J M Zhou, V Bushlya, Ru Peng, Sten Johansson, P Avdovic and J-E Stahl, Effect of Tool

Wear on Subsurface Deformation of Nickel-based Superalloy, 2011, Procedia Engineering,

(19), 407-413.

http://dx.doi.org/10.1016/j.proeng.2011.11.133

Copyright: Elsevier. Under a Creative Commons license

http://www.elsevier.com/

Postprint available at: Linköping University Electronic Press

http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-73804

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Procedia Engineering 19 ( 2011 ) 407 – 413

1877-7058 © 2011 Published by Elsevier Ltd. doi: 10.1016/j.proeng.2011.11.133

1

st

CIRP Conference on Surface Integrity (CSI)

Effects of Tool Wear on Subsurface Deformation of

Nickel-based Superalloy

J. M. Zhou

a

aDivision of Production and Materials Engineering, Lund University, Sweden

*, V. Bushlya

a

, R. L. Peng

b

, S. Johansson

b

, P. Avdovic

c

, J-E. Stahl

a bDivision of Engineering Materials, Linköping University, Linköping, Sweden

cSiemens Industrial Turbomachinery AB, Finspång, Sweden

Abstract

Increased demand of energy efficiency for the components used in aerospace and energy industries requires high efficiency and low cost in the production of component made of nickel-based superalloy, such as aged Inconel 718. With use of whisker reinforced ceramic cutting tool in finishing machining process, higher cutting speed and higher production efficiency can be reached accordingly. However, surface integrity of the part produced by this process still needs to be studied due to the high demand of surface quality. The paper analyses the effects of tool wear on subsurface deformation of nickel-based super-alloy in finishing turning. The objective is to understand the nature of subsurface deformation under the influence of tool wear for prediction of the surface integrity in machined components based upon the machining conditions and material behaviours that give rise to them. Machined samples were studied under a Backscattered electron microscope to distinguish the subsurface features produced by the machining. The electron back scatter diffraction (EBSD) was also used to quantify the depth of deformation zones in the subsurface after the machining.

© 2012 Published by Elsevier Ltd. Selection and peer-review under responsibility of Prof. E. Brinksmeier

Keywors: Surface integrity, Wear, Nickel alloy, Machinability, Turning

1. Introduction

Among the factors affecting surface integrity, subsurface deformation produced by machining process is one of essential factors to determine the mechanical properties of the material beneath the machined surface, such as residual stresses, hardness, and fatigue strength and has substantial influence to the

* Corresponding author. Tel.: 46 46 2228601; fax: 46 46 2224529.

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408 J.M. Zhou et al. / Procedia Engineering 19 ( 2011 ) 407 – 413

performance and life time of final products. Subsurface deformation is inherent to a metal cutting process [1], where a sharp tool is used to remove a preset depth of material by moving in a direction perpendicular to its cutting edge and produces the chip with thickness. Deformation occurs by shear concentrated in a narrow zone (shear plane). The shear zone is formed by shearing the workpiece material. The plastic deformations are also introduced as the result of friction at the interface of chip/rake face and surface/flank face, and the area where the workpiece material is deformed and separated under the high compressive stresses. Nickel based superalloy is well-known as one of the most difficult materials to machine due to high cutting temperatures and high strength encountered during the machining. The finishing operations of aerospace parts are commonly conducted by using WC tools at relatively low cutting speeds (30 – 60 m/min) due to the uncertainty of surface quality produced with other tool materials and their associated operation parameters [2]. In recent years, with consideration of sustainable development and environmental issues, there is an increase demanding on energy efficiency of the component in aerospace and power industry, which brings the large challenges on the machining of nickel-based superalloy with more aggressive cutting conditions, such as high speed machining with use of ceramic and CBN cutting tools, for the purpose of higher production efficiency and lower cost [3-4]. However, it is essential to have full knowledge of surface integrity produced by a novel machining process in order to predict the life time of the machined part. Objective of the presented study is to determine the effect of tool wear on the subsurface deformation of nickel-based superalloy, in particularly Inconel 718, produced with whisker reinforced ceramic cutting tool at the finishing cutting condition in terms of subsurface features, microstructure and deformation depth.

Fig. 1. (a) Microstructure of received work material. (b) Surface and subsurface layer upon machining at vc= 300 m/min, f = 0.2

mm/rev. and ap= 0.3 mm with new cutting tool.

2. Experimental setup

A typical nickel-based superalloy, Inconel 718, was used in the cutting test. The material was solution annealed and aged to a nominal bulk hardness of 45±1 HRC, and received as a bar shape with diameter of 70 mm and 200mm in length. The original workpiece was machined down to 40 mm in diameter for convenience of cut-off after machining test. The material has a chemical composition of 53.8 % Ni, 18.1 % Cr, 5.5 % Nb, 2.9 % Mo, 1 % Ti, 0.55 % Al, 0.25 % C, 0.04 % Si and balance Fe (weight percent). Material has grain sizes ranging from 2 to 20 Pm, as shown in Fig. 1(a). The microstructure consists of a J matrix (fcc structure) with precipitates of G-phase (Ni3Nb) and is strengthened by coherent J´´

precipitates, a metastable Ni3Nb phase (BCT structure).

Whisker reinforced alumina ceramic (Al2O3+SiCw) with honed cutting edge, with an edge radius of 20

Pm, and negative rake chamfer (0.1 x 20º) was employed throughout the cutting tests. The insert was mounted in the tool holder with tool geometryí6º of rake angle, 6º of clearance angle 93º of approach angle and íž of cutting edge inclination angle. Type CDJNL3025P11 (ISO) tool holder was used. New

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tool, semi-worn tool and worn tool were used in the test. Cutting parameters for typical finishing machining operation were selected during the cutting tests with cutting speed, vc= 300 m/min, feed, f =

0.2 mm/rev. and depth of cut, ap= 0.3 mm. Coolant was used throughout the tests. The selected cutting

parameters also covered typical industrial application in the finishing machining of this workpiece material with whisker reinforced ceramic cutting tool. New tool, semi-worn tool with VBmax= 0.15 mm

and worn tool with VBmax= 0.3 mm were employed in the cutting tests. The selected values for VBmax

represent the middle and the end of tool life during the machining. All machining trials were conducted on a SMT500 CNC turning machine with spindle speed up to 4000 rpm and a drive motor rated up to 70kW.

Backscattered electron (BSE) microscopy and EBSD techniques were used to assess the microstructure of polished samples. All the BSE studies were carried out on a Hitachi SU-70 FED electron scanning microscope equipped with EBSD set-ups from Oxford Instrument. EBSD measurements were taken on a high-resolution field emission gun (FEG) at a working distance of 20 mm and accelerating voltage of 20 kV. Channel-5 software from HKL technology was used to analyze the EBSD measurements.

Fig. 2.BSE images showing the effect of tool wear, (a) new tool, (b) semi-worn tool, (c) worn tool, on extent of subsurface deformation and microstructure modification and (d) refinement of microstructure.

3. Results and discussions

3.1. Plastic deformation

The BSE image shown in Fig. 1(b) reveals a typical morphology of subsurface deformation after machining with cutting speed of 300 m/min and new cutting tool. This BSE images confirmed that the subsurface is affected by the cutting process. Three zones were observed in the Fig. 1(b) in the machined subsurface region. Zone 1 is heat affected zone which includes the surface and near surface region. The workpiece material in this region was strongly affected by both mechanical (friction force) and local thermal load generated in the machining. In some cases, the surface topography in this area clearly demonstrates the feature of re-solidification rather than shearing under the cutting forces, which indicates that the temperature experienced in this region is close to melting temperature of the material (1260 ~

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410 J.M. Zhou et al. / Procedia Engineering 19 ( 2011 ) 407 – 413

1336ºC [4]) during the machining. In fact, the temperature on flank face was measured up to 1100 ºC with

embedded thermocouple by Kitagawa [5] in high speed machining of Inconel 718. The microstructure of heat affected zone was characterized by nanocrystalline structure with about 1~2 µm thickness, as shown in Fig. 2(d). The nanocrystalline layer is believed to be generated under the condition of high cutting speed and large tool flank wear [6]. Additional heat input during the cutting, as the consequences of higher cutting speed, is assumed to be responsible for generation of nanocrystalline layer. In the deformation zone (zone2), deformation layer was clear identified by severe bending and elongation of grain boundaries and slip bands. The intensity of deformation is reduced as depth increase from top surface until it reaches the bulk (zone3) with undeformed material.

Fig. 2(a), (b) and (c) demonstrate the effect of tool wear on the deformation of subsurface layer when tool changes from new, semi-worn and worn tool. The deformations and slip in grain boundaries and elongation of grains indicate the severe plastic deformation in the subsurface layer. When cutting with a new tool, both cutting force and cutting temperature were relatively low in comparisons to worn tool, small plastic deformation was induced at the subsurface layer (Fig. 2(a)). However, surfaces produced with semi-worn tool (VBmax= 0.15 mm) and worn tool (VBmax= 0.3 mm) had greater levels of plastic

deformation at the subsurface layer, as presented in Fig. 2(b) and (c). This can be explained by the fact that with increasing tool wear, the tool/workpiece contact area is increased due to reduced clearance angle on the tool, which create more rubbing of the workpiece surface and rise both temperature and total cutting force. In general, localized heating and high stresses due to increased forces are considered as the major reason for change on subsurface layer. Sharman et al. [7] have also shown that when machining Inconel 718 with worn cutting tools, cutting forces of between three and ten times those obtained with new cutting tools are generated, with associated increase in the depth of microstructure deformation. The effects of tool wear on the subsurface deformation may be attributed to both mechanical and thermal effects [9]. The mechanical effect is associated with more superficial shear between tool flank and workpiece surface due to increased tool wear. The thermal effect is generated by friction. A higher and larger temperature field is generated due to the larger friction at the interface of flank/workpiece. The direct effect of the increased temperature on the subsurface layer is an additional plastic deformation due to the constrained thermal expansion.

When tool wear increases from initial condition (VBmax= 0) to worn tool (VBmax= 0.3mm), the zone

with recrystallized microstructure was observed, as shown in Fig.2(c). A close view of the heat affected zone in Fig. 2(c) was presented in Fig. 2(d), which clearly demonstrates the material with grain size of

200 ~ 300 nm and they are much smaller than the grains (2 – 20Pm) in the bulk area. The nano grain size

confirmed recrystallization of the material in near surface region. The thermal (high temperature and rapid quenching) and mechanical (high stress and strain) effects are the main reasons for the microstructure alterations in the material [10]. On the right part of Fig. 2(d) demonstrates the recrystallization grains in the immediate subsurface of the machined workpiece with layer thickness of ~2

Pm produced with worn tool. Partly recrystallized area was found below the depth of 2Pm, as shown on

the left part of the Fig. 2(d). As the tool wears, increase of the layer of recrystallization and the total plastic deformation beneath the machined surface was observed.

3.2. EBSD assessment

Although different zones are evident in BSE images, more detailed information is required to characterize them and identify their origin. Electron backscatter diffraction (EBSD) microscopy provides grain orientation as well as information about intragranular misorientations [11]. In EBSD analysis, the characteristic diffraction pattern (the so called Kikuchi bands) generated by backscattered electrons is used to determine the crystallographic orientation of the measured point. By scanning a surface area in a predetermined grid, a crystallographic orientation map can be obtained and quantitative information about

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the lattice orientation changes associated with plastic deformation within individual grains can be derived in the form of misorientation angle distribution. The EBSD analysis was carried out on a Hitachi SU-70 FED electron scanning microscope equipped with EBSD set-ups from Oxford Instrument. Line scanning was employed to obtain crystallographic orientation information, given as Euler angles, I1, Iand I2 for

each measured point. An area of  ȝP by  ȝP stretching from the machined surface into sample

depth was measured in 0.5 micrometer resolution. A misorientation angle falling within the range of 2o and 5oare denoted by green line and within the range of 6oand 15oare indicated with red line in Fig. 3(a), (b) and (c) respectively. From the measurements, orientation maps were constructed using Channel 5 software to visualize the variation of deformation microstructure with sample depth, which is indicated by the distribution of plastic deformation induced misorientation angles.

Fig.3. EBSD maps showing the depth of plastic deformation in subsurface layer from (a) new tool, (b) semi-worn tool, (c) worn tool and (d) microstructure recystallization.

Fig. 4. (a) Misorientation within grains beneath the machined surface (direction of linescan perpendicular to the machined surface) (b) Depth of subsurface deformation in machined material proportional to resultant cutting force.

Fig. 3(a) - (c) show the EBSD maps obtained from subsurface layer machined with different tool conditions. It is evident that the lattice rotation due to the deformation increases towards the machined

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412 J.M. Zhou et al. / Procedia Engineering 19 ( 2011 ) 407 – 413

surface as shown in Fig. 3(a) and (c). The sub-grain boundaries and the associated gradients provide evidence of increasing intragranular misorientation and plastic activity. A high density of subgrain boundaries is found in the region beneath the surface as a result of large deformation in this region after the machining operation. This machining affected region consist of a heavy deformation layer with misorientation angles homogenously spread over the grains and a partially deformed layer where misorientation angles distributed mostly around grain boundaries. Grains in the heavy deformation layer also became elongated and tended to bend towards the cutting direction as observed in BSE. Fig. 3(a) shows that when new tool was used, deformations are mostly concentrated in a very thin surface layer and the thickness of heavy deformation layer is of the order of ȝP. This layer is extended deeper from the

machined surface and reached about ȝP depth when worn tool was used, as shown in Fig. 3(c). The

distribution of grains in subsurface area of  ȝP by  ȝP for new, semi-worn and worn tool in

comparison to bulk material was presented in Fig. 3(d). Fig. 4(a) represents the change of misorientation versus the depth of subsurface layer in the machined surface from new tool, semi-worn tool and worn tool, derived from measurements on 120 lines. The deformation depth for surface machined with worn tool can be as much as 250Pm. Fig. 4(b) confirmed that the mechanical (stress and strain) effects are

associated with the increase of the subsurface deformation.

4. Conclusions

In the presented work, an attempt has been made to characterise the subsurface deformation of Inconel 718 after machining with whisker reinforced ceramic tool. Backscattered electron (BSE) microscopy and EBSD techniques were used to analysis and quantify the deformation zone on subsurface after machining. The results indicate that the impacts of subsurface deformation from a machining process are governed by not only the process parameters selected, but also tool wear during chip formation. The levels of tool wear have major contribution to the change of subsurface deformation depth and microstructure. This may be attributed to the rise of the thermal/mechanical load acting on the machined surface as the result of the tool wear. Recrystallization layer and partly recrystallization layer were observed in the immediate subsurface of the workpiece with grain size of 200~300 nm, which is dependent on tool wear. The depth of deformation zone can be effectively characterised by EBSD techniques.

Acknowledgements

Authors also would like to acknowledge Swedish Strategic Foundation (SSF), Swedish Institute for their financial support in the investigation within the ShortCut project and the frame of Sustainable Production Initiative (SPI).

References

[1] Jahanmir S and Suh PN, Surface topography and integrity effects on sliding wear, J Wear 1977;44:87-99.

[2] Jeelani S and Ramakrishnan K, Subsurface plastic deformation in machining annealed 18% Ni maraging steel, J Wear 1982; 81:263-273.

[3] El-Wardany TI, Mohammed E. and Elbestawi MA, Cutting temperature of ceramic tools in high speed machining of difficult-to-cut materials. Int J Machine Tool and Manufacturing, 1996; 36(5):611-634.

[4] Arunachalam, R. and M. A. Mannan, Machinability of Nickel-Based High Temperature Alloys, Machining Science and

Technology, 2000; 4(1):127–168.

[5] Kitagawa T, Kubo A, Maekawa K, Temperature and wear of cutting tools in high speed machining of Inconel 718 and Ti-6Al-6V-2Sn, J Wear, 1997; 202:142-148

[6] Sims CT, Stoloff NS, Hagel WC, Superalloy II, John Wiley & Sons. Toronto, 1987

[7] Sharman ARC, Hughes JI and Ridgway K, An analysis of the residual stress generated in Inconel 718 when turning. J

Material Processing, 2006;173: 359-367.

[8] Schlauer C and Oden M, Residual stress evolution and near-surface microstructure after turning of the nickel-based superalloy Inconel 718. Zeitschrift fur Metallkunde. 2005;96: 385-392.

[9] Liu CR and Barash MM, The mechanical state of the sublayer of a surface generated by chip-removal process, Transaction of ASME, Journal of Industrial Engineering, 1976;1192-99.

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[11]Saoubi RM and Ryde L, Application of the EBSD technique for the characterisation of deformation zones in metal cutting.

References

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