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Effects of machine stiffness on the loading–displacement curve during spherical nano-indentation

Published online by Cambridge University Press:  27 June 2013

Weidong Li
Affiliation:
Department of Materials Science and Engineering, University of Tennessee, Knoxville, Tennessee 37996
Hongbin Bei*
Affiliation:
Materials Science and Technology Division, Oak Ridge National Laboratory, Oak Ridge, Tennessee 37831
Jun Qu
Affiliation:
Materials Science and Technology Division, Oak Ridge National Laboratory, Oak Ridge, Tennessee 37831
Yanfei Gao*
Affiliation:
Department of Materials Science and Engineering, University of Tennessee, Knoxville, Tennessee 37996; and Materials Science and Technology Division, Oak Ridge National Laboratory, Oak Ridge, Tennessee 37831
*
a) Address all correspondence to these authors. e-mail: beih@ornl.gov
b) e-mail: Ygao7@utk.edu

Abstract

By taking the machine stiffness into the classic Hertzian solution rather than assuming a constant machine stiffness, we developed an approach to simultaneously derive the spherical indenter tip radius and machine stiffness in arbitrary ranges of loads and indenter radii. In contrast, the direct Hertzian fitting method tends to underestimate the radius, especially for larger indenter tips. The success is based on indention tests on two materials with known material stiffness, and the displacement difference under the same load is not affected by the machine stiffness. A total of eight spherical indenter tips with the radii ranging from a few microns to hundreds of microns have been indented on fused silica and single crystal sapphire. Our method gives correct indenter radii for all indenters. The machine stiffness is found to indeed vary with the indentation load and indenter radius. This method has many potential applications in the area of nano-indentation with spherical indenters, such as indentation size effect, modulus and hardness measurement, and micropillar testing.

Information

Type
Articles
Copyright
Copyright © Materials Research Society 2013 
Figure 0

FIG. 1. (a) Schematic illustration of the instrumented indentation system (reproduced after Oliver and Pharr1) and (b) schematic diagram showing that the experimentally measured displacement is the sum of the loading frame deflection, hmachine, and the penetration into the sample, hsample, i.e., htotal = hsample + hmachine.

Figure 1

FIG. 2. Line scan and three-dimensional view of the indentation impression on tin characterized by a white light interferometer, from which the indenter tip radius can be determined. Dash curve represents the spherical tip with a radius of 253 μm.

Figure 2

TABLE I. Indenter tip radii provided by the manufacturer (denoted as nominal), measured by the optical image of the indentation impressions on tin, derived by fitting to Eq. (1) and by our subtraction method in Eq. (8) using two materials (sapphire and fused silica). The corresponding machine stiffness can be fitted to the form of ${S_{{\rm{machine}}}} = {S_0} + kP$.

Figure 3

FIG. 3. Determination of the indenter tip radius. (a) Experimental P–hreported data on sapphire and fused silica using the Tip #2 indenter, shown by symbols. Direct Hertzian fitting is shown by the black solid curves and the Hertzian solutions with indenter radii obtained from our subtraction method are given by the red dashed curve. (b) The subtraction method is used to fit hfs − hsp (fs: fused silica; sp: sapphire) to $P^{{2 \mathord{\left/ {\vphantom {2 3}} \right. \kern-\nulldelimiterspace} 3}} $ as in Eq. (8). The slope can be used to determine the indenter tip radius.

Figure 4

FIG. 4. Load–displacement curves using the small tip-radius indenter (Tip #7). Symbols represent experiment P–hreported curves. Direct Hertzian fitting by using Eq. (1) is shown by the black solid curves and the Hertzian solutions with indenter radii obtained from our subtraction method are given by the red dashed curve. Note that the black solid curves overlap the red dashed curve.

Figure 5

FIG. 5. Maximum indentation loads and deviation loads for various indenters. The deviation load denotes load where the Hertzian solutions deviate noticeably from experimental P–hreported curves, as shown in Fig. 3(a). For small indenters, negligibly tiny deviation occurs, and the maximum loads equal to the deviation loads. The deviation load is around 0.05 N for the large indenters.

Figure 6

FIG. 6. Machine stiffness under different loads with selected indenter tips. The machine stiffness approximately shows linear dependence on the load and can be described with ${S_{{\rm{machine}}}} = {S_0} + kP$, in which fitting parameters k and S0 can be found in Table I. For small indenters, the calculated machine stiffness is close to the predefined machine stiffness, Sdefault = 9.1 N/μm. Machine stiffness at loads below 10% of the maximum load was not calculated because of great system errors.

Figure 7

FIG. 7. Plots of contact stiffness versus load for the two materials using large indenter Tip #2 in (a) and small indenter Tip #7 in (b).