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Parameters identification of mechanical behaviour law for polyether-ether-ketone composites.

Abstract: Mechanical properties of neat poly-ether-etherketone (PEEK), reinforced PEEK with 30 (wt%) carbon fibres (PEEK CF 30) and filled PEEK with 15.8 (wt%) carbon nanotubes (PEEK Nano) were investigated at compression test for differing strain-rates. The G'Sell-Jonas phenomenological model was used to describe the flow curve of the PEEK composites.

Key words: mechanical law, parameters, polyether-etherketone, composites

1. INTRODUCTION

Poly-ether-ether -ketone polymer is a linear aromatic semi-crystalline thermoplastic with excellent mechanical properties (Zhang et al., 2004). Capable of being processed on conventional thermoplastic equipment, PEEK is a high performance material and has been used as matrix for advanced polymer composites. PEEK is used in applications that need high loading for long period at high temperature without permanent deformation. However, the tensile strength of PEEK exceeds that of most usual polymers. Due to their properties, carbon fibres are the reinforcement currently used in high performance thermoplastic composite. Carbon fibres reinforced PEEK is one of the best thermoplastic composite. Otherwise, in order to improve thermal and electrical behavior, PEEK matrices are filled with carbon nanotubes. The mechanical properties of PEEK composites mostly depend on fillers and fibers reinforcement (Ogasawara et al., 2011). After the parameters identification of mechanical behaviour law the next step will be the implementation of the behaviour law in ABAQUS Software for validation.

2. THEORETICAL

Rheology of polymer matrix makes difficult to predict the flow curve of composite under compression test, so that a simply model could not describe well such behaviour. A constitutive equation, including involved parameters (displacement, load, time and temperature) is needed to represent the whole phenomenon, just by modifying a limited number of parameters. A global relationship that describes the rheological behaviour of polymer matrix can be expressed as follows:

[bar.[sigma]] = f([lambda], [bar.[epsilon]], [??], T) (1)

where: [bar.[sigma]] is the true stress, [bar.[epsilon]] is the true strain, [lambda] represents material coefficients, [??] is the strain-rate, and T is the absolute temperature. For the purpose of this discussion, we used a multiplicative model for semi-crystalline polymers proposed by G'Sell and Jonas (Rezgui et al., 2011; G'Sell, 1988), according to the equation (2). The applicability of G'Sell-Jonas model for semi-crystalline polymers at different strain-rates was shown by many researchers (Rezgui et al., 2011; Schossig et al., 2008).

[bar.[sigma]] = K x f([bar.[epsilon]]) x g([??]) (2)

f([bar.[epsilon]]) = V([bar.[epsilon]]) x Y ([bar.[epsilon]]) x H([bar.[epsilon]]) (3)

g(??]) = [[??].sup.m] (4)

The equation (3) can be divided into three terms: the first term V([bar.[epsilon]]) = 1 - [e.sup.-w x [bar.[epsilon]]], refers to a Maxwell viscoelasticity up to the yield point, w is the viscoelastic coefficient; the second term, Y([bar.[epsilon]]) = 1 + [alpha] x [e.sup.-b x [bar.[epsilon]]], describes the softening portion of the stress--strain curve, where a and b are softening coefficients; the third term of the equation (3) refers to the plastic strain hardening, [MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], where h and n are hardening coefficients. The equation (4) describes the strain-rate g([??]) = [[??].sup.m], where m is the sensitivity coefficient to the strain- rate. In the equation (2), K is the consistency of the material.

3. EXPERIMENTAL DETAILS AND MATERIALS

To determine the mechanical behavior, we used the quasi-static compression test for three materials, PEEK, PEEK CF 30, and PEEK Nano. Tests were performed using an INSTRON 3369 testing machine (Fig.1). The samples were cylinders with 6 mm diameter and 9 mm height, in order to avoid material buckling during testing. Compression tests of the samples were performed at 23[degrees]C for three compression speed, 0.5 mm/min, 5 mm/min and 10 mm/min, corresponding to following initial generalized strain-rate: 1 x [10.sup.-3][s.sup.-1], 1 x [10.sup.-2][s.sup.-1], 2 x [10.sup.-2][s.sup.-1] (Fig. 2). We assume that the material is homogeneous and isotropic, and the coefficient of friction between specimen and the platen of the testing machine is neglected.

[FIGURE 1 OMITTED]

[FIGURE 2 OMITTED]

4. RESULTS AND DISCUSSION

The flow curve, according to G'Sell-Jonas model, was found using only mechanical behavior parameters of each material (Figs. 1, 2, 3). Rheological parameters were calculated successively, taking into account the corresponding strain domain. The first parameter obtained was the sensitivity to the strain-rate, m. In the second step, parameters K and w were calculated from the stress-strain curve. Hardening coefficients h and n=2 (G'Sell, 1988), were analyzed on the largest strain sub domain, in the third step. The yield-drop sub domain is described by the parameters a and b, only in the case of neat PEEK. The values of the flow curve parameters for three materials, calculated on the basis of experimental data, are shown in the Table 1.

[FIGURE 3 OMITTED]

[FIGURE 4 OMITTED]

[FIGURE 5 OMITTED]

Neat PEEK shows a typical polymer yield point as compared to its composites, followed by a softening range, and a roughly straight sub domain up to 0.4 value of strain.

Due to the effect of the additives, the two composites (PEEK CF 30 and PEEK Nano) show a different behaviour related to the neat PEEK, and a larger viscoelastic sub domain is determined by smaller values of the w parameter.

Carbon fibres and carbon nanotubes make maximal stress to increase, while the smallest sensitivity to the strain-rate can be noticed in the case of PEEK CF 30 composite (m takes smallest value). Also, it can be seen on the figures 4 and 5 that no softening range appears for PEEK CF 30 and PEEK Nano composites.

5. CONCLUSION

The calculated constitutive parameters applied to G'Sell-Jonas model describe fairly well the mechanical behavior of the materials tested, according to experimental data. Parameters values are valid for a function [bar.[sigma]]([bar.[epsilon]]; [??]) that describes the deformations for the three materials at strain- rates in the range 1 x [10.sup.-3] [s.sup.-1] - 2 x [10.sup.-2][s.sup.-1]. The yield strength get highest value in the case of PEEK CF 30, while no significant increase was recorded for PEEK Nano composite.

For small deformations and high stress, the best behavior was noticed in the case of PEEK CF 30, owing the reinforcement with carbon fibers that enhances mechanical strength of material.

6. ACKNOWLEDGEMENTS

The work of Dan Trufasu and Aida Besnea was supported by Project SOP HRD--SIMBAD 6853, 1.5/S/15-01.10.2008

7. REFERENCES

G'Sell, C. (1988). Instabilites de deformation pendant l'etirage des polymeres solides (Deformation instabilities during stretching of solid polymers). Revue de Physique Appliquee, Vol. 23, No. 6, 1085-1101, http://hal.archivesouvertes.fr/jpa-00245911/en/

Ogasawara, T.; Tsuda, T. & Takeda, N. (2011). Stress-strain behavior of multi-walled carbon nanotube/PEEK composites. Composites Science and Technology, Vol. 71, No. 2, (January 2011) 73-78, ISSN 0266-3538

Rezgui, F.; G'Sell, C.; Dahoun, A.; Hiver, J.M. & Sadoun, T. (2011). Plastic deformation of Low-Density Polyethylene reinforced with biodegradable polylactide, part 2: creep characterization and modeling. Polymer Engineering & Science, Vol. 51, No. 1, (January 2011) 126-132, ISSN: 1548-2634

Scholssig, M.; Bierogel, C.; Grellmann, W. & Mecklenburg, T. (2008). Mechanical behavior of glass-fiber reinforced thermoplastic materials under high strain rates. Polymer testing, Vol. 27, No. 7, (October 2008) 893-900, ISSN 0142-9418

Zhang, Z.; Breidt, C.; Chang, L. & Friedrich, K. (2004). Wear of PEEK composites related to their mechanical performances. Tribology International, Vol. 37, No. 3, (March 2004), 271-277, ISSN 0301-679X
Tab. 1. Constitutive parameters of the flow curve

                    Parameters of G'Sell-Jonas model

Materials      K       w       m      a      b      h    n

PEEK         141.1   28.27   0.015   1.27   24.2   --    --
PEEK CF 30   183.4   35.7    0.008    --     --    --    --
PEEK Nano    156.3   41.4    0.023    --     --    0.3   2
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Author:Trufasu, Dan Catalin; Besnea, Maria Aida Cristina; Andrei, Gabriel; Dima, Dumitru
Publication:Annals of DAAAM & Proceedings
Article Type:Report
Geographic Code:1USA
Date:Jan 1, 2011
Words:1286
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