![]() ·Table of Contents ·Materials Characterization and testing | X-Ray Refraction Topography for Non-Destructive Evaluation of Advanced MaterialsBernd R. Müller, Manfred P. Hentschel,Karl-Wolfram Harbich, Axel Lange, Jörg Schors Federal Institute for Materials Research and Testing (BAM) D-12200 Berlin, Germany Contact |
| (1) |
Fig 1: Effect of oriented small angle scattering by refraction of glass fibres.
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Fig 2: The normalized shape of the angular intensity distribution of cylindrical objects.
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Fig. 3 demonstrates the X-ray deflection at circular objects (sections of fibres or spheres) by refraction and (very few) total reflection. In fibres and spherical particles the deflection of X-rays occurs twice, when entering and when leaving the object (Fig. 3, left). The intensity of the deflected X-rays falls down to nearly zero at the critical angle of total reflection (see Fig. 2 and Fig. 3, right). A cross section of 10-3 of the fibre diameter contributes to the detectable intensity above typically 2 minutes of arc. The effect of total reflection of X-rays occurs as well at the angle
Fig 3: X-ray deflection at circular objects by refraction and total reflection (left); angular intensity distribution for fibres and spheres (right) |
of grazing incidence but only 10-6 of the diameter is involved and therefore negligible. But well oriented planar surfaces can produce strong reflections. Based on Snell's Law the angular intensity distribution has been calculated and approximated for cylindrical fibre and spheres, as illustrated by Fig. 3. The refracted intensity of a cylinder without absorption effects can be expressed as[2]
| (2) |
Fig 4: SAXS instrumentation with primary X-ray beam, collimator, sample, sample manipulator, scattering foil, a refraction detector with a slit unit, which measures the refracted intensity of the sample (IR) or if the sample is not in place (IR0) and a reference detector, which measures the intensity I '0 or I ', which is proportional to I0 (without sample) or I (with sample), respectively. |
The refraction intensity can be measured according to Eq. (3). IR* depends on the transmitted intensity I, the thickness d and the inner surface density x = N × R (N is the amount of fibres) of the sample, respectively. The proportional factor k is a specific constant of the used apparatus and can be determined by measuring a probe with a known inner surface density.
| (3) |
| (4) |
The conventional understanding of "continuous" small angle X-ray scattering (SAXS) is governed by the interpretation of diffraction effects. Apart from Guinier's theory for separated particles Porod explains diffraction of densely packed colloids similar to Eq. (3). However both deal with particles two orders of magnitude smaller. A simple proof for the refraction effect at large objects can be found by scanning a fibre through a narrow X-ray beam and collecting the intensity at each fibre position (Fig. 5). Even focussing by pores is possible. The behaviour is exactly the same as in an experiment with visible light. Any diffraction effect would result in a symmetric intensity above background level.
Fig 5: X-ray refraction by a 125 mm polymer fibre is demonstrated by scanning a fibre through a narrow X-ray beam and collecting the intensity at each fibre position.
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Fig 6: Comparison of inner surface densities of selected non-metallic materials
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Fig 7: Pores in glass ceramics: micrograph, optical chordlength analysis of pores and pore diameter probability by X-ray Refraction
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The measurement of the crack density in light weight materials can be performed by X-ray refractometry as well. The knowledge of the crack development is believed to play the key role in all long-term material behaviour. Fig. 8 correlates the residual shear strength of CFRP to the average inner surface of cracks created by ageing treatment at 150°C, 180°C and 200°C up to 10,000 h. The investigation compares epoxy and BMI matrix systems for high temperature applications in supersonic aviation. Although BMI has a high strength at the beginning, it falls below epoxy at the end of the ageing treatment. The results explain clearly the dependence of the shear strength on the crack density. The slope defines an ageing module which can be regarded as a new materials parameter[6].
Fig 8: Correlation of the residual shear strength of CFRP to the average inner surface of cracks created by ageing treatment at 150 °C, 180 °C, 200 °C for 1,000, 3,000, 5,000, 10,000 h.
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Fig 9: Model of X-ray refraction at interfaces of bonded and debonded fibres of a composite, X-ray topography of model, investigation of single fibre debonding at different fibre volume ratios.
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Single fibre debonding in composites is not measurable - except by X-ray refractometry (although some attempts of pulling off individual fibres under the microscope have high artistic value). It is a central parameter of composites characterization. The basic principle can be understood by the optical analogue: compare the focussing properties of a lens in air (fibre in air) and in a liquid (fibre in matrix)! The refraction effect is lower in the second case. The density difference between fibre and matrix determines the X-ray scattering effect as well.
A model composite has been made in order to demonstrate the refraction behaviour of a debonded and a bonded 140 µm sapphire fibre in wax matrix (Fig. 9, left). The upper ray crosses the bonded fibre-matrix interface causing a small amount of deflected intensity. At the debonded fibre and at the matrix surfaces (lower ray) much more X-rays are deflected, as the larger density difference between the materials and air corresponds to a higher index of refraction.
The middle of Fig. 9 shows the resulting intensity distribution of a refraction scan of the model composite. The wax channel is clearly separated from the fibre surface. The bonded fibre is less contrasted. A practical measurement of the fraction of debonded fibres in a real thermoplastic C-fibre composite is given on the right of Fig. 9. There is a non-linear dependence of debonding on the fibre volume fraction. This can be explained by the very viscous thermoplastic matrix, which is hindered to penetrate between densely packed fibres during melt impregnation processing. Formulas for the calculation of individual or collective fibre debonding have been given[3].
Fig 10: Model of X-ray refraction at interfaces of bonded and debonded fibres of a composite, X-ray topography of model, investigation of single fibre debonding at different fibre volume ratios.
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Fig 11: X-ray refraction topographs of crack patterns in CFRP after ageing of 10,000 h at 180°C (epoxy) and 200°C (BMI).
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Another problem of CFRP characterization relates to impact damages. Ultrasound C-scans resolve delaminations created by impact very well, but the single fibre debonding area, which develops at lower loads, is only detectable by X-ray refraction topography. In Fig. 11 seven impact areas are imaged at 1 mm resolution. The reduction of details compared to Fig. 10 is compensated by 100 times faster measurements (10 mm²/s). (The three bright capitals are not impacted, simply pencil written [graphite scattering].)
Fig 12: X-ray refraction Computer-Tomography of CFRP laminate: micrograph, left; conventional absorption tomography, middle; interface tomography, right. |
The computer tomography experiment is carried out by 18 keV single beam scanning in a Kratky camera according to Fig. 4. Linear scans are performed for 360 angular positions, Fourier filtered for linear smearing on a PC and added up in an image file (filtered back projection). The reconstruction of detector signals I¢ shows a quite homogeneous density of the conventional (absorption) computer tomographic image (Fig. 12, centre). The final refraction image reveals the spatial interface/inner surface distribution free of absorption effects. The typical layer and crack structure of the micrograph can be recognised by a non-destructive technique.
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