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epi-fluorescence
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Published: 01 December 2004
Fig. 12 Intraply microcracks in a carbon fiber composite material. Epi-fluorescence, 390–440 nm excitation, 25× objective
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Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003464
EISBN: 978-1-62708-195-5
...-fluorescence. The article also provides information on transmitted light microscopy. composite materials epi-bright-field illumination epi-dark-field illumination epi-fluorescence epi-polarized light failure analysis illumination methods mounting polishing quality control reflected light...
Abstract
Microscopy is a valuable tool in materials investigations related to problem solving, failure analysis, advanced materials development, and quality control. This article describes the sample preparation techniques of composite materials. These techniques include mounting, rough grinding, and polishing. The preparation techniques of ultrathin sections are also summarized. The article explains the illumination methods used by reflected light microscopy to view a specimen. These consist of epi-bright-field illumination, epi-dark-field illumination, epi-polarized light, and epi-fluorescence. The article also provides information on transmitted light microscopy.
Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0009079
EISBN: 978-1-62708-177-1
... Abstract This article describes the microcrack analysis of composite materials using bright-field illumination, polarized light, dyes, dark-field illumination, and epi-fluorescence. bright-field illumination composite materials dark-field illumination dyes epi-fluorescence microcrack...
Image
Published: 01 December 2004
Fig. 3 Impact damage of a carbon fiber composite material that has a brittle matrix. (a) Montage of the impact area. Epi-fluorescence, 390–440 nm excitation, 5× objective. (b) Fiber fracture area in the composite. Epi-fluorescence, 390–440 nm excitation, 25× objective. (c) Fracture shown
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Image
Published: 01 December 2004
Fig. 11 Intraply microcrack in a carbon fiber composite that is difficult to observe using bright-field illumination but easily identified after the application of a fluorescing dye (Magnaflux Zylgo, Magnaflux Corp.) and epi-fluorescence. (a) Bright-field illumination, 10× objective
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Image
Published: 01 December 2004
Fig. 4 Impact damage of a carbon fiber composite material that has a toughened matrix. (a) Montage of the impact area. Epi-fluorescence, 390–440 nm excitation, 5× objective. (b) Multiple intraply fractures. Epi-fluorescence, 390–440 nm excitation, 25× objective. (c) Adhesive failure
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Image
Published: 01 December 2004
Fig. 5 Impact damage of a carbon fiber composite material that has a toughened matrix. (a) Montage of the impact area. Epi-fluorescence, 390–440 nm excitation, 5× objective. (b) Wide crack formation in the 45° plies and mainly cohesive failure in the interlayer. Epi-fluorescence, 390–440 nm
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Image
Published: 01 December 2004
Fig. 14 Comparison of the same area in a carbon fiber composite using epi-bright-field illumination and epi-fluorescence. The microcracked area of the composite material was sectioned and polished at an oblique angle through the thickness to emphasize the interlayer region. (a) Bright-field
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Image
in Viewing Composite Specimens Using Reflected Light Microscopy[1]
> Metallography and Microstructures
Published: 01 December 2004
Fig. 10 Microcracks in a composite material that are difficult to observe using epi-bright-field illumination. (a) Bright-field illumination, 25× objective. (b) Same location viewed after applying a fluorescent penetrant dye (Magnaflux Zyglo) to the surface and back-polishing. Epi-fluorescence
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Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0009081
EISBN: 978-1-62708-177-1
... the origin and extent of the damage in the composite. To better identify the location of the damage in the intra- and interlayer areas, greater contrast may be required. In this case, epi-fluorescence can prove to be very valuable. Further information regarding the effect on the matrix microstructure...
Abstract
This article describes methods for analyzing impact-damaged composites in the aircraft industry. These include C-scan and x-radiography methods and optical microscopy. The article reviews brittle-matrix composite and tough-matrix composite failures. It explains the different types of composite failure mechanisms such as thermoplastic-matrix composite failure mechanisms, untoughened thermoset-matrix composite failure mechanisms, toughened thermoset-matrix composite failure mechanisms, dispersed-phase and rubber-toughened thermoset-matrix composite failure mechanisms, and particle interlayer-toughened composite failure mechanisms.
Image
Published: 01 December 2004
of the polished specimen, wiped off after 2 min, and cleaned with water. The solvent/dye preferentially absorbed into the particles and phases and not the thermoset matrix. Epi-fluorescence, 390–440 nm excitation, 25× objective
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Image
Published: 01 December 2004
present is a very small dispersed phase that fluoresces yellow. Epi-fluorescence, 390–440 nm excitation, 25× objective
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Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0009085
EISBN: 978-1-62708-177-1
..., including polarized light, bright- and dark-field illumination, and epi-fluorescence. The damage characteristics depend on many factors, including the type of lightning strike protection material on the surface (expanded foil or interwoven wire), the polymer matrix, the fiber type and volume, the lay-up...
Image
in Sample Preparation and Mounting for Fiber-Reinforced Composites[1]
> Metallography and Microstructures
Published: 01 December 2004
Fig. 5 Composite material that was cut using a waterjet. Very little damage is observed at the cut edge of the specimen. A fluorescing dye was applied to the cut edge to determine if cracks were present. Epi-fluorescence, 390–440 nm excitation, 25× objective
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Image
in Viewing Composite Specimens Using Reflected Light Microscopy[1]
> Metallography and Microstructures
Published: 01 December 2004
to enhance the contrast of the microcracks. Epi-fluorescence, 390–440 nm excitation, 10× objective
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Image
in Viewing Composite Specimens Using Reflected Light Microscopy[1]
> Metallography and Microstructures
Published: 01 December 2004
× objective. (b) Dark-field illumination, 25× objective. (c) Polarized light, 25× objective. (d) Slightly uncrossed polarized light, 25× objective. (e) Epi-fluorescence, 390–440 nm, 25× objective. (f) Transmitted light, Hoffman modulation contrast, 20× objective
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Image
Published: 01 December 2004
Fig. 13 Large-scale microcracking in a carbon fiber composite material. Epi-fluorescence, 390–440 nm excitation, 10× objective
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Image
in Sample Preparation and Mounting for Fiber-Reinforced Composites[1]
> Metallography and Microstructures
Published: 01 December 2004
, and then subjected to the last stage of polishing to remove additional dye from the surface. Epi-fluorescence, 390–440 nm excitation, 50× objective
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Image
Published: 01 December 2004
Fig. 9 Thermoplastic stitch in carbon fiber composite material. Note the microcracks in the of the stitch. Epi-fluorescence, 390–440 nm excitation, 25× objective
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Image
in Analysis of the Effects of Lightning Strikes on Polymeric Composites[1]
> Metallography and Microstructures
Published: 01 December 2004
Fig. 5 Micrograph taken under the strike zone showing damage induced by the lightning strike. Epi-fluorescence, 390–440 nm excitation, 25× objective
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