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prepreg plies
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Image
Published: 01 December 2004
Fig. 7 Large void at the termination of two prepreg plies. Slightly uncrossed polarized light, 10× objective
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Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0009077
EISBN: 978-1-62708-177-1
.... This article describes the optical microscopy and bright-field illumination techniques involved in analyzing ply terminations, prepreg plies, splices, and fiber orientation to provide the insight necessary for optimizing composite structure and performance. bright-field illumination composite materials...
Abstract
Analyzing the structure of composite materials is essential for understanding how the part will perform in service. Assessing fiber volume variations, void content, ply orientation variability, and foreign object inclusions helps in preventing degradation of composite performance. This article describes the optical microscopy and bright-field illumination techniques involved in analyzing ply terminations, prepreg plies, splices, and fiber orientation to provide the insight necessary for optimizing composite structure and performance.
Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0009083
EISBN: 978-1-62708-177-1
..., as described in Fig. 1 . This figure documents the movement of the core as viewed from the tool side and shows the smooth surface, with surfacing film, against the tool. The deformation of the prepreg plies is evident from the core movement that occurred during the cure cycle. The prepreg plies are wavy...
Abstract
Honeycomb-cored sandwich panels increase part stiffness at a lower weight than monolithic composite materials. This article illustrates an area of a honeycomb-cored sandwich structure composite cross section that is viewed using transmitted polarized light. This area shows the differences in the constituents and resin intermingling. The article discusses the factors that govern the honeycomb core movement and honeycomb core crush, with illustrations. Some common tests performed on honeycomb composites to characterize the skin-to-core bond strength are the climbing drum peel and flatwise tensile tests. The article concludes with a description on the reasons for core failure, which are analyzed after these tests.
Image
Published: 01 December 2004
Fig. 1 Montage of micrographs taken of a cross section of a composite made from unidirectional prepreg that shows the termination of two prepreg plies near the center of the part. Bright-field illumination, 5× objective
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Image
Published: 01 December 2004
Fig. 2 Laminate made with unidirectional carbon fiber prepreg and woven carbon fabric prepreg plies. Voids are shown in the woven fabric area at the bottom of the composite part that was against the tool surface during cure. Bright-field illumination, 65 mm macrophotograph
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Image
Published: 01 December 2004
Fig. 3 Ultrathin section of areas of the honeycomb sandwich composite structure where resin was found to span the separated prepreg plies after core movement. (a) Transmitted light, phase contrast, 40× objective. (b and c) Transmitted light, phase contrast, 20× objective
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Image
Published: 01 December 2004
Fig. 2 Ultrathin section of an area of a honeycomb sandwich composite structure showing the effects of core movement during manufacturing and the resulting deformation and separation of the prepreg plies. (a) Transmitted crossed polarized light, 20× objective. (b and c) Transmitted polarized
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Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0009078
EISBN: 978-1-62708-177-1
... or liquid resins, depending on the processing method. High-viscosity, controlled-flow resins and resins having high thixotropy can almost completely resist degassing. During the lay-up of a composite part using prepreg materials, air may be entrapped between the adjacent plies, resulting in voids...
Abstract
Voids in fiber-reinforced composite materials are areas that are absent of the composite components: matrix (resin) and fibers. Voids have many causes but generally can be categorized as voids due to volatiles or as voids that result from entrapped air. This article describes the analysis of various types of voids. It reviews techniques for analysis of voids at ply-drops, voids due to high fiber packing, and voids that occur in honeycomb core composites. The final section of the article discusses void documentation through the use of nondestructive inspection techniques and density/specific gravity measurement methods.
Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0009074
EISBN: 978-1-62708-177-1
... of the sample uses the same procedure as mentioned previously, where the unstaged (and will be staged as a complete mount) or staged prepreg plies are cut with sharp scissors and bonded together. The width of the overall sample, made from multiple plies of prepreg, that is in contact with the platen surface...
Abstract
This article focuses on the sample preparation methods for titanium honeycomb composites, boron fiber composites, and titanium/polymeric composite hybrids. These include mounting, sectioning, grinding, and polishing. The article also provides information on the sample preparation of unstaged and staged prepreg materials for optical analysis.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003419
EISBN: 978-1-62708-195-5
... are the starting point in most cases. With prepregs, composite manufacturing may be batchwise or more or less continuous. In batch techniques, the route from prepreg to final component may be divided into three basic steps: layup, consolidation, and molding. In the first step the number of prepreg plies required...
Abstract
This article describes the characteristics of thermoplastic composites and its material forms. It presents the steps and considerations in manufacturing the thermoplastic composites. The article describes the various techniques of manufacturing, such as consolidation, autoclave molding, diaphragm forming, compression molding, roll forming, bladder molding, liquid molding, filament winding, and pultrusion.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003434
EISBN: 978-1-62708-195-5
... heating the adhesive using heat guns and tacking irons certified for use on adhesives. The heat guns and tacking irons are kept in motion in small circles over the area to be tacked, at least 76 mm (3 in.) away from the adhesive surface. Prepreg plies may be removed for repositioning by using portable...
Abstract
In-process inspection during composite material lay-up is essential if the structural, dimensional, and environmental performance designed into a part is to be consistently achieved. This article discusses the requirements to be met by the facilities and equipment to produce high-quality composites. It reviews the procedures that are allowed and prohibited in controlled-contamination areas of lay-up. The article emphasizes significant areas, such as material control and lay-up process, in which quality-control personnel can be effective in preventing production problems. It concludes with a discussion on automated tape laying and fiber placement, as well as the numerically aided lay-up process.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003408
EISBN: 978-1-62708-195-5
... Abstract This article reviews the history of prepreg and ply cutting technologies and outlines the options available for creating the necessary data and for nesting, cutting, and kitting the plies. It discusses the ways in which these steps influence the workflow for various applications...
Abstract
This article reviews the history of prepreg and ply cutting technologies and outlines the options available for creating the necessary data and for nesting, cutting, and kitting the plies. It discusses the ways in which these steps influence the workflow for various applications. The characteristics of prepreg and ply cutting methods are presented in a table.
Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0009071
EISBN: 978-1-62708-177-1
... impregnation of the matrix resin into the continuous unidirectional or woven fiber fabric materials ( Ref 5 , 6 ). These pre-engineered laminating materials have a discrete resin/fiber ratio that requires further lay-up of the continuous fiber plies to achieve the final composite. The prepreg lay-up...
Abstract
This article illustrates the polymer matrices used for composite materials. It describes the use of prepeg materials in manufacturing high-performance composites. The article discusses the various infusion processes for the development of fiber-reinforced composites, namely, resin transfer molding, vacuum-assisted resin transfer molding, and resin film infusion. It explains the composite- and matrix-toughening methods for fiber-reinforced composites, such as dispersed-phase toughening and interlayer toughening. The article concludes with information on optical microscopy, which provides an insight into the micro- and macrostructure of fiber-reinforced composites.
Image
in Viewing Composite Specimens Using Reflected Light Microscopy[1]
> Metallography and Microstructures
Published: 01 December 2004
prepreg material combinations (glass fabric prepreg and carbon fiber prepreg), and the number of plies. Bright-field illumination, 5× objective
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Book Chapter
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003360
EISBN: 978-1-62708-195-5
.... The part fabricator requires a prepreg with tack, drape, and a certain tack life and out time. Tack is the tendency of two plies or layers to adhere sufficiently to allow laying-up of complex parts yet allow a clean strip-back if layers are applied incorrectly. Too low an adhesion level will allow layers...
Abstract
This article describes the types of fabrics and preforms used in the manufacture of advanced composites and related selection, design, manufacturing, and performance considerations. The types of fabrics and preforms include unidirectional and two-directional fabrics; multidirectionally reinforced fabrics; hybrid fabrics; woven fabric prepregs; unidirectional and multidirectional tape prepregs; and the prepreg tow. The article discusses three major categories of tape manufacturing processes, namely, the hand lay-up, machine-cut patterns that are laid up by hand, and the automatic machine lay-up. It provides a description of the two classes of prepregs. These include those that are suitable for high-performance applications and suitable for lower-performance molding compounds.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003418
EISBN: 978-1-62708-195-5
... cylindrical tapered tubes TUBE ROLLING is the most widely used method of producing composite tubular parts that require high strength-to-weight properties as well as high production capabilities. The tube rolling process utilizes prepreg materials having accurate resin content, which are produced on very...
Abstract
This article describes processes and equipment that are used to produce composite tubular parts. The processes include sheeting, pattern cutting, tube rolling, shrink tape debulking, and finishing. The article provides a discussion on materials that are most suitable for tube rolling: preimpregnated materials and unidirectional tapes. The article also discusses wrapping techniques of cylindrical and tapered tubes, such as convolute and spiral wrapping.
Book Chapter
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003036
EISBN: 978-1-62708-200-6
... are large fiber bundles that are woven into a very thick fabric, which is used to build up part thickness with a minimum number of plies. These materials are available in large rolls of various widths. The full and partial plies in the part are cut from the prepreg rolls using large scissors, utility knives...
Abstract
Wet lay-up using hand or spray techniques is one of the simplest methods of combining a fiber reinforcement with a solidifying resin to form a composite structure. This article describes several wet lay-up processes - including contact molding, spray molding, vacuum bag molding, and autoclave molding - suited for making parts on open-faced molds using polyester and vinyl ester resins. The article also provides information on mechanically assisted lay-up which can be automated to alleviate some of the manual work.
Image
in Special Sample Preparation and Polishing for Fiber-Reinforced Composites[1]
> Metallography and Microstructures
Published: 01 December 2004
Fig. 12 Polished stack of prepreg that was bonded with “5 min epoxy” and then staged in an oven at 60 °C (140 °F) for 2 weeks. This micrograph is of 4 1 2 plies of polished prepreg taken from the 20-ply mount. Bright-field illumination, 10× 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.a0003409
EISBN: 978-1-62708-195-5
... to minimize cutting waste from the prepreg roll. The software is used to match the total kit of plies to the material-roll width and to define the cutter paths. Users of large quantities of prepreg use an automated device that cuts the material and, in some models, stamps a bar code or number...
Abstract
The prepreg hand lay-up process is a versatile, reliable, cost-effective, and high quality process for fabricating large or small components. This article discusses the technique characteristics and applications of the process. It describes the stages involved in the process of lay-up, namely, lay-up definition, ply-kit cutting, layup, debulking, and preparation for curing. The article concludes with a discussion on the component properties and design guidelines of the prepreg hand lay-up process.
Book Chapter
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003041
EISBN: 978-1-62708-200-6
..., and the resin content of the prepreg material used in the layup. In advanced composites, essentially all excess resin is bled from the surface of the laminate, with edge bleeding being minimized by properly damming the layup edges. Personnel should establish tables giving plies of bleeder per ply of layup...
Abstract
Autoclave molding is a process used to impart a controlled heat and pressure cycle cure to a layup. This article describes the materials used for preparing a layup, including peel ply, separator, bleeder, barrier, breather, dam, and vacuum bag. It describes the major elements and functions of an autoclave system, including pressure vessel, gas stream heating and circulation sources, gas stream pressurizing systems, vacuum systems, control systems, and loading systems. The article includes information about modified autoclaves for specialized applications and safety practices in autoclave molding. It also describes the tooling configuration and type of tooling which includes aluminum and steel tooling, electroformed nickel tooling, graphite-epoxy tooling, and elastomeric tooling.
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