Products in Infrastructure, Roads & Paving: Prepreg

APCM DA 4090 is modified epoxy pre-impregnated system which can cure at 250°F (121°C) for one hour. DA 4090 | DA 4092 can be supplied on any commercially available glass, Kevlar, or graphite fabric. DA 4090 is a one sided pre-impregnated fabric yielding a single sided tack material. DA 4092 is the same system where both sides of the fabric are pre-impregnated yielding a double sided tack material. Both prepreg systems can be used for laminating and honeycomb sandwich construction.

PREPREG system BD (epoxy resin) are based on modified epoxy resins with high impact strength and excellent dynamic properties. They can be processed into high-strength structural components using all common methods. The hardening range is between 85 ° C and 140 ° C ; the max. heat resistance is 125 ° C . The delivery program with fabric, laid and unidirectional reinforced PREPREGS allows the load-based design of your components.

PREPREG system HH (polyimide resin) are based on a high temperature resistant polyimide resin . Its processing is hot pressing or PREPREG winding.

EF 12 is above 240 °C. High Tg EF12 resin system is used to produce structural prepregs. Optimized cure methods for these resin systems are Press and Autoclave molding.

ZOLTEK produces uni-directional (UD) prepreg tapes based on ZOLTEK carbon fiber. ZOLTEK prepreg is ideal for large-volume composite applications where high production throughput, excellent composite properties, and low material cost are important. A wide selection of epoxy resin formulations meet most processing and composite property requirements for tack, toughness, surface finish, cure time, cure temperature, and delivered composite strength and modulus. Custom formulations are also available. ZOLTEK prepreg properties, such as fiber areal weight (FAW), resin content, and width, are readily adjusted to exactly meet customer requirements. Packaging options include core size, customer specified knitting requirements, and custom labeling. ZOLTEK prepreg production is geared to large volumes and low cost. Special projects are welcomed.

PREPREG Low temperature, system BX (epoxy resin) are based on modified epoxy resins with an extremely wide curing range from 55 ° C to 185 ° C and meet the requirements of a low-pressure / low-temperature PREPREG. The BX system is suitable for the production of structural components as well as fiber composite tools with a heat resistance of up to 195 ° C. The processing can take place according to all common methods.

APCM DA 4080 is 200°F cure modified epoxy prepreg system which can be prepreged on fiberglass fabric, woven Kevlar, or other woven fabrics. In addition to their low temperature cure capabilities, DA 4080 prepregs have excellent flow to allow for vacuum bag cure conditions. DA 4080 is a one sided pre-impregnated system yielding a single sided tack material. DA 4082 is the same system except that both sides of the fabric are coated yielding a double sided tack material. Both prepregs can be used for laminating and honeycomb sandwich construction.

THINPREG™ TP 402 is a resin system suitable for manufacture of unidirectional prepreg material. ThinPreg™ 402 is a versatile system that is used most often with carbon fiber, but can also be impregnated into a wide range of reinforcing fibers including quartz, glass, aramid fiber etc. ThinPreg™ 402 features a high Tg (180°C) capability with additional toughening, and has been designed to be a good all-round product in terms of mechanical strength and processability.

APCM DA 4518 E-Glass is a modified epoxy system coated on heavy weight unidirectional E-Glass fibers. This product is designed to build excellent unidirectional strength using a minimum number of plies. DA 4518/E-Glass Uni also features extended room temperature out time and service temperatures to 300°F.

OM 13SF is a Sandable surfacing film and autoclave curable, sandable, Class A giving surfacing film.

THINPREG™ TP 415 is a rubber toughened version of TP402, design for sporting goods application, combining high elongation and great toughness. It is available in ultra-Thin Ply format, as low as 15gsm. This hot-melt epoxy prepreg is recommended to be cured at 135°C for optimal performance and a Tg until 145°C Onset (by E’ DMA). This matrix has a very good flow control. TP415 offers excellent mechanical properties on a wide variety of fibers, and fiber weights.

AX-4270 is Structural Epoxy Aramid Prepreg.

Ecotechnilin L-FLAXPREG T-UD-50-5m² is a unidirectional (UD) fibers - FLAXPREG T-UD 50.

OM10 is highly toughened structural Low Tg resin for press and autoclave curing for the needs of structural parts used in Automotive Industry. OM10 prepreg cures at both press and Autoclave with long out-life of 4 weeks at ambient temperature.

OM11 is a resin structural Low Tg prepreg that specifically customized for fatigue resistance part production in Industry. OM11 prepreg materials can be curable with Autoclave and Press.

APCM DA 4517 is an epoxy prepreg designed for a temperature range of -67°F (-55°C) to 350°F (177°C), with a cure of 180°F (82°C) for three hour. Shorter cures times are available at higher temperatures. The system is designed to be post cured if the higher temperature service range is required.

OM14 is a fast curing structural prepreg for press curing for the needs of structural parts used in Automotive Industry. Its short curing cycle and hot de-moldable nature are especially optimized for mass production at Automotive Industry with the addition of exceptionally long out life at room temperature. OM14 eliminates the need of Autoclave and Cold storage plus it is especially optimized for mass production. New resin system not only cures under 1-2 minutes at 150°C at press under isothermal curing conditions but also hot de-moldable and long out-life of one year at ambient temperature.

CM11 resin is Mid Tg and its prepregs are suitable for hot painting, hot gluing and cataphoresis processes. New resin system not only cures under 3 minutes at 150°C at press under isothermal curing conditions but also hot de-moldable and long out-life of two weeks at ambient temperature. These extreme conditions does not affect the visual Performance of prepreg system with CM11, capable of Class A Surface. Drapability is suitable for press molds and low to medium tack optimized for press curing.

THINPREG™ TP 150SC is designed for the automotive market due to the snap-cure capability for low TAKT times while achieving good mechanical properties, and the additional benefit of not requiring frozen or refrigerated storage.

PREPREG system SG (silicone resin) are based on a silicone resin. Its Processing is hot pressing or prepreg winding.

Evopreg® PFC502 prepregs are a range of fire-retardant, pre-impregnated composite materialsbased on a PFA (Polyfurfuryl Alcohol) bioresin. PFA is a thermosetting bioresin derived from crop waste and is similar to phenolic resin but withlower toxicity and VOC emissions. In addition to its environmental credentials, PFA hasoutstanding fire retardant properties, plus excellent temperature and chemical resistance. The prepregs can be supplied with a range of reinforcement fibers and fabric constructions,including woven and unidirectional E-glass fiber and carbon fiber. They can be consolidated byvacuum bagging, autoclave or press molding and are designed for applications includingaircraft interiors, rail interiors, marine, offshore and construction.

OM 12 is a glass fiber or carbon fiber reinforced composites offer advantages of high corrosion resistance and high strength-to-weight ratio than traditional wood or steel materials. Kordsa may provide different reinforcement materials including glass or carbon UD, 2D and multiaxial impregnated with epoxy. For the huge size part production, generally vacuum bag only prepregs (OM12) are recommended

PREPREG system BE (epoxy resin) are based on a temperature- resistant modified epoxy resin . Its processing is hot pressing or PREPREG winding. Its tack has no to little stickiness.

Ecotechnilin L-FLAXPREG-T-UD-110-36m² is a unidirectional (UD) fibers - FLAXPREG T-UD 70.

APCM DA 4082 is 200°F cure modified epoxy prepreg system which can be prepreged on fiberglass fabric, woven Kevlar, or other woven fabrics. In addition to their low temperature cure capabilities, DA 4080 prepregs have excellent flow to allow for vacuum bag cure conditions. DA 4080 is a one sided pre-impregnated system yielding a single sided tack material. DA 4082 is the same system except that both sides of the fabric are coated yielding a double sided tack material. Both prepregs can be used for laminating and honeycomb sandwich construction.

EF 11 is also optimized for press molding and used in extreme applications. The highest glass transition temperature reached with epoxy products.

APCM DA 4518 is an epoxy prepreg designed for a temperature range of -67°F (-55°C) to 350°F (177°C), with a cure of 250°F (121°C) for one hour and or a cure of 350º F (177ºC) for 1 hour. This material needs to be post cure or cured to 350ºF to get the 350º properties.

AX-5270 is a Structural Epoxy Carbon Prepreg.

THINPREG™ TP 513 is a prepreg resin matrix used for the manufacture of light weight prepreg molding materials. ThinPreg™ 513 is a versatile system that is used most often with carbon fiber, but can also be impregnated into a wide range of reinforcing fibers including quartz, glass, aramid etc.

EF 10 is highly toughened Mid Tg prepreg can be cured with autoclave and used in extreme applications in automotive industry and aviation industry.

OM13 is a structural resin system. It is translucent when cured.

Ecotechnilin L-FLAXPREG-T-UD-110-5m² is a unidirectional (UD) fibers - FLAXPREG T-UD 110.

CM 15 is a Visual composites, Semi Structural and Fast Isothermally Press Curable, Class A Surface quality for painting, Hot Demoldable, Improved UV and environmental resistance, Improved fiber imprinting resistance

AX-5201 is a Toughened Epoxy Carbon Laminating Prepreg.

Ecotechnilin L-FLAXPREG-T-UD-50-60m² is a unidirectional (UD) fibers - FLAXPREG T-UD 50.

THINPREG™ TP 135 is a breakthrough product combining high strength and high toughness in a thin ply format. The PES-toughened epoxy system shows compression after impact properties typical of 3rd generation aerospace matrices. Thin ply materials achieve higher usable properties from the fiber through spreading load more consistently though the laminate and delaying first ply failure. Negligible ply drop-off effects and greater degrees of freedom in design are now combined with a PES-toughened system for high resolution, highly optimized, super-strong composite structures.