Supplier: Manufacturers Supplies Co.
Description: in the petro-chemical industry (tang graphite included), foams and adhesive backed foams (up to 25mm in thickness), rubber materials, composites (kevlar, pre-preg, carbon fiber etc.), plastics and similar products.
Supplier: Dow Polyurethanes
Description: The AIRSTONE™ Mold Building System is a low viscosity epoxy tooling system designed for making glass or carbon fiber reinforced composite molds. The AIRSTONE Mold Building System consists of an epoxy resin and two amine hardeners with different pot lives. The two hardeners can be used
- Material Type / Grade: Thermoset
- Chemical / Polymer System Type: Epoxy
- Compound Type: Liquid
- Industry: Electric Power, Other
Supplier: Toray Industries (America), Inc.
Description: Toray Group is focusing on the development of the TORAYCA® Prepreg business. TORAYCA® Prepreg is an intermediate TORAYCA® product supplied in sheets consisting of resin-impregnated carbon fiber. The quality characteristics of TORAYCA® make it ideal for a wide range of uses
- Polymer Matrix Type: Specialty / Other
- Reinforcement / Filler Material: Carbon / Graphite
- Form / Shape: Film / Sheet
- Industry: Aerospace, Other
Supplier: Georgia-Pacific Corporation
Description: lay-up/RTM process. The phenolic resin systems have passed United States, British, and International Maritime Organization Standard Fire Tests. Honeycomb and Prepreg We offer phenolic resins for Nomex® and Kevlar® honeycomb, glass and carbon fiber prepregs for aerospace applications
- Material Type / Grade: Composite Material, Thermoset
- Chemical / Polymer System Type: Phenolics (Melamine, Furan)
- Filler Material: Aramid Fiber
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PEEK into the Future of Aircraft
material in the manufacture of advanced thermoplastic composite prepregs made of carbon, glass or aramid continuous fibers. The outstanding mechanical properties and processability of VICTREX PAEK-based composites make them an excellent substitute for metals and thermosets in a wide range of aerospace, offshore, medical and industrial applications. Find out more: · New Thermoplastic Composite Fabrics made with VICTREX PEEK Polymer Reduces Cycle Time. · VICTREX PEEK Polymer Used in Suprem Prepreg... (read more)
Browse Thermoplastics and Thermoplastic Resins Datasheets for Victrex plc.
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Optical Microscopy of Fiber-Reinforced Composites
J.F. Harper, N.A. Miller, and S.C. Yap, The Influence of Temperature and Pressure during the Curing of Prepreg Carbon Fiber Epoxy Resin, Polym.-Plast. Technol. Eng., Vol 32 (No. 4), 1993, p 269–275 .
Blade System Design Study. Part II, final project report (GEC).
Results for a third type of prepreg carbon fiber material were provided by MSU for comparative purposes, fabricated from Grafil 34-600 fibers (48k) and Newport NB307 resin.
Harper, N.A. Miller, and S.C. Yap, The Influence of Temperature and Pressure during the Curing of Prepreg Carbon Fiber Epoxy Resin, Polym.-Plast. Technol. Eng., Vol 32 (No. 4), 1993, p 269275 12.W.-B.
Low-cost, low-weight CNG cylinder development. Final report
OEMswere willingto considerAdvantex as an alternativeto carbon fiber(assumingall qualification testscould bepassed) and that the cost analysesfavoredAdvantex.Thus,it wasdecidedthat further discussionswith Thiokolregarding the prepreg carbon fiber approach would be suspended until the environmentalperformanceof Advantex couldbe gauged.
Prepreg carbon fiber tape, specifically unidirectional fibers set in PEEK, can be used as a compatible implant material; a metallic implant would introduce foreign material into the thermoplastic joint.
• The Hexcel prepreg carbon fiber demonstrated less consistency between samples but much greater consistency within each sample in comparison to the DragonPlate samples in terms of the overall .
Flying Insects and Robots
Using unidirectional and woven resin-impregnated ( prepreg ) carbon fiber , the wing structure is laid out on the tool.
Alpi Gamma Pioneer 400
Similar to earlier Alpi Pioneer designs, but with employment of prepreg carbon fibre ; cockpit doors in place of sliding canopy, permitting taller cockpit; and other ergonomic improvements.
Quasi-Static Four-Point Bend Testing of Macro-Fiber Composite Unimorphs
However, to cure the epoxy in the prepreg carbon fiber , the assembly is placed in an oven at 127 °C for four hours.