| High-Temperature Resins for Composite Materials |
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| Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio | |
| Nov 30 2007 | |
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Advertisement: The resins in question have the molecular structures shown in the figure. In experiments performed thus far, samples of resins and polymers were prepared as described below. •Toughened Cyanate Esters These resins were derived from the di(cyanate ester) of bisphenol A (BADCy). Amorphous polycarbonate (APC) were used as a polymeric toughening agent. Samples of toughened cyanate esters were cast from mixtures that were formed by dissolving the toughening agent in methylene chloride and adding it to molten BADCy at temperatures between 80 and 100 °C. In some samples, the proportions of the ingredients by weight were 1 part APC and 10 parts BADCy; in other samples, the weight proportions were 1 part APC and 5 parts BADCy. Samples of neat BADCy were also cast. For each sample, the casting solution was poured into a mold, then baked at a temperature of 190°C for two hours), followed by 225°C for one hour, followed by 250°C for one hour, followed by 300°C for one hour. •Silane-Based Cyanate Esters These resins were derived from the di(cyanate ester) of dimethyldi(p-phenol) silane [abbreviated “SiMCy”], which is a silicon-containing analog of BADCy. This resin melts at 59°C. Samples of this resin, without and with APC as a toughening agent, were cast in molds in the same manner as that of the toughened BADCy resins. •Poly-p-Phenylenes Phenyl ethynyl-terminated polyphenylene oligomers denoted generally as “P3- 2300-PE” were synthesized and purified in powder form. Castings of P3-2300-PE were made by melting the powder in open molds at 180°C. The castings were subsequently cured at temperatures increasing gradually from 350 to 450°C. Samples of these polymers were subjected to a variety of thermal, thermomechanical, and water-absorption tests. The following conclusions were drawn from the test results:
This work was done by Gregory R. Yandek and Darrell Marchant of the Air Force Research Laboratory, Andrew J. Guenthner and Michael E. Wright of the Naval Air Warfare Center, and Thomas K. Tsotsis of the Boeing Co. AFRL-0049 This Brief includes a Technical Support Package (TSP).High-Temperature Resins for Composite Materials (reference AFRL-0049) is currently available for download from the TSP library. Login first to download.
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