Browsing by Subject "carbon fiber composites"
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Item High Temperature Materials for Aerospace Applications(2011-08-08) Adamczak, Andrea DianeFurther crosslinking of the fluorinated polyimide was examined to separate the cure reactions from degradation and to determine the optimum post curing conditions. Glass transition/melting temperatures were ascertained using DSC, while weight loss during curing and Td were determined using TGA. Furthermore, the mechanical properties were measured using an Instron to relate to the thermal properties to find the optimum curing conditions. The polyimide resin exhibited the best post-curing conditions for further crosslinking for 8 hours at 410 degress C based on Tg, thermal stability, and mechanical properties. Blister temperatures, resulting from rapid heating, were obtained by monitoring changes in transverse thickness expansion using two different techniques. Both techniques employed showed similar blister temperatures in relation to the amount of absorbed moisture, regardless of sample size. The polyimide resin exhibited blister temperatures ranging from 225 - 362 degrees C, with 1.7 - 3.0 wt% absorbed moisture, and the polyimide composite had blister temperatures from 246 - 294 degrees C with 0.5 - 1.5 wt% moisture. Weight loss of the fluorinated polyimide and its corresponding polyimide carbon fiber composite under elevated temperature was examined. Weight loss as a function of exposure temperature and time was measured using TGA and by pre- and post-weighing of specimens treated in an oven. Both techniques showed similar weight loss trends as a function of time and temperature, but TGA showed much greater weight loss due to greater surface area to volume (i.e., small sample size). The neat polyimide resin and carbon fiber composite exhibited negligible weight loss at temperatures below 430 degrees C for exposure times up to 20 minutes. Transition-metal carbides were initially synthesized by carbothermal reduction of transition-metal halides and polymer precursor mixtures, at temperatures that range from 900 to 1500 degrees C in an argon atmosphere. TaC was synthesized from TaBr5, as a model carbide for this process. Significant (> 40 vol%) amounts of TaC were formed at reaction temperatures as low as 900 degrees C for one hour, with greater times and temperatures leading to > 90 vol% yield. Universality of method was also proven by using other various transition-metal halide salts (NbBr5, WCl4, and WCl6) with the polyimide.Item Processing and Characterization of Carbon Nanotubes Reinforced Epoxy Resin Based Multi-scale Multi-functional Composites(2011-02-22) Thakre, Piyush R.This research is focused on investigating the effect of carbon nanotubes on macroscale composite laminate properties, such as, interlaminar shear strength, interlaminar fracture toughness and electrical conductivity along with studying the micro and nano-scale interactions of carbon nanotubes with epoxy matrix via thermomechanical and electrical characterization of nanocomposites. First an introduction to the typical advanced composite laminates and multifunctional nanocomposites is provided followed by a literature review and a summary of recent status on the processing and the characterization work on nanocomposites and composite laminates. Experimental approach is presented for the development of processing techniques and appropriate characterization methods for carbon nanotubes reinforced epoxy resin based multi-functional nanocomposites and carbon fiber reinforced polymer composite laminates modified with carbon nanotubes. The proposed work section is divided into three sub-sections to describe the processing and the characterization of carbon nanotube reinforced epoxy matrix nanocomposites, woven-carbon fabric epoxy matrix composite laminates modified with selective placement of nanotubes and unidirectional carbon fiber epoxy matrix composite laminates modified with carbon nanotubes. Efforts are focused on comparing the effects of functionalized and unfunctionalized carbon nanotubes on the advanced composite laminates. Covalently functionalized carbon nanotubes are used for improved dispersion and fiber-matrix bonding characteristics and compared with unfunctionalized or pristine carbon nanotubes. The processing of woven carbon fabric reinforced epoxy matrix composite laminates is performed using a vacuum assisted resin transfer molding process with selective placement of carbon nanotubes using a spraying method. The uni-directional carbon fiber epoxy matrix pre-preg composites are processed using a hot press technique along with the spraying method for placement of nanotubes. These macroscale laminates are tested using short beam shear and double cantilever beam experiments for investigating the effect of nanotubes on the interlaminar shear stress and the interlaminar fracture toughness. Fractography is performed using optical microscopy and scanning electron microscopy to investigate the structure-property relationship. The micro and nano-scale interactions of carbon nanotubes and epoxy matrix are studied through the processing of unfunctionalized and functionalized single wall carbon nanotube reinforced epoxy matrix nanocomposites. The multifunctional nature of such nanocomposites is investigated through thermo-mechanical and electrical characterizations.