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Woven carbon

Figure 12.4 Compaction behavior of a woven carbon fiber fabric. The solid curve shows the behavior at room temperature the other two lines show the behavior at 100 C and 110°C. The fabric was factory treated with an epoxy preform binder... Figure 12.4 Compaction behavior of a woven carbon fiber fabric. The solid curve shows the behavior at room temperature the other two lines show the behavior at 100 C and 110°C. The fabric was factory treated with an epoxy preform binder...
Engineering thermoplastics have also been used in preimpregnated constructions. The thermoplastic is thoroughly dispersed as a continuous phase in glass, other resins, carbon fibers (qv), or other reinforcement. Articles can be produced from these constructions using thermoforming techniques. For example, the aerospace industry uses polyetheretherketone (PEEK) in woven carbon-fiber tapes (26). Experimental uses of other composite constructions have been reported (27) (see also COMPOSITE MATERIALS, POLYMER-MATRIX). [Pg.263]

The weakness of MRI technique is mainly in the requirement that the materials have to be nonmagnetic. For this reason, the fuel cell components must be carefully chosen, of which many are not the same size or composition as in industrial cells. Additionally, the water content in the CL and GDL, either made from nonwoven carbon paper or from woven carbon cloth, will be difficult to visualize with MRI.54... [Pg.140]

Carbon-fiber based porous materials, namely non-woven carbon paper and woven carbon cloth, shown in Fig. 5, have received wide acceptance as materials of choice for the PEFC GDL owing to high porosity ( 70% or higher) and good electrical/thermal conductivity. Mathias et al.32 provided a comprehensive overview of the GDL structure and functions. In this work, the reconstruction of non-woven carbon paper GDL is presented. [Pg.262]

The stochastic simulation technique creates 3-D realization of the non-woven carbon paper GDL based on structural inputs,... [Pg.262]

Figure 6 shows the reconstructed microstructure of a typical non-woven, carbon paper GDL with porosity around 72% and thickness of 180 ixm along with the structural parameters in terms of... [Pg.263]

Figure 6. Reconstructed non-woven carbon paper GDL microstructure along with the evaluated structural properties. Figure 6. Reconstructed non-woven carbon paper GDL microstructure along with the evaluated structural properties.
FIGURE 5 Fiber structures left, knitted silicon fibers catalyst (6) right, woven carbon fibers (7). [Pg.255]

Materials commonly used for the gas diffusion layers are carbon paper or woven carbon mats (examples of which are shown in Fig. 3.41). They combine the cormectivity allowing electron transport with a pore structure suitable for hydrogen or oxygen gas access to the catalyst layer. In cell manufacture, the catalysts may be deposited either on the gas diffusion layer or on the membrane. [Pg.184]

Defibrillation lead employing electrodes fabricated from woven carbon fibers 5..3,36,2.54 1994 Brennen. Williams. Gabler... [Pg.58]

Carbon felt, carbon wool and woven carbon, which due to their isotropic structure only exhibit low mechanical strengths and low elasticity moduli, are manufactured by the pyrolysis of organic textiles. Depending on the form of the starting material utilized e.g. as woven textiles or felt, woven carbon or carbon felt is produced after carbonization. [Pg.381]

Applications of carbon felts, carbon wool and woven carbon ... [Pg.381]

The materials for the experiments were an aqueous dispersion PTFE (FLUON XAD -911 average diameter of particles 0.25 pm, concentration 60 wt%, Mn 1.4 x 106, viscosity at 25 °C 20 mPa-s, Asahi-Glass Fluoropolymers Co. Ltd.), and fluorinated-compound such as fluorinated-pitch (Rinoves P N-7-M average diameter of particles 1.2 pm, atom ratio of F/C 1.6, Mn 2.0 x 103, Osaka Gas Chemicals Co. Ltd.) [12, 13]. And also the plane-woven carbon fabric (TORAYCA T-300, C06142, TORAY Industries, Inc.) was used for the mechanical tests such as the tensile and the flexural tests. [Pg.206]

Table I shows the mechanical properties of the carbon fiber-reinforced PTFE (PTFE composite non-crosslinked) and the carbon fiber-reinforced PTFE with fluorinated-pitch (PTFE / FP composite thermo-chemical crosslinked). For the tensile test with a direction of 45 ° for plane-woven carbon fabric, the tensile strength of the PTFE / FP composite was about 2.3 times higher than that of the non-crosslinked PTFE composite. Moreover, the Young s modulus of the crosslinked composite was about 2.6 times higher than that of the PTFE composite. The tensile strength and Young s modulus are results of 0 ° or 90 ° direction for the fabric reflected the carbon fiber strength and the modulus. Table I shows the mechanical properties of the carbon fiber-reinforced PTFE (PTFE composite non-crosslinked) and the carbon fiber-reinforced PTFE with fluorinated-pitch (PTFE / FP composite thermo-chemical crosslinked). For the tensile test with a direction of 45 ° for plane-woven carbon fabric, the tensile strength of the PTFE / FP composite was about 2.3 times higher than that of the non-crosslinked PTFE composite. Moreover, the Young s modulus of the crosslinked composite was about 2.6 times higher than that of the PTFE composite. The tensile strength and Young s modulus are results of 0 ° or 90 ° direction for the fabric reflected the carbon fiber strength and the modulus.
Figure 5 The tensile strength and the Young s modulus with the direction of 45 ° tensile properties of one ply sheet composites consist ofplain-woven carbon fiber-reinforced RX-PTFE and the carbon-fiber-reinforced SX-PTFE (fluorinated-pitch 1.8 wt% additive) as a function of EB dose. Figure 5 The tensile strength and the Young s modulus with the direction of 45 ° tensile properties of one ply sheet composites consist ofplain-woven carbon fiber-reinforced RX-PTFE and the carbon-fiber-reinforced SX-PTFE (fluorinated-pitch 1.8 wt% additive) as a function of EB dose.
E. Tani, K. Shobu, and K. Kishi, Two-dimensional-woven-carbon-fiber-reinforced Silicon Carbide/Carbon Matrix Composites Produced by Reaction Bonding, J. Am. Ceram. Soc., 82 [5] 1355-57(1999). [Pg.448]

Karahan M, Lomov SV, Bogdanovich AE, Mungalov D, Verpoest I. Internal geometry evaluation of non-crimp 3D orthogonal woven carbon fabric composite. Composites Part A 2010 41 1301-11. [Pg.48]

Yazid YM, Cantwell WJ, Langdon GS, Nurick GN. The blast resistance of a woven carbon fiber-reinforced epoxy composite. J Compos Mater 2011 45 789-801. http // dx.doi.org/10.1177/0021998310376103. [Pg.223]

Li WW, Crosky A. Effect of cure pressure on the behavior of woven carbon/epoxy composite laminates. Int J Mater Prod Technol 2003 19 275-83. http //dx.doi.org/10.1504/ DMPT.2003.002511. [Pg.225]

Archer E, Broderick J, Buchanan S, Mcllhagger AT. Internal strain measurement and impact response of three-dimensional angle interlock woven carbon fibre composites. J Reinf Plast Compos 2013 32(12) 912-24. [Pg.411]

Reinforcement/ Typical 300g woven Carbon 200g... [Pg.943]

Bishop SM, Curtis PT. An assessment of the potential of woven carbon fibre reinforced plastics for high performance applications. Composites 1984 15 259-65. [Pg.23]

Fishpool DT, Rezai A, Baker D, Ogin SL, Smith PA. Interlaminar toughness characterisation of 3D woven carbon fibre composites. Plast Rubber Compos 2013 42 108-14. [Pg.25]


See other pages where Woven carbon is mentioned: [Pg.5]    [Pg.9]    [Pg.9]    [Pg.108]    [Pg.91]    [Pg.264]    [Pg.280]    [Pg.259]    [Pg.5]    [Pg.103]    [Pg.381]    [Pg.4]    [Pg.207]    [Pg.213]    [Pg.5]    [Pg.474]    [Pg.776]    [Pg.217]    [Pg.279]    [Pg.263]    [Pg.590]    [Pg.30]    [Pg.41]    [Pg.9]    [Pg.9]   
See also in sourсe #XX -- [ Pg.381 ]




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