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Composite Materials Research Progress

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An Experimental and Analytical Study of Unidirectional Carbon Fiber… 131<br />

Monte Carlo simulation on the tensile failure process of unidirectional carbon prepreg<br />

laminates.<br />

<strong>Materials</strong><br />

T700SC 12000-50C carbon fiber used in this research is manufactured by Toray Carbon<br />

Fibers America, Inc., USA. It is the highest strength, standard modulus fiber in the form of<br />

continuous filament tows with outstanding processing characteristics for filament winding,<br />

weaving and prepregging produced using the PAN (polyacrylonitrile) process.<br />

The epoxy system used was CR46T. It’s a high temperature cure prepreg resin system.<br />

To avoid degradation of its properties, the resin is kept under sub-zero temperatures in a<br />

sealed atmosphere. This resin system is well suited for prepreg applications, and its properties<br />

are shown in Table 1.<br />

Table 1. Resin properties<br />

Density 0.0457 lb/in 3<br />

Gell (min) @ 350 0 F 6 – 10<br />

GIC<br />

0.733<br />

lb/in<br />

± 0.3<br />

2<br />

Tg DRY 2hr @ 375 0 F 437 0 F<br />

Tg WET 2hr @ 375 0 F 295 0 F<br />

Tensile strength @ RT 10 ksi<br />

Tensile modulus @ RT 643 ksi<br />

Poisson ratio 0.36<br />

Elongation 1.7 %<br />

The nanosized fillers for this present investigation were chosen as nano-sized silicon<br />

carbide particles. These are highly complex material existing primarily in amorphous or<br />

crystalline states. The amorphous SiC is mainly used in coating industries. In functional and<br />

structural applications, crystalline SiC are extensively used due to their excellent thermomechanical<br />

properties such as high hardness and stiffness, good corrosion and oxidation<br />

resistance, high thermal conductivity and high chemical and thermal stability. [10-12]. Such<br />

SiC is available in two different phases, namely alpha (α) and beta (β) phases. The formation<br />

of these two structures depends on the molecular organization of the basic structural unit, a 2layer<br />

planner unit of Si and C in tetrahedral coordination. β−SiC is formed when the planes of<br />

Si and C are rearranged in a cubic symmetry with a lattice constant a = 0.4358 nm. On the<br />

other hand, heating of β−SiC to high temperature causes the transformation of the cubic<br />

symmetry to a mixture of hexagonal (6H) and rhombohedral (15R) polytypes known as α-<br />

SiC. The corresponding lattice constant parameters of α-SiCs are: a = 0.3082 nm and c =

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