Composite Materials Research Progress
Composite Materials Research Progress
Composite Materials Research Progress
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Preface ix<br />
composite technology are realized in the Boeing Model 787 with over 50% by weight of<br />
composites, bringing the application of composites in large structures into a new age. This<br />
mostly-composite Boeing 787 has been credited with putting an end to the era of the all-metal<br />
airplane on new designs, and it is perhaps the most visible manifestation of the fact that<br />
composites are having a profound and growing effect on all sectors of society.<br />
It is generally well-known that composite materials are made of reinforcement fibers and<br />
matrix materials, and light weight and high mechanical properties are the primary benefits of<br />
a composite structure. Accordingly, the development trends in composite technology lie in 1)<br />
new material technology specifically for developing novel fibers and matrices, enhancing<br />
interfacial adhesion between fiber and matrix, hybridization and multi-functionalization, and<br />
2) more reliable, high quality, rapid and low cost manufacturing technology.<br />
New reinforcement fiber technology including next generation carbon fibers and organic<br />
fibers with improved mechanical and physical properties, such as Spectra®, Dyneema®, and<br />
Zylon®, have been developing continuously. More significantly, various nanotechnology<br />
based novel fiber reinforcements have conspicuously and rapidly appeared in recent years.<br />
Matrix materials have become as complex as the fibers, satisfying increasing demands for<br />
impact resistant and damage tolerant structure. Various means of accomplishing this have<br />
ranged from elastomeric/thermoplastic minor phases to discrete layers of toughened<br />
materials. Nano-modified polymeric matrices are mostly involved in the development trends<br />
for matrix polymer materials. Technology for enhancing the interfacial adhesion properties<br />
between the reinforcement and matrix for a composite to provide high stress-transfer ability is<br />
more critically demanded and the science of the interface is expanding. Fiber/matrix<br />
interfacial adhesion is vital for the application of the newly developed advanced<br />
reinforcement materials. Effective approaches to improving new and non-traditional<br />
treatment methods for better adhesion have just started to receive sufficient attention. Multifunctionality<br />
is also an important trend for advanced composites, in particular, utilizing<br />
nanotechnology developments in recent years to provide greater opportunities for forcing<br />
materials to play a more comprehensive role in the designs of the future.<br />
More reliable and low cost manufacturing technology has been pursued by industry and<br />
academic researchers and the traditional material forms are being replaced by those which<br />
support the growing need for high quality, rapid production rates and lower recurring costs.<br />
Major trends include the recognition of the value of resin infusion methods, automated<br />
thermoplastic processing which takes advantage of the unique advantages of that material<br />
class, and the value of moving away from dependence on the large and expensive autoclaves.<br />
In Chapter 4, an innovative manufacturing process was developed to fabricate<br />
nanophased carbon prepregs used in the manufacturing of unidirectional composite laminates.<br />
In this technique, prepregs were manufactured using solution impregnation and filament<br />
winding methods and subsequently consolidated into laminates. Spherical silicon carbide<br />
nanoparticles (β-SiC) were first infused in a high temperature epoxy through an ultrasonic<br />
cavitation process. The loading of nanoparticles was 1.5% by weight of the resin. After<br />
infusion, the nano-phased resin was used to impregnate a continuous strand of dry carbon<br />
fiber tows in a filament winding set-up. In the next step, these nanophased prepregs were<br />
wrapped over a cylindrical foam mandrel especially built for this purpose using a filament<br />
winder. Once the desired thickness was achieved, the stacked prepregs were cut along the<br />
length of the cylindrical mandrel, removed from the mandrel, and laid out open to form a<br />
rectangular panel. The panel was then consolidated in a regular compression molding