| KEYWORD |
DESCRIPTION |
| Carbon
Fiber |
Reinforcing
fiber known for its high strength and high stiffness. Fibers are produced
by high temperature treatment of an organic precursor fiber based
on PAN (polyacrylonitrile), rayon or pitch in an inert atmosphere
at temperatures above 1,800 ° F |
| Composite |
A
material that combines fiber reinforcements and a binding matrix to
maximize specific performance properties. The final part can achieve
mechanical properties of great strength and stiffness along the designed
load axi. |
| Core |
In
sandwich construction, the central component to which inner and outer
lamiante skins are attached. Foam, honeycomb, paper and wood and aluminium
are all commonly used as a core material. A core is the web in an
"I" beam. |
| Cross
Lamination |
Layers
oriented at various to other layers with respect to the laminate grain.
A cross-ply laminate usually has plies oriented only at 0°/ 90°.
(see Fiber Architechture) |
| Cure |
To
irreversibly change the molecular structure and physical properties
of a thermosetting resin by chemical reaction via heat and catalysts
alone or in combination, with or without pressure. |
| Delamination |
The
seperation of ply layers due to adhesive failure. A delamination may
be associated with bridging, drilling and trimming, thermal failure
or mechanical stress. |
| E-Glass |
Borosilicate
glass fibers most often used in conventional polymer matrix composites.
This is the most common reinforcement used in the marine industry. |
| Epoxy
Plastics |
Thermoset
resins made by reaction of epoxides with other materials such as amines
and alcohols; used as a matrix resin in reinforced composites and
structural adhesives. |
| Epoxy
Resin |
A
common thermoset material used as a bonding matrix to hold fibers
together when mixed with a hardener. Epoxies are very stable and resistant
to cyclic fatigue. |
| Exotherm |
Heat
released during a chemical reaction for example the curing of a matrix. |
| Fiber
Architecture |
The
design of a composite part in which the fibers are arranged in a particular
way as to achieve the desired mechanical charasteristics. This may
include braided, stitched or wowen fabrics, mats, rovings or carbon
tows. |
| Fiber
Content |
The
amount of fiber in a composite expressed as a ratio to the matrix.
(The most desirable fiber content is 60:40 ratio, or 60% fiber and
40% matrix resin) |
| Fiberglass |
Reinforcing
fiber made by drawing molten glass through bushings. The predominant
reinforcement for polymer matrix composites, it is known for its good
strength, processability and low cost. |
| Hybrid
Composite |
A
composite made with two or more types of reinforcing fibers. |
| Kevlar |
A
strong, lightweight aramid fiber trademarked by DuPont and used as
a reinforcement fiber. |
| Laminate |
To
unite layers with a bonding material, usally via pressure and heat. |
| Matrix |
The
material in which the fiber reinforcements of a composite system are
embedded. Thermoplastic and thermoset resin systems, as well as metal
and ceramic, can be used. |
| Microcracking |
Cracking
in composites at points where thermal stresses exceed the strength
of the matrix. |
| Modulus |
The
physical measurement of stiffness in a material, equalling the ratio
of applied load (stress) to the resultant derformation of the material,
such as elasticity or shear. (A high modulus indicates a stiff material) |
| Mold |
The
cavity or matrix into or on which the resin/ fiber material is placed
and from which it takes form. |
| Molding |
The
forming of a resin/ fiber material into a solid mass of prescribed
shape and size. |
| One-Off |
A
single part that is individually fabricated |
| Outgassing |
The
release of solvents and moisture from composite parts under a vacuum. |
| Peel
Ply |
Layer
of material applied to a lay up surface that is removed from the cured
laminate prior to bonding operations, leaving a clean, resin-rich
surface ready for bonding. |
| Pin
Holes |
Small
holes caused by the mold used. ? or other undescribing things! |
| Postcure |
Additional
elevated temperature cure, usually without pressure, to improve final
properties and/ or complete cure the cure. In certain resins, complete
cure and ultimate mechanical properties are attained only by exposure
of the cured resin to higher temperatures than those of curing. |
| Prepreg |
Resin-impregnated
fibers, fabric or mat in flat form that is preimpregnated with resin
before being stored for later use in molds and in hand layup. |
| Reinforcement |
The
key element added to matrix to provide required properties (primarily,
strength and stiffness); ranges from short fibers and continuous fibers
through complex textile forms. |
| Resin |
A
solid or pseudosolid material with indefinite and often high molecular
weight and a softening or melting range that exhibits a tendency to
flow when subjected to stress. (As composite matrices, resins bind
together reinforcement fibers) |
| Resin
System |
A
mixture of resin and ingredients required for an intended processing
method and final product. |
| S-Glass |
Magnesia/
alumina/ silicate glass reinforcement designed to provide very high
tensile strength. (Commonly used in high-performance parts) |
| Sandwich
Structure |
A
composite composed of lightweight core material to which two relatively
thin, dense, high-strength, funtional or decorative laminate skins
are adhered. |
| Stress |
Internal
resistance to change in size or shape, expressed in force per unit
area. |
| Thermoplastic |
A
composite matrix capable of being repeatedly softened by an increase
in temperature and hardened by a decrease in temperature. |
| Thermoset |
Composite
matrix cured by heat and pressure or with a catalyst into an infusible
and insoluble material. Once cured, a thermoset cannot be returned
to the uncured state. |
| Unidirectional
(UD) |
Orientation
of fibers in the same direction, as in unidirectional fabric, tape
or laminate. |
| Vacuum
Bag Molding |
A
molding technique wherein the part is cured inside a layer of film
from which entrapped air is removed by vacuum. |
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