NIST
GCR 04-863
Composites Manufacturing Technologies: Applications in Automotive, Petroleum,
and Civil Infrastructure Industries
Economic Study of a Cluster of ATP-Funded Projects
Appendix 3: Composite Materials
for Engineered Products
Engineers can utilize
over 50,000 materials for the design and manufacture of engineered products.
These materials, depending on their mechanical and physical characteristics
such as strength, stiffness, density, melting temperature, and conductivity,
can be divided into four main categories: metals, plastics, ceramics,
and composites.
While metals and plastics
are currently the dominant materials for engineering applications, there
has been an increasing utilization of composite materials, reflecting
their superior performance characteristics. The key factor holding back
additional increases in composite utilization has been the high cost
of composites.
Composites are systems
composed of at least two distinctly dissimilar materials, acting in concert.
The properties of the polymeric composite system are not attainable by
individual components acting alone. Engineered composites can be defined
as systems of reinforcing fibrous materials in a polymer matrix binder.
The reinforcing fiber
provides strength and stiffness to the composite. The matrix material
binds the fibers together, provides form and rigidity, transfers the
load to the fibers, and protects the load-bearing fiber from corrosion
and wear. For composites in structural applications, continuous or long-fiber
configurations are typical, whereas for nonstructural applications, short
fibers can be used (Figure A3-1).
Figure
A3-1: Continuous-Fiber versus Short-Fiber Composites
Common composite
reinforcing fibers include glass fibers and carbon/graphite fibers.
For specialized applications, boron and aramid (Kevlar) fibers can
also be used. General fiber properties are described below:
- Kevlar fibers are
organic fibers which have high strength and stiffness which is possible
in fully aligned polymers. Kevlar fibers have a very low resistance
to failure under axial compression.
- Glass fibers (fiberglass)
have excellent electrical insulating properties, good chemical and
moisture resistance, and low cost. Glass fibers come in several grades
(higher performance S-glass with greater tensile strength and higher
use temperatures versus lower performance E-glass) and are widely
used in industrial composites.
- Carbon/graphite
fibers are high-strength, high-modulus, lightweight fibers, used
as reinforcement for high-performance applications.
- Mixed fiber structures
use a combination of Kevlar, glass, carbon, or other fibers to fabricate
hybrid composites to optimize composite properties and cost.
The matrix material
(polymer resin and elastomer) surrounds and binds the fiber in the
composite structure and has a lower modulus and greater elongation
than the fiber reinforcement. The matrix determines the service operating
temperature of a composite as well as processing parameters for parts
manufacturing. Polymer matrix materials may come as thermoset and
thermoplastic resins:
- During curing, thermoset
resins form three-dimensional molecular chains (crosslinking chains)
and, once cured, cannot be remelted and reformed. The higher degree
of the cross-linking chains, the more rigid and thermally stable
the composite material will be. The most common resin materials are
epoxy, polyester, vinyl ester, phenolics, and cyanate esters.
- Thermoplastic resin
molecules do not cross-link and thus remain flexible and reformable.
They are, in general, more ductile and tougher than thermosets and
are used in a wide variety of industrial (nonstructural) applications.
At the same time, they have lower stiffness and strength values,
which can be selectively improved by the appropriate choice of fiber
reinforcement. Typical thermoplastic resins include nylon, polypropylene,
polyetheretherketone (PEEK), polyester, and teflon.
Table A3-1 indicates representative
physical properties of various composites, compared to common engineering
materials. Composite materials have high specific strength (strength-to-density
ratio) and high specific stiffness (modulus-to-density ratio).
Table
A3-1: Typical Properties of Some Engineering Materials
|
Density
g/cc
(r) |
Tensile
strength
MPa
(s) |
Tensile
modulus
GPa
(E) |
Specific
strength
(s/r) |
Specific
modulus
(E/r) |
Max.
service
temp
(°C) |
Metals |
Steel, ASI 1045
HR |
7.8 |
0.57 |
205 |
0.073 |
26.3 |
500-650 |
Aluminum 2024-T4 |
2.7 |
0.45 |
23` |
0.17 |
27.0 |
150-250 |
|
Polymer
without reinforcement |
Nylon 6,6 |
1.15 |
0.082 |
2.9 |
0.071 |
2.52 |
75-100 |
Epoxy |
1.25 |
0.069 |
3.5 |
0.055 |
2.80 |
80-215 |
|
Reinforced
polymers with continuous fiber (% by weight) |
S-glass/epoxy
(45%) |
1.81 |
0.87 |
39.5 |
0.48 |
21.8 |
80-215 |
Carbon/epoxy (61%) |
1.59 |
1.73 |
142 |
1.08 |
89.3 |
80-215 |
|
Reinforced
polymer with short fiber (% by weight) |
Glass/epoxy (35%) |
1.90 |
0.30 |
25 |
0.16 |
8.26 |
80-200 |
Glass/nylon (35%) |
1.62 |
0.20 |
14.5 |
0.12 |
8.95 |
75-110 |
Source: Mazumdar
2002.
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of Contents or go to next section.
Date created: July 14,
2004
Last updated:
August 3, 2005
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