Wet/Hand Lay-up
Description:
Resins are impregnated by hand into fibres which are in the form
of woven, knitted, stitched or bonded fabrics. This is usually
accomplished by rollers or brushes, with an increasing use of
nip-roller type impregnators for forcing resin into the fabrics by
means of rotating rollers and a bath of resin. Laminates are left
to cure under standard atmospheric conditions.
Materials Options:
- Resins: Any, e.g. epoxy, polyester, vinylester, phenolic
- Fibres: Any, although heavy aramid fabrics can be hard to
wet-out by hand.
Typical Applications:
Standard wind-turbine blades, production boats, architectural
mouldings.
Main Advantages:
- Widely used for many years.
- Simple principles to teach.
- Low cost tooling, if room-temperature cure resins are
used.
- Wide choice of suppliers and material types.
- Higher fibre contents and longer fibres than with spray
lay-up.
Main Disadvantages:
- Resin mixing, laminate resin contents, and laminate quality are
very dependent on the skills of laminators. Low resin content
laminates cannot usually be achieved without the incorporation of
excessive quantities of voids.
- Health and safety considerations of resins. The lower molecular
weights of hand lay-up resins generally mean that they have the
potential to be more harmful than higher molecular weight products.
The lower viscosity of the resins also means that they have an
increased tendency to penetrate clothing.
- Limiting airborne styrene concentrations to legislated levels
from polyesters and vinylesters is becoming increasingly hard
without expensive extraction systems.
- Resins need to be low in viscosity to be workable by hand. This
generally compromises their mechanical/thermal properties due to
the need for high diluent/styrene levels.
Prepregs
Description:
Fabrics and fibres are
pre-impregnated by the materials manufacturer, under heat and
pressure or with solvent, with a pre-catalyzed resin. The catalyst
is largely latent at ambient temperatures giving the materials
several weeks, or sometimes months, of useful life when defrosted.
However to prolong storage life the materials are stored frozen.
The resin is usually a near-solid at ambient temperatures, and so
the pre-impregnated materials (prepregs) have a light sticky feel
to them, such as that of adhesive tape. Unidirectional materials
take fibre direct from a creel, and are held together by the resin
alone. The prepregs are laid up by hand or machine onto a mould
surface, vacuum bagged and then heated to typically 120-180°C. This
allows the resin to initially reflow and eventually to cure.
Additional pressure for the moulding is usually provided by an
autoclave (effectively a pressurized oven) which can apply up to 5
atmospheres to the laminate.
Materials
Options:
- Resins: Generally epoxy, polyester, phenolic and high
temperature resins such as polyimides, cyanate esters and
bismaleimides.
- Fibres: Any. Used either direct from a creel or as any type of
fabric.
- Cores: Any, although special types of foam need to be used due
to the elevated temperatures involved in the process.
Typical Applications:
Aircraft structural components (e.g. wings and tail sections),
F1 racing cars, sporting goods such as tennis racquets and
skis.
Main Advantages:
- Resin/catalyst levels and the resin content in the fibre are
accurately set by the materials manufacturer. High fibre contents
can be safely achieved.
- The materials have excellent health and safety characteristics
and are clean to work with.
- Fibre cost is minimized in unidirectional tapes since there is
no secondary process to convert fibre into fabric prior to
use.
- Resin chemistry can be optimized for mechanical and thermal
performance, with the high viscosity resins being impregnable due
to the manufacturing process.
- The extended working times (of up to several months at room
temperatures) means that structurally optimized, complex lay-ups
can be readily achieved.
- Potential for automation and labour saving.
Main Disadvantages:
- Materials cost is higher for preimpregnated fabrics.
- Autoclaves are usually required to cure the component. These
are expensive, slow to operate and limited in size.
- Tooling needs to be able to withstand the process temperatures
involved.
- Core materials need to be able to withstand the process
temperatures and pressures.