Why aren't Spectra and S-glass used very much?
From : Don Stackhouse
Paul,
Actually S-glass is used quite a bit. It has been used for many years
in helicopter rotor blades; in fact, in that application it was one of the
first composites used for primary structure in an aircraft. It has impact
strength rivaling Kevlar but has excellent compressive strength (unlike
Kevlar, whose compressive strength is less than half that of ordinary
E-glass!). We've used quite a bit of S-glass in Monarchs, particularly the
2-meter. The big reason you don't see more S-glass (besides its unfortunate
lack of publicity) is that its density, like E-glass, is higher than Kevlar
or carbon fiber. Its stiffness is also lower, although still better than
E-glass.
Depending on the design, these properties may or may not result in a heavier
structure. For example, in the case of helicopter rotors, one of the toughest
design requirements is making them strong enough to support their own weight
when they aren't turning (centrifugal force holds them out straight in
flight). A Kevlar rotor blade would require a huge amount of material on the
lower spar cap to carry the high compressive loads while parked, while an
S-glass blade can use a much thinner (and lighter) lower spar cap.
The lower stiffness of S-glass can also be used to an advantage: it can make
the laminate less sensitive to stress concentrations, and in the case of an
impact (such as the loads on a fuselage in a "dork" landing), the lower
stiffness allows the structure to deflect farther, which reduces the loads by
reducing the severity of the decelleration.
Spectra has a lot of wonderful and amazing properties, but also some terrible
shortcomings. The principle difficulty is its creep properties (also called
"cold-flow" and "relaxation"). This means that if you put it under a
sustained load it will gradually distort, stretching or compressing depending
on the nature of the load. This isn't a problem for fishing line, you just
have to turn the crank a little farther. On the other hand, an aircraft
component that won't hold its shape is a serious problem. How would you like
to have a fuselage with a tail boom that warped a few degrees due to gravity
while sitting on the shelf through the winter?
The bottom line is that composites have much more complex behavior than
conventional materials, which can create opportunities for the designer, but
can also create more ways to get into trouble. You have to thoroughly
understand the situation and do your homework when designing with composites!
Don Stackhouse @ DJ Aerotech
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