When a composite
barrel is subjected to
high heat from rapid or prolonged firing, however, they are usually less durable than
solid steel barrels.
Even with the addition of thermally conductive chopped carbon
pitch, however, rapidly firing a gun fitted with a
carbon fiber composite barrel may cause barrel temperatures to significantly exceed the use-temperature capability of
epoxy resins.
At the Tg, the PMC softens significantly and the
mechanical integrity of the composite barrel is compromised.
Because all of these thermally conductive additives tend to strongly increase the
viscosity of the resin, however, higher concentrations of the thermally conductive additive make the resin mixture more viscous, inhibiting complete
coating of the carbon
fiber tow with resin and making manufacturing more difficult and less consistent.
Additionally, high loadings of conductive additives generally diminish the mechanical properties (e.g., strength) of the composite.
Other resins having higher
glass transition temperatures than
epoxy exist, but they are generally more difficult to process and manufacture PMC articles with and are significantly more expensive than epoxies.
Although cured
polyimide resins have superior thermal performance as compared to epoxy resins, many have relatively high
toxicity from the solvents and monomers used in their manufacture.
The RP46 resin, however, at high enough solids concentration for manufacturing PMCs is semi-
solid at
room temperature; its high
viscosity makes it very difficult to work with when “wet” winding
fiber filament tows.
When curing a wound
gun barrel that inherently has minimal part “edges”, however, it has proven difficult to remove the volatile products and gasses because they tend to become trapped between the continual filament windings.
This problem is compounded when utilizing the higher
viscosity polyimide resins.
Despite the advantages of using a polyimide resin to wrap a thin cylinder such as a
small caliber gun barrel, use of polyimide resins for PMCs—even with alternative composite manufacturing techniques such prepreg, towpreg, and resin transfer infusion—has been substantially confined to flat or relatively large
radius carbon fiber sheets or panels.
PEEK is significantly more expensive than epoxies.
Further, the
glass transition temperature of PEEK is only about 290° F., with (even more costly) higher-temperature formulations exhibiting glass transition at about 315° F. These glass transition temperatures are still lower than desirable in a rapid-fire weapon.
When a PMC is used as an outer shell for a barrel, solving the heat problem is difficult because most heat must be conducted radially to the outside surface of the barrel and ambient
atmosphere, through the composite shell, requiring heat to transfer through resin and transversely across individual fibers.
However, the interstitial space is not uniform; the space may range from, for example, from about <1 micron to about 50 microns.
Therefore, effective quantities of particles
sized small enough to occupy the smaller interstitial spaces will tend to make the resin mixture too viscous, and may locally weaken the matrix if / where the smaller additive particles “clump” in the larger interstitial spaces.
On the other hand, if the thermally conductive material particles are sized too large, larger than available interstitial spaces, they will not fit into the smaller interstitial spaces, thus displacing the continuous reinforcing fibers.