Resistively heated thermoplastic washout mandrel
The present disclosure is directed to a method of forming a composite component. The method includes laying one or more layers of uncured composite material onto a mandrel. The mandrel which includes a plurality of conductive media dispersed in a thermoplastic material. An electric current is supplied to the mandrel to resistively heat the one or more layers of uncured composite material to a temperature sufficient to cure the one or more layers of uncured composite material to form a cured composite component. The mandrel is removed from the cured composite component.
1. A method of forming a composite component, comprising:
laying one or more layers of uncured composite material onto a mandrel, the mandrel comprising a plurality of conductive media dispersed in a thermoplastic material, wherein the thermoplastic material of the mandrel has a glass transition temperature, and wherein the uncured composite material has a glass transition temperature;
supplying an electric current to the mandrel to resistively heat the mandrel and the one or more layers of uncured composite material to a temperature above both the glass transition temperature of thermoplastic material of the mandrel and the glass transition temperature of the uncured composite material;
deforming the mandrel and the uncured composite material from a first shape to a second shape;
curing the uncured composite material; and
removing the mandrel from the composite component.
2. The method of claim 1 , wherein the cured composite material remains in the second shape after curing and removing the mandrel.
3. The method of claim 1 , wherein removing the mandrel comprises dissolving the mandrel with a solvent.
4. The method of claim 3 , wherein the solvent comprises acetone, the thermoplastic material of the mandrel comprises polycarbonate, and the one or more layers of uncured composite tape comprise polyether ether ketone.
5. The method of claim 1 , wherein the plurality of conductive media comprise carbon black or carbon nanotubes.
6. The method of claim 1 , wherein the one or more layers of uncured composite tape comprise a thermoplastic polymeric matrix composite tape.
7. The method of claim 1 , wherein the cured composite component is a tube, a duct, an airfoil, or a curved panel.