System and apparatus for manufacturing simple curvature thermoplastic composite parts
A system for manufacturing a composite part including a conductive flexible facesheet and an automated tape layup (ATL) machine for laying up composite tape onto the facesheet that is laid flat on a flat surface. The system also includes a curved tooling surface for transferring the facesheet with the composite material thereon to the curved tooling surface for attachment of substructures and curing into the composite part. System may also include insulation placed below the facesheet and insulation placed above the composite material, as well as a source of electricity and heat for heating the conductive facesheet to cure, melt, or fuse the composite tape and substructures without heating the tooling surface and other tooling used in the composite curing process. Heating of the facesheet may be performed using joule heat provided by a single turn transformer inducing current to conductive wires attached at opposing ends to the facesheet.
1. A system for forming a composite part, the system comprising:
a facesheet made of a conductive material for placement of the composite part thereon;
a tooling surface;
a first insulating material positioned onto the tooling surface, wherein the facesheet is positioned on the first insulating material, wherein at least a portion of the tooling surface is not flat; and
a source of heat or electricity at least one of physically and electrically coupled to the facesheet,
wherein the source of heat or electricity includes two bus bars at opposing ends of the facesheet and one or more conductive wires providing joule heating to the face sheet,
wherein the source of heat or electricity further comprises a single turn transformer, wherein the one or more conductive wires extend from one of the bus bars to another one of the bus bars and are threaded through an air gap of the single turn transformer such that heating the facesheet includes inducing current into the one or more conductive wires with the single turn transformer.
2. The system of claim 1 , further comprising an impermeable membrane for placement over the composite part, wherein the impermeable membrane is sealed to the tooling surface and applies consolidation pressure to the composite part when a pressure differential is applied to the impermeable membrane forcing the impermeable membrane toward the tooling surface.
3. The system of claim 1 , wherein the tooling surface is curved and the facesheet is curved by the tooling surface.
4. The system of claim 1 , further comprising a second insulating material for placement over the composite part, wherein the second insulating material is an insulating sheet cut to allow at least one substructure of the composite part to protrude therethrough, such that the second insulating material serves as a template for locating the substructure at a predetermined location on a skin of the composite part.
5. The system of claim 1 , wherein the facesheet is made of steel.
6. The system of claim 1 , further comprising an automated tape layup (ATL) machine for laying strips of composite material onto the facesheet on a flat surface prior to insertion of the facesheet onto the tooling surface.
7. The system of claim 6 , further comprising a magnet-placement apparatus operable to lay down and pick up magnets by effectuating a change in polarity, wherein the magnet-placement apparatus is configured to place magnets onto a first layer of strips of composite material during layup by the ATL machine and to pick up magnets from the strips of composite material prior to the ATL machine placing a second layer of strips of composite material.
8. A system for forming and curing a composite part, the system comprising:
a facesheet made of a conductive sheet of material for placement of the composite part thereon, the facesheet having opposing ends;
a tooling surface, wherein the tooling surface is made of insulating material or a first insulating material is positioned onto the tooling surface, wherein the facesheet is positioned on at least one of the tooling surface and the first insulating material, wherein the tooling surface has a simple curvature;
a second insulating material for placement over the composite part; and
a source of joule heat at least one of physically and electrically coupled to the facesheet,
wherein the source of joule heat is electrically coupled with the opposing ends of the facesheet to provide joule heating to the facesheet,
wherein the source of joule heat comprises a single turn transformer and one or more conductive wires extending from one of the opposing ends of the facesheet to another one of the opposing ends of the facesheet, wherein the one or more conductive wires are threaded through an air gap of the single turn transformer such that inducing current into the one or more conductive wires with the single turn transformer heats the facesheet.
9. The system of claim 8 , further comprising an impermeable membrane for placement over the second insulating material and the composite part, wherein the impermeable membrane is sealed to the tooling surface and applies consolidation pressure to the composite part when a pressure differential is applied to the impermeable membrane forcing the impermeable membrane toward the tooling surface.
10. The system of claim 8 , wherein the second insulating material is an insulating sheet cut to allow at least one substructure of the composite part to protrude therethrough, such that the second insulating material serves as a template for locating the substructure at a predetermined location on a skin of the composite part.
11. The system of claim 8 , further comprising an automated tape layup (ATL) machine for laying strips of composite material onto the facesheet on a flat surface prior to insertion of the facesheet onto the tooling surface.
12. The system of claim 11 , further comprising a magnet-placement apparatus operable to lay down and pick up magnets by effectuating a change in polarity, wherein the magnet-placement apparatus is configured to place magnets onto a first layer of strips of composite material during layup by the ATL machine and to pick up magnets from the strips of composite material prior to the ATL machine placing a second layer of strips of composite material.
13. A system for forming and curing a thermoplastic composite part, the system comprising:
a facesheet made of a conductive sheet of material for placement of the thermoplastic composite part thereon;
an automated tape layup (ATL) machine for laying strips of composite material onto the facesheet on a flat surface;
a magnet-placement apparatus operable to lay down and pick up magnets by effectuating a change in polarity, wherein the magnet-placement apparatus is configured to place magnets onto a first layer of the strips of composite material during layup by the ATL machine and to pick up magnets from the first layer of the strips of composite material prior to the ATL machine placing a second layer of the strips of composite material;
a tooling surface, wherein the tooling surface is made of insulating material or a first insulating material is positioned onto the tooling surface, wherein the facesheet is transferable from the flat surface onto the at least one of the tooling surface and the first insulating material, wherein the tooling surface has a simple curvature to which the facesheet is conformable upon transfer from the flat surface;
a second insulating material for placement over the strips of composite material when the facesheet is on the at least one of the tooling surface and the first insulating material;
an impermeable membrane placed over the second insulating material and the thermoplastic composite part, wherein the impermeable membrane is sealed to the tooling surface and is configured to apply consolidation pressure to the thermoplastic composite part when a pressure differential is applied to the impermeable membrane forcing the impermeable membrane toward the tooling surface; and
a source of joule heat at least one of physically and electrically coupled to the facesheet, wherein the source of joule heat includes at least two conductive bus bars attached to opposing ends of the facesheet, and one or more conductive wires providing current to heat the facesheet.
14. The system of claim 13 , wherein the second insulating material is an insulating sheet cut to allow a plurality of frames and stringers of the thermoplastic composite part to protrude therethrough, such that the second insulating material serves as a template for locating the frames and stringers at a predetermined location on a skin of the thermoplastic composite part.
15. The system of claim 13 , wherein the source of joule heat further includes a single turn transformer, wherein the at least two bus bars are made of copper, wherein the one or more conductive wires extend from one of the bus bars to another one of the bus bars and are threaded through an air gap of the single turn transformer such that heating the facesheet includes inducing current into the one or more conductive wires with the single turn transformer.