Abstract: Methods and a double vacuum processing system are presented. A method of performing a double vacuum debulk and cure on a composite laminate is presented. A composite laminate is heated to begin a double vacuum debulk of the composite laminate while vacuum is pulled in a first vacuum zone containing the composite laminate and a second vacuum zone containing the first vacuum zone. Pressure within the second vacuum zone is increased to above atmospheric pressure. Heating the composite laminate is continued to complete a cure cycle for the composite laminate while the second vacuum zone is above atmospheric pressure.

Abstract: An induction heating system and methods of forming an induction heating system are presented. The induction heating system comprises a conductor, a susceptor surrounding the conductor, and magnetic field reduction. The susceptor has a Curie temperature. The magnetic field reduction is configured to reduce magnetic fields escaping the induction heating system when the susceptor is at the Curie temperature independent of a layout of the induction heating system within an induction heating device.

Abstract: An induction curing system comprises a slip sheet and a power supply. The slip sheet comprises a layup surface configured to receive a composite material, a tool interface surface configured to interface with an upper surface of a tool, a rigid body extending between the layup surface and the tool interface surface, and an induction coil circuit within the rigid body of the slip sheet. The induction coil circuit is configured to heat the layup surface to a temperature sufficient to cure the composite material. The induction coil circuit has a diameter selected to generate heat using a power supply having a frequency below 150 kHz. The rigid body is configured to support the composite material during transport of the composite material. The power supply is coupled with the induction coil circuit, the power supply is selected based on the diameter of the induction coil circuit.

Abstract: A composite sandwich panel includes a first composite part and a second composite part. A plurality of stiffeners extend between the first and second composite parts. A fiberglass composite perimeter edge closeout is positioned along one or more edges of the first and second composite parts. The fiberglass composite perimeter edge closeout controls a magnetic flux to bond the first and second composite parts to the plurality of stiffeners.

Abstract: An apparatus for thermoplastic welding includes at least one tool configured to support first and second thermoplastic composite parts in a first welding position having one or more joint lines between the first and second thermoplastic composite parts. The tool includes a plurality of induction coils. The apparatus further includes a susceptor removably positioned along the one or more joint lines. The susceptor is configured to heat the one or more joint lines when exposed to a magnetic flux generated by the plurality of induction coils to bond the first and second thermoplastic composite parts along the one or more joint lines. The apparatus also includes a susceptor removal device coupled to the susceptor and configured to remove the susceptor during bonding of the first and second thermoplastic composite parts.

Abstract: A method for curing a thermoset composite part, including placing the composite part within a heating assembly and using the heating assembly to heat the composite part; placing the heating assembly within a pressurization vessel and applying a consolidation pressure; removing the heating assembly from the pressurization vessel and using the heating assembly to cool down the composite part.

Abstract: An apparatus for thermoplastic welding includes at least one tool configured to support first and second thermoplastic composite parts in a first welding position having one or more joint lines between the first and second thermoplastic composite parts. The tool includes a plurality of induction coils. The apparatus further includes a susceptor removably positioned along the one or more joint lines. The susceptor is configured to heat the one or more joint lines when exposed to a magnetic flux generated by the plurality of induction coils to bond the first and second thermoplastic composite parts along the one or more joint lines. The apparatus also includes a susceptor removal device coupled to the susceptor and configured to remove the susceptor during bonding of the first and second thermoplastic composite parts.

Abstract: A composite sandwich panel includes a first composite part and a second composite part. A plurality of stiffeners extend between the first and second composite parts. A fiberglass composite perimeter edge closeout is positioned along one or more edges of the first and second composite parts. The fiberglass composite perimeter edge closeout controls a magnetic flux to bond the first and second composite parts to the plurality of stiffeners.