Induction heating augmentation for thermal curing

Patent metadata

Field	Value
Publication number	US-9277594-B2
Application number	US-201313770235-A
Country	US
Kind code	B2
Filing date	Feb 19, 2013
Priority date	Feb 19, 2013
Publication date	Mar 1, 2016
Grant date	Mar 1, 2016

Abstract

The thermal cycle time for curing a thermoset composite part in an autoclave is reduced by placing a heating blanket in proximity to an area of the composite part that is slow-to-heat, and inductively heating the area of the composite part that is slow-to-heat using the heating blanket.

First claim

What is claimed is:

1. A method of curing a thermoset resin part, comprising:
placing an assembly of a thermoset resin part and a cure tool inside an autoclave;
placing a heating blanket in proximity to an area of the assembly that is normally slow-to-heat during a thermal cure cycle;
using the autoclave to heat the assembly; and,
using heating blanket to heat the area of the assembly that is slow-to-heat by inductive heating.

2. The method of claim 1 , wherein placing the heating blanket is performed by placing the heating blanket against a portion of the assembly having a mass is substantially greater than the mass of other portions of the assembly.

3. The method of claim 2 , wherein placing the heating blanket against a portion of the assembly is performed by placing the heating blanket against a surface of the tool.

4. The method of claim 1 , further comprising:
placing the thermoset resin part on one side of the cure tool, and,
placing the heating blanket in proximity to the area of the assembly that is slow-to-heat includes placing the heating blanket on a side of the cure tool opposite the one side thereof.

5. The method of claim 1 , wherein the inductive heating is performed by:
inductively heating a susceptor sleeve in response to a magnetic field, and,
reducing the inductive heating of the susceptor sleeve when the susceptor sleeve becomes non-magnetic upon reaching a Curie temperature of the susceptor sleeve.

6. The method of claim 5 , further comprising the step of:
applying alternating current to a conductor having the susceptor sleeve mounted thereto, the susceptor sleeve being formed of magnetic material having the Curie temperature.

7. The method of claim 5 , further comprising:
selecting a susceptor sleeve having a Curie temperature that is substantially equal to the cure temperature of the thermoset resin part.

8. A method of reducing the thermal cycle time required for heating a composite part in heating chamber, comprising:
placing a heating blanket in proximity to an area of the composite part that is slow-to-heat; and
inductively heating the area of the composite part that is slow-to-heat using the heating blanket by:
inductively heating a susceptor sleeve in response to a magnetic field,
reducing the inductive heating of the susceptor sleeve when the susceptor sleeve becomes non-magnetic upon reaching a Curie temperature of the susceptor sleeve,
applying alternating current to a conductor having the susceptor sleeve mounted thereto, the susceptor sleeve being formed of magnetic material having the Curie temperature, and
generating a magnetic field along the length of the susceptor sleeve in response to the alternating current.

9. The method of claim 8 , wherein placing a heating blanket in proximity to an area of the composite part includes placing the heating blanket against a tool that contacts the composite part.

10. A method of heating a composite part having areas of differing thermal mass or differing thermal insulation characteristics, comprising:
placing the composite part on a cure tool;
placing the cure tool and composite part in an autoclave;
using the autoclave to apply external heat to the tool and the composite part; and,
augmenting the heat supplied to an area of the composite part having high mass or thermal insulation characteristic by inductively heating the area.

11. The method of claim 10 , wherein augmenting the heat supplied to the area of the composite part includes placing an inductive heating blanket in proximity to the area.

12. The method of claim 10 , wherein placing the inductive heating blanket in proximity to the area includes placing the heating blanket against one of the tool and surfaces of the composite part.

13. An apparatus for thermally curing a thermoset part on a tool, comprising:
an autoclave adapted to have the combination of the tool and the thermoset part placed therein, the autoclave including a heating element adapted to provide heat to the combination of the tool and the thermoset part; and,
at least one heating blanket in the autoclave for generating heat in a local area of the combination of the tool and the thermoset part wherein the heating blanket is an induction heater.

14. The apparatus of claim 13 , wherein the heating blanket is located in an area of the combination of the tool and the part having a mass greater than other areas of the combination of the tool and the part.

15. The apparatus of claim 13 , wherein:
the heating blanket includes a matrix in thermal contact with a susceptor sleeve.

Assignees

• Boeing Co

Inventors

• Matsen Marc Rollo
• Miller Robert James
• Smith Brian W
• Butler Geoffrey Allen
• Nelson Karl Marius

Classifications

• B29C35/0227 Primary

  using pressure vessels, e.g. autoclaves, vulcanising pans (B29C35/065 takes precedence) · CPC title

• B29C2035/0816

  using eddy currents · CPC title

• B29C35/0805

  using electromagnetic radiation · CPC title

• B29C2035/0811

  using induction · CPC title

• H05B1/00 Primary

  Details of electric heating devices · CPC title