Curing composites out-of-autoclave using induction heating with smart susceptors

Patent metadata

Field	Value
Publication number	US-10425997-B2
Application number	US-201615012843-A
Country	US
Kind code	B2
Filing date	Feb 1, 2016
Priority date	Dec 15, 2009
Publication date	Sep 24, 2019
Grant date	Sep 24, 2019

Abstract

A composite part is cured out-of-autoclave using an inductively heated, stand-alone tooling. The part in placed on a tool and is covered by a heating blanket. One side of the part is heated by inductive coil circuits in the tool, and the other side of the part is heated by inductive coil circuits in the blanket.

First claim

What is claimed is:

1. A method of out-of-autoclave curing a composite part, comprising:
placing the composite part to be cured on a tool comprising a substantially rigid base;
heating a first side of the composite part via:
coupling a plurality of inductive coil circuits in parallel with each other, such that each circuit in the plurality of inductive coil circuits comprises, respectively, an inductive coil and a susceptor comprising a Curie temperature;
driving each of the plurality of inductive coil circuits with an alternating electrical current; and
shunting power away from a circuit in the plurality of inductive coil circuits when the susceptor in the circuit reaches the Curie temperature;

placing a heating blanket on a second side of the composite part; and
using the heating blanket to heat the composite part from the second side thereof.

2. The method of claim 1 , wherein inductively heating the tool includes:
flowing electrical current through at least one conductor passing through the tool;
using electrical current flow to heat the susceptor within the tool; and
conducting heat from the susceptor through a matrix in the heating blanket to a surface of the tool in contact with the first side of the composite part.

3. An out-of-autoclave method of curing of a part of a composite aircraft, comprising:
fabricating a tool by encasing a plurality of first induction heating coil circuits in a layer of polymer resin, including coupling the first induction heating coil circuits in parallel with each other, each of the first induction heating coil circuits including an induction coil and a susceptor having a first Curie temperature;
supporting the tool on a tool base;
hollowing out one side of the tool base to dissipate heat used to cure the part;
placing the part to be cured on the tool with a first side of the part in contact with the layer of polymer resin;
heating the first side of the part using the tool, including using the plurality of first induction heating coil circuits to heat the layer of polymer resin and shunting power away from at least one of the first induction heating coil circuits to the other of the first induction heating coil circuits when the susceptor in the one of the first induction heating coil circuits reaches the first Curie temperature;
fabricating a heating blanket by embedding a plurality of second induction heating coil circuits in an elastomeric matrix, each of the second induction heating coil circuits including a second induction coil and a second susceptor comprising a second Curie temperature;
placing the heating blanket on the tool and in contact with a second side of the part, including conforming the heating blanket to the second side of the part;
coupling an AC power supply in series with the plurality of first induction heating coil circuits and in series with the plurality of second induction heating coil circuits; and
using the heating blanket to heat the second side of the part including using the plurality of second induction heating coil circuits to heat the elastomeric matrix, and shunting power away from at least one of the second induction heating coil circuits to the other of the second induction coil heating circuits when the susceptor in the one of the second induction heating coil circuits reaches the second Curie temperature.

4. The method of claim 1 further comprising:
prior to placing, fabricating the tool by encasing a plurality of first induction heating coil circuits in a layer of polymer resin.

5. The method of claim 4 , wherein fabricating further comprises:
coupling the first induction heating coil circuits in parallel with each other.

6. The method of claim 5 , further comprising:
hollowing out one side of the tool to form a hollow; and
using the hollow to dissipate heat while using the heating blanket to heat the composite part.

7. The method of claim 6 , wherein placing the composite part further comprises:
placing the composite part with a first side of the composite part in contact with the layer of polymer resin.

8. The method of claim 7 further comprising:
driving each of the first induction heating coil circuits with an alternating electrical current; and
shunting power away from one of the first induction heating coil circuits when the susceptor reaches its Curie temperature.

9. The method of claim 8 further comprising;
prior to placing the heating blanket, fabricating the heating blanket by embedding a plurality of second induction heating coil circuits in a thermally conductive elastomeric matrix.

10. The method of claim 9 , further comprising:
conforming the heating blanket to the second side of the composite part.

11. The method of claim 10 further comprising:
coupling an AC power supply in series with the plurality of first induction heating coil circuits and in series with the plurality of second induction heating coil circuits.

12. The method of claim 11 , wherein using the heating blanket to heat the composite part comprises:
using the plurality of second induction heating coil circuits to heat the thermally conductive elastomeric matrix.

13. The method of claim 12 further comprising:
shunting power away from at least one of the second induction heating coil circuits to another of the second induction coil heating circuits when a second susceptor reaches its Curie temperature.

14. The method of claim 3 , wherein the layer of polymer resin comprises a rigid layer of polymer resin.

15. The method of claim 14 , wherein the heating blanket comprises a flexible heating blanket.

16. The method of claim 15 , wherein the elastomeric matrix comprises a thermally conductive elastomeric matrix.

17. The method of claim 15 , wherein fabricating the heating blanket comprises forming a susceptor sleeve extending over a conductor for inductive heating of the susceptor sleeve.

18. The method of claim 1 , further comprising a heat sink adjacent to the susceptor.

19. The method of claim 4 , further comprising the layer of polymer resin comprising a rigid layer of polymer resin.

20. The method of claim 3 , further comprising the tool base comprising a rigid form.

Assignees

• Boeing Co

Inventors

• Matsen Marc Rollo
• Miller Robert James
• Negley Mark Alan
• Noel Jennifer Sue

Classifications

• B29C73/30

  for local pressing or local heating · CPC title

• B29K2105/253

  Preform · CPC title

• B29C2035/0811

  using induction · CPC title

• B29C73/34

  for local heating · CPC title

• H05B6/106

  in the form of fillings · CPC title