Induction forming and curing of thermoset composite charges

Patent metadata

Field	Value
Publication number	US-10814526-B2
Application number	US-201715713424-A
Country	US
Kind code	B2
Filing date	Sep 22, 2017
Priority date	Sep 22, 2017
Publication date	Oct 27, 2020
Grant date	Oct 27, 2020

Abstract

A first tooling die and a second tooling die are movable with respect to each other. The first tooling die and the second tooling die form a die cavity. The first tooling die and the second tooling die comprise a plurality of stacked metal sheets. A plurality of air gaps is defined between adjacent stacked metal sheets. A first smart susceptor material is within the die cavity and connected to the first tooling die. The first smart susceptor material has a first Curie temperature. A second smart susceptor material is within the die cavity and associated with the second tooling die. The second smart susceptor material has a second Curie temperature lower than the first Curie temperature. A flexible membrane is between the second tooling die and the first smart susceptor material. The flexible membrane is configured to receive pressure.

First claim

What is claimed is:

1. A method comprising:
placing a thermoset composite charge within a die cavity of an induction tool, wherein the induction tool comprises a first tooling die and a second tooling die movable with respect to each other, and wherein the first tooling die and the second tooling die form the die cavity, the first tooling die and the second tooling die comprising a plurality of stacked metal sheets, a plurality of air gaps defined between adjacent stacked metal sheets;
heating the thermoset composite charge within the die cavity to a forming temperature using a second smart susceptor material within the die cavity;
moving the thermoset composite charge within the die cavity towards a first smart susceptor surface connected to the first tooling die after heating the thermoset composite charge to the forming temperature;
applying pressure to the thermoset composite charge using a flexible membrane to conform the thermoset composite charge to the first smart susceptor surface; and
heating the thermoset composite charge to a curing temperature using the first smart susceptor surface.

2. The method of claim 1 further comprising:
cooling portions of the first smart susceptor surface to below a first Curie temperature of the first smart susceptor surface.

3. The method of claim 1 , wherein heating the thermoset composite charge to the forming temperature comprises heating the thermoset composite charge using a conformable smart susceptor blanket positioned within the die cavity, wherein the conformable smart susceptor blanket comprises the second smart susceptor material.

4. The method of claim 3 , wherein moving the thermoset composite charge within the die cavity comprises increasing a pressure between the conformable smart susceptor blanket and a second smart susceptor surface connected to the second tooling die, wherein the conformable smart susceptor blanket comprises the flexible membrane.

5. The method of claim 3 further comprising:
cooling the thermoset composite charge in a controlled fashion by simultaneously cooling the first smart susceptor surface using cooling medium flowing through the plurality of air gaps of the first tooling die and applying heat from the conformable smart susceptor blanket.

6. The method of claim 3 , wherein heating the thermoset composite charge to the forming temperature comprises generating a second frequency range using a second plurality of conductors in the conformable smart susceptor blanket.

7. The method of claim 6 , wherein heating the thermoset composite charge to the curing temperature comprises generating a first frequency range using a first plurality of conductors, wherein a first smart susceptor material of the first smart susceptor surface is configured to be heated by the first frequency range, and wherein the first frequency range is separate from the second frequency range.

8. The method of claim 1 , wherein heating the thermoset composite charge within the die cavity to the forming temperature using the second smart susceptor material comprises:
heating a first side of the thermoset composite charge using the second smart susceptor material; and
heating the die cavity using the first smart susceptor surface.

9. The method of claim 1 , wherein the second smart susceptor material has a second Curie temperature different from a first Curie temperature of a first smart susceptor material of the first smart susceptor surface.

10. The method of claim 9 , wherein the first Curie temperature is higher than the second Curie temperature.

11. A method comprising:
placing a thermoset composite charge within a die cavity of an induction tool, wherein the induction tool comprises a first tooling die and a second tooling die movable with respect to each other, and wherein the first tooling die and the second tooling die form the die cavity, the first tooling die and the second tooling die comprising a plurality of stacked metal sheets, a plurality of air gaps defined between adjacent stacked metal sheets, a first set of conductors, a first smart susceptor surface connected to the first tooling die, and second smart susceptor surface connected to the second tooling die;
heating the thermoset composite charge within the die cavity to a forming temperature using a conformable smart susceptor blanket comprising a second smart susceptor material positioned within the die cavity;
moving the thermoset composite charge within the die cavity towards a first smart susceptor surface connected to the first tooling die after heating the thermoset composite charge to the forming temperature;
applying pressure to the thermoset composite charge using a flexible membrane to conform the thermoset composite charge to the first smart susceptor surface; and
heating the thermoset composite charge to a curing temperature using the first smart susceptor surface.

12. The method of claim 11 further comprising:
cooling portions of the first smart susceptor surface to below a first Curie temperature of the first smart susceptor surface.

13. The method of claim 11 , wherein moving the thermoset composite charge within the die cavity comprises increasing a pressure between the conformable smart susceptor blanket and a second smart susceptor surface connected to the second tooling die, wherein the conformable smart susceptor blanket comprises the flexible membrane.

14. The method of claim 11 further comprising:
cooling the thermoset composite charge in a controlled fashion by simultaneously cooling the first smart susceptor surface using cooling medium flowing through the plurality of air gaps of the first tooling die and applying heat from the conformable smart susceptor blanket.

15. The method of claim 11 , wherein heating the thermoset composite charge to the forming temperature comprises generating a second frequency range using a second plurality of conductors in the conformable smart susceptor blanket.

16. The method of claim 15 , wherein heating the thermoset composite charge to the curing temperature comprises generating a first frequency range using a first plurality of conductors, wherein a first smart susceptor material of the first smart susceptor surface is configured to be heated by the first frequency range, and wherein the first frequency range is separate from the second frequency range.

17. A method comprising:
placing a thermoset composite charge within a die cavity of an induction tool, wherein the induction tool comprises a first tooling die and a second tooling die movable with respect to each other, and wherein the first tooling die and the second tooling die form the die cavity, the first tooling die and the second tooling die comprising a plurality of stacked metal sheets, a plurality of air gaps defined between adjacent stacked metal sheets;
forming a first pressure region between a first smart susceptor surface of the induction tool and a vacuum film;
forming a second pressure region between the vacuum film and a conformable smart susceptor blanket, wherein the thermoset composite charge is within the second pressure region;
forming a third pressure region between the conformable smart susceptor blanket and a second smart susceptor surface of the induction tool;
heating the thermoset composite charge within the die cavity to a forming temperature using the conformable smart susceptor blanket, wherein the conformable smart susceptor blanket comprises a second smart susceptor material having a second Curie temperature;
forming the thermoset composite charge to the first smart susceptor surface; and
heating

Assignees

• Boeing Co

Inventors

• Matsen Marc R
• Luchini Timothy J
• Voss Bret A
• Hottes Christopher J

Classifications

• B29C70/44 Primary

  using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding · CPC title

• B29C2035/0816

  using eddy currents · CPC title

• B29C35/0805

  using electromagnetic radiation · CPC title

• B30B5/02

  wherein the pressing means is in the form of a flexible element, e.g. diaphragm, urged by fluid pressure · CPC title

• B29C2035/0811

  using induction · CPC title