IP Library Granted Patent US 8,377,248
Granted Patent B2
US 8,377,248 · App. 12/816,568 · Granted Feb 19, 2013

Method and system for forming a complex monolithic thermoset part

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Quick Facts
Patent No.
US 8,377,248
App. No.
12/816,568
Granted
Feb 19, 2013
Kind
B2
Abstract

A system and method for forming a hollow, complex, monolithic composite part. Composite material may be placed around the mandrel, then an internal impermeable membrane may be placed into and/or through tunnels formed in the mandrel. Next, an external impermeable membrane may be placed around the composite material and sealed against itself and the internal impermeable membrane such that the mandrel and the composite material are both contained in an airtight manner between the internal and external impermeable membranes. Air may then be removed from within the sealed impermeable membranes, compressing the impermeable membranes against the mandrel and/or the composite material. The consolidated composite material may be hardened to form the composite part. Finally, the impermeable membrane may be removed from around the hollow composite part and from within the mandrel, followed by removal of the mandrel from within the composite part by breaking it up into smaller pieces.

Claims (32)

1. A method of forming a composite part having an external surface and an internal surface, the method comprising:

placing composite material around a mandrel having a hollow inner area;

inserting an internal impermeable membrane into the hollow inner area of the mandrel;

placing an external impermeable membrane around at least a portion of the composite material;

sealing portions of the internal impermeable membrane to portions of the external impermeable membrane forming an airtight envelope around the mandrel and the composite material;

removing air from between the internal impermeable membrane and the external impermeable membrane such that the internal and external impermeable membrane compress the mandrel and composite material toward each other;

heating the mandrel, the composite material, and the impermeable membranes to cure the composite material, thereby forming the composite part; and

removing the internal and external impermeable membranes and the mandrel from the composite part.

2. The method of claim 1 , wherein the mandrel has a monolithic, complex, trapped geometry.

3. The method of claim 1 , wherein the mandrel has a monolithic grid or monolithic crossed-beam configuration.

4. The method of claim 1 , wherein the mandrel is fragmented and removed from within the composite part by media blast, thermal shock, mechanical shock, or differential positive air pressure.

5. The method of claim 1 , wherein the mandrel is made of a solidified formable media.

6. The method of claim 5 , wherein the formable media is at least one of urethane, ceramic, carbon-carbon, coal-carbon, carbon foam, any liquid-reacting expanding foam filler, borosilicate glass, injectable expanding polyurethane foam, thermally transitive materials, eutectic salts, cured silicones, differential coefficient of thermal expansion metals, and composites.

7. The method of claim 5 , wherein the hollow inner area of the mandrel includes a plurality of intersecting tube-shaped channels forming a grid or crossed-beam configuration.

8. The method of claim 5 , further comprising placing a protective membrane against an outer surface of the mandrel prior to placing composite material around the mandrel, wherein the protective membrane is between the mandrel and the composite material.

9. The method of claim 8 , further comprising dividing the protective membrane into a plurality of sections for ease of removal from within the composite part and removing the protective membrane from the composite part after the mandrel is removed therefrom.

10. The method of claim 8 , wherein the protective membrane is a hardened protective membrane, wherein the combined size and shape of the mandrel and the protective membrane placed on the mandrel corresponds with the size and shape of the internal surface of the composite part.

11. A method of forming a composite part having an external surface and an internal surface, the method comprising:

forming a mandrel made of solidified formable media having a hollow inner area with at least two open ends within a hardened protective membrane, such that the protective membrane rests against an outer surface of the mandrel, wherein the combined size and shape of the mandrel and the protective membrane placed on the mandrel corresponds with the size and shape of the internal surface of the composite part;

placing composite material around the protective membrane;

inserting an internal impermeable membrane into the hollow inner area of the mandrel;

placing an external impermeable membrane around the composite material;

sealing end portions of the internal impermeable membrane to the external impermeable membrane;

removing air from between the internal and external impermeable membranes;

heating the mandrel, protective membrane, composite material, internal impermeable membrane, and external impermeable membrane to cure the composite material, changing the composite material into the composite part; and

removing the external impermeable membrane, the internal impermeable membrane, the mandrel, and the protective membrane from the composite part.

12. The method of claim 11 , wherein the mandrel has a trapped geometry.

13. The method of claim 11 wherein at least a portion of the mandrel is shaped as at least one of a monolithic lattice, a monolithic grid, a monolithic crossed-beam configuration, and a monolithic complex contoured shape.

14. The method of claim 11 , further comprising the step of dividing the protective membrane into a plurality of sections for ease of removal from within the composite part.

15. The method of claim 11 , wherein the formable media is at least one of urethane, ceramic, carbon-carbon, coal-carbon, carbon foam, any liquid-reacting expanding foam filler, borosilicate glass, injectable expanding polyurethane foam, thermally transitive materials, eutectic salts, cured silicones, differential coefficient of thermal expansion metals, and composites.

16. The method of claim 11 , wherein the mandrel is fragmented and removed from within the composite part by media blast, thermal shock, mechanical shock, or differential positive air pressure coupled with vacuum.

17. The method of claim 11 , wherein the hollow inner area of the mandrel includes a plurality of intersecting tube-shaped channels forming a grid or crossed-beam configuration.

Assignments (17)
RELEASE OF SECURITY INTEREST Recorded Dec 11, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073932/0669 →
RELEASE OF SECURITY INTEREST Recorded Dec 10, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073900/0356 →
RELEASE OF SECURITY INTEREST Recorded Dec 9, 2025
From: MORGAN STANLEY SENIOR FUNDING, INC., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073916/0346 →
SECURITY AGREEMENT Recorded Jul 8, 2024
From: SPIRIT AEROSYSTEMS, INC.
To: MORGAN STANLEY SENIOR FUNDING, INC.
Reel/Frame 068217/0456 →
RELEASE OF SECURITY INTEREST Recorded Dec 4, 2023
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
To: SPIRIT AEROSYSTEMS, INC.; SPIRIT AEROSYSTEMS HOLDINGS, INC.; SPIRIT AEROSYSTEMS NORTH CAROLINA, INC.
Reel/Frame 065772/0456 →
SECURITY AGREEMENT (SECOND LIEN NOTES) Recorded Nov 21, 2023
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
Reel/Frame 065659/0585 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Nov 23, 2022
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 061993/0847 →
RELEASE OF SECURITY INTEREST Recorded Nov 23, 2022
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 061995/0281 →
RELEASE OF SECURITY INTEREST Recorded Oct 28, 2020
From: BANK OF AMERICA, N.A.
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 054230/0578 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 053983/0350 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 053993/0505 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 053993/0569 →
SECURITY INTEREST Recorded Apr 17, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 052433/0843 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Feb 24, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
Reel/Frame 052004/0929 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded May 2, 2016
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 038592/0181 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Apr 19, 2012
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
Reel/Frame 028072/0647 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 16, 2010
From: COLEMAN, ROBERT ALEXANDER; KING, TIMOTHY DEAN; HANSON, STEVEN FILLMORE; BACA, LEONARD LLOYD
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 024543/0823 →