IP Library Granted Patent US 8,460,502
Granted Patent B2
US 8,460,502 · App. 13/086,618 · Granted Jun 11, 2013

Method and tooling for manufacture of co-cured composite structures

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Quick Facts
Patent No.
US 8,460,502
App. No.
13/086,618
Granted
Jun 11, 2013
Kind
B2
Abstract

A method and part forming apparatus configured for forming an aircraft stringer. The part forming apparatus may comprise a forming tool, a rigid plate, and a hollow bladder. The forming tool may comprise a material trough, a bladder extension trough laterally aligned with and open to the material trough, and a recessed pocket extending from either side of the bladder extension trough and adjacent to the material trough. The method comprises placing composite material into the material trough, placing the bladder onto the composite material and through the bladder extension trough, placing the rigid plate into the recessed pocket and over the bladder, and then placing skin laminate over the bladder and the composite material. Once each of these components is in place, the forming tool may be vacuum bagged and the composite material and skin laminate may be co-cured to form the stringer.

Claims (32)

1. A method of forming a hollow, elongated part, the method comprising:

placing a composite material onto a forming tool within a material trough formed in the forming tool;

placing a hollow, flexible bladder over the composite material such that the bladder extends through the material trough and into an adjacent bladder extension trough formed in the forming tool and laterally aligned with the material trough;

placing a rigid plate onto the forming tool, over the bladder at or proximate to an end of the material trough;

placing a skin laminate over the composite material, at least a portion of the bladder, and at least a portion of the rigid plate;

sealing a flexible, impermeable sheet of material to the forming tool, such that the impermeable sheet extends over the skin laminate and cooperatively forms an air tight pocket with at least one of the forming tool and the bladder;

removing atmosphere from between the impermeable sheet and at least one of the forming tool and the bladder, thereby compressing the composite material and skin laminate;

co-curing the composite material and the skin laminate together via heat and pressure, thereby forming the hollow, elongated part; and

removing the skin laminate from the rigid plate.

2. The method of claim 1 , wherein the hollow, elongated part is a stringer.

3. The method of claim 1 , wherein placing the rigid plate onto the forming tool comprises placing the rigid plate into a recessed pocket of the forming tool, the recessed pocket being sized and shaped such that a top surface of the rigid plate rests flush with the composite material when the rigid plate is placed into the recessed pocket.

4. The method of claim 1 , wherein at least one of a width and a depth of the bladder extension trough gradually increases along a length of the bladder extension trough such that at least one of the width and the depth of the bladder extension trough is smaller at a location immediately adjacent to the material trough than at a location spaced lengthwise apart from the material trough.

5. The method of claim 3 , wherein the bladder extension trough comprises opposing side walls, wherein the recessed pocket comprises a first portion and a second portion, each positioned to border and open into the opposing side walls of the bladder extension trough.

6. The method of claim 5 , wherein the material trough comprises a bottom wall, two side walls extending upward from the bottom wall, and two flange recesses extending outward from the side walls, wherein the first and second portions of the recessed pocket substantially boarder the flange recesses of the material trough.

7. The method of claim 3 , wherein the rigid plate comprises a middle portion configured to extend over the bladder extension trough and two side portions configured to mate with and nestle into the recessed pocket, wherein the middle portion of the rigid plate has a thickness that gradually increases in a direction away from the material trough such that the middle portion is thinner at a first location of the rigid plate adjacent to the material trough than at a second location of the rigid plate spaced a distance apart from the material trough.

8. The method of claim 7 , wherein the side portions of the rigid plate each have a uniform thickness.

9. The method of claim 1 , wherein the impermeable sheet is a vacuum bag.

10. The method of claim 1 , wherein the bladder comprises at least one vent opening therein, located in or proximate to the bladder extension trough.

11. A method of forming a hollow stringer, the method comprising:

placing a composite material onto a forming tool within a material trough formed in the forming tool;

placing a hollow, flexible bladder over the composite material such that the bladder extends through the material trough and into an adjacent bladder extension trough formed in the forming tool and laterally aligned with the material trough;

placing a rigid plate onto a recessed pocket of the forming tool, such that the rigid plate extends over the bladder at or proximate to an end of the material trough;

placing a skin laminate over the composite material, at least a portion of the bladder, and at least a portion of the rigid plate;

sealing a vacuum bag to the forming tool, such that the vacuum bag extends over the skin laminate and cooperatively forms an air tight pocket with at least one of the forming tool and the bladder;

removing atmosphere from between the vacuum bag and at least one of the forming tool and the bladder, thereby compressing the composite material and skin laminate;

co-curing the composite material and the skin laminate together via heat and pressure, thereby forming the hollow, elongated part; and

removing the skin laminate from the rigid plate.

12. The method of claim 11 , further comprising cutting off a portion of the skin laminate after cure along a cutter groove formed into the rigid plate, wherein the cutter groove is formed into the rigid plate prior to placing a skin laminate over the composite material, at least a portion of the bladder, and at least a portion of the rigid plate.

13. The method of claim 12 , wherein the cutter groove is filled with sacrificial material.

14. The method of claim 1 , wherein the bladder extension trough comprises opposing side walls spaced apart from each other, wherein a distance between the opposing side walls of the bladder extension trough gradually widens along a length of the bladder extension trough.

15. The method of claim 1 , wherein the bladder extension trough has a variable depth that gradually deepens along a length of the bladder extension trough.

16. The method of claim 3 , wherein the rigid plate comprises a middle portion configured to extend over the bladder extension trough and two side portions configured to mate with and nestle into the recessed pocket, wherein the middle portion of the rigid plate has a thickness that tapers in a direction toward the material trough.

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 →
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 →
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 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: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 053993/0569 →
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: BANK OF AMERICA, N.A.
Reel/Frame 053983/0350 →
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 Apr 14, 2011
From: BERGMANN, BLAISE F.; SPAULDING, DWIGHT D.; MCPHERSON, JOHN P.
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 026126/0279 →