IP Library Granted Patent US 11,708,143
Granted Patent B2
US 11,708,143 · App. 17/668,954 · Granted Jul 25, 2023

Method and apparatus for fabricating reformable stiffening elements

Inventor: Mark Anthony Wadsworth (Sedan, KS)
Assignee: Spirit AeroSystems, Inc.
B64C1/064B29B11/06B29C70/44B64F5/10B29L2031/3082
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Quick Facts
Patent No.
US 11,708,143
App. No.
17/668,954
Granted
Jul 25, 2023
Kind
B2
Abstract

A stiffening element comprises a tension and compression member, a shear member, an attachment member, and a plurality of beads. The tension and compression member is positioned spaced apart from the skin and configured to bear tension or compression forces that stiffen the skin and prevent the skin from buckling or bending. The shear member is connected to the tension and compression member and configured to bear shear forces between the skin and the tension and compression member. The attachment member is connected to the shear member and is configured to connect to the skin. The beads each create out-of-plane feature that is positioned in at least one of the shear member and the attachment member. The beads permit the stiffening element be reshaped to adjust a longitudinal curvature of the stiffening element.

Claims (63)

1. A method of adjusting a longitudinal curvature of a stiffening element to be attached to a skin of aircraft components for providing structural reinforcement, the method comprising:

applying a force to at least a portion of the stiffening element to induce a change in the longitudinal curvature of the stiffening element;

wherein the stiffening element comprises:

a tension and compression member positioned spaced apart from the skin and configured to bear tension or compression forces that stiffen the skin and prevent the skin from buckling or bending,

a shear member connected to the tension and compression member and configured to bear shear forces between the skin and the tension and compression member,

an attachment member connected to the shear member and configured to connect to the skin, and

a plurality of beads, each bead creating an out-of-plane feature that is positioned in at least one of the shear member and the attachment member, at least one of the beads configured to be reshaped; and

wherein application of the force reshapes at least one of the plurality of beads to adjust the longitudinal curvature of the stiffening element.

2. The method of claim 1 , further comprising:

heating the stiffening element to a temperature above the glass transition temperature for the stiffening element material; and

reducing or removing the heat after a time period.

3. The method of claim 2 , wherein reshaping the bead further comprises applying a clamping force to the bead with a clamp, wherein the clamp comprises:

an upper clamp member contacting at least a portion of a first surface of the bead,

a lower clamp member contacting at least a portion of a second, opposing surface of the bead, and

a plurality of resilient members which urge the upper clamp member to apply pressure on the stiffening element toward the lower clamp member.

4. The method of claim 3 , further comprising flattening or enhancing the bead to adjust the longitudinal curvature of the stiffening element, and wherein

the upper clamp member includes at least one wall with a contact surface that contacts at least a portion of the first surface of the bead and the contact surface includes a first feature to flatten the bead or a second feature to enhance the bead, and

the lower clamp member includes at least one wall with a contact surface that contacts at least a portion of the second surface of the bead and the contact surface includes a first feature to flatten the bead or a second feature to enhance the bead.

5. The method of claim 4 , further comprising flattening the bead, and wherein

the first feature of the contact surface of the upper clamp member includes a recess that has a depth smaller than a height of the bead, and

the first feature of the contact surface of the lower clamp member includes a protrusion that has a height smaller than a depth of the bead.

6. The method of claim 4 , further comprising enhancing the bead, and wherein

the second feature of the contact surface of the upper clamp member includes a recess that receives the bead, and

the second feature of the contact surface of the lower clamp member includes a protrusion that has a height greater than a depth of the bead.

7. The method of claim 4 , further comprising flattening the bead, and wherein

the first feature of the contact surface of the upper clamp member includes a protrusion that has a height smaller than a depth of the bead, and

the first feature of the contact surface of the lower clamp member includes a recess that has a depth smaller than a height of the bead.

8. The method of claim 4 , further comprising enhancing the bead, and wherein

the second feature of the contact surface of the upper clamp member includes a protrusion that has a height greater than a depth of the bead, and

the second feature of the contact surface of the lower clamp member includes a recess that receives the bead.

9. The method of claim 2 , wherein

the shear member includes a first shear member connected to a first edge of the attachment member and a second shear member connected to a second edge of the attachment member; and

the tension and compression member includes a first tension and compression member connected to the first shear member and a second tension and compression member connected to the second shear member, and

wherein beads are formed in the attachment member with each bead starting near an edge of the first shear member adjacent to the first tension and compression member, extending in a transverse direction across the first shear member, extending into and across the entire width of the attachment member, extending in a transverse direction across the second shear member, and ending near an edge of the second shear member adjacent to the second tension and compression member.

10. The method of claim 2 , wherein

the shear member includes a first shear member connected to a first edge of the tension and compression member, and a second shear member connected to a second edge of the tension and compression member;

the attachment member includes a first attachment member connected to the first shear member, and a second attachment member connected to the second shear member; and

wherein beads are formed in each of the first and second attachment members.

11. The method of claim 1 , wherein each bead has an arch or roughly parabolic cross-sectional shape.

12. The method of claim 1 , further comprising:

attaching a first clamp to the stiffening element adjacent to a first side of one of the beads;

attaching a second clamp to the stiffening element adjacent to a second side of the bead;

connecting a resilient member between the first clamp and the second clamp;

heating the stiffening element to a temperature above the glass transition temperature for the stiffening element material;

reducing or removing the heat after a time period; and

wherein the application of force comprises the resilient member applying either tension to draw the first and second clamps together, or compression to push the first and second clamps apart, to reshape the bead to adjust the longitudinal curvature of the stiffener.

13. The method of claim 12 , further comprising limiting the movement of the first clamp relative to the second clamp to control the adjustment of the longitudinal curvature of the stiffener, wherein

the first clamp includes a first limit block extending from the first clamp toward the bead, and

the second clamp includes a second limit block extending from the second clamp toward the bead.

14. The method of claim 13 , wherein the resilient member is a spring, and the application of force comprises the spring pulling the first clamp and the second clamp toward one another until the first limit block contacts the second limit block.

15. The method of claim 13 , wherein the resilient member is a spring, and the application of force comprises the spring pushing the first clamp and the second clamp away from one another.

16. The method of claim 1 , further comprising:

placing an outer surface of the skin in contact with an upper surface of a tool;

placing the stiffening element in contact with an inner surface of the skin, wherein the attachment member contacts the skin;

applying a force to the stiffening element that presses the attachment member against the skin; and

attaching the stiffening element to the skin.

17. The method of claim 16 , further comprising:

placing a vacuum bag over the stiffening element and the skin,

sealing the vacuum bag against the upper surface of the tool, and

wherein applying the force to the stiffening element comprises applying a vacuum between the vacuum bag and the tool.

18. The method of claim 16 , further comprising:

heating the stiffening element to a temperature above the glass transition temperature for the stiffening element material; and

reducing or removing the heat after a time period.

Assignments (9)
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 →
RELEASE OF SECURITY INTEREST Recorded Dec 9, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073900/0653 →
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 065757/0004 →
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 →
SECURITY INTEREST Recorded Nov 23, 2022
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
Reel/Frame 061869/0241 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Nov 23, 2022
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
Reel/Frame 061993/0236 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 10, 2022
From: WADSWORTH, MARK ANTHONY
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 059010/0178 →
Continuity (2)
Division 16720491 · Dec 19, 2019
Related Publication 20220161916A1 · May 26, 2022