IP Library Granted Patent US 8,877,114
Granted Patent B2
US 8,877,114 · App. 13/238,879 · Granted Nov 4, 2014

Method for removing a SMP apparatus from a cured composite part

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Quick Facts
Patent No.
US 8,877,114
App. No.
13/238,879
Granted
Nov 4, 2014
Kind
B2
Abstract

A method and apparatus for removing a SMP apparatus from within a cured composite part. The method may comprise the steps of triggering the SMP apparatus from a rigid state to a malleable state, inducing a pressure differential that drives the SMP apparatus, in the malleable state, away from the cured composite part and toward an inner mandrel tool, and removing the inner mandrel tool with the SMP apparatus resting thereon out of the cured composite part. The inner mandrel tool may comprise an outer surface having varying contours such that a surface area of the outer surface is great enough to prevent the SMP apparatus from folding over onto itself or creasing when driven toward the inner mandrel tool. A maximum straight line distance between points on the outer surface may be small enough to allow the inner mandrel tool clearance for removal from the cured composite part.

Claims (44)

1. A method of removing a shape memory polymer (SMP) apparatus from within a cured composite part, the method comprising:

triggering the SMP apparatus from a rigid state to a malleable state;

inducing a pressure differential that drives the SMP apparatus, in the malleable state, away from the cured composite part and toward an inner mandrel tool, wherein the inner mandrel tool comprises:

an outer surface having varying contours such that a surface area of the outer surface is great enough to prevent the SMP apparatus from folding over onto itself or creasing when driven toward the inner mandrel tool, wherein a maximum straight line distance between points on the outer surface is small enough to allow the inner mandrel tool clearance for removal from the cured composite part; and

removing the inner mandrel tool with the SMP apparatus resting thereon out of the cured composite part.

2. The method of claim 1 , wherein the outer surface has holes formed therethrough, wherein the step of inducing a pressure differential comprises applying vacuum via the holes to drive the SMP apparatus, in its malleable state, toward the outer surface.

3. The method of claim 1 , wherein the step of inducing a pressure differential comprises forcing air or gas through ports formed in a rigid external tool to which the SMP apparatus is sealed.

4. The method of claim 2 , wherein the inner mandrel tool further comprises a pressurization system configured for forcing a pressurized gas through the holes for forming the SMP apparatus or consolidating the composite part during cure.

5. The method of claim 1 , wherein the varying contours comprise a plurality of protrusions and at least some of the protrusions are elongated, sinusoidal-shaped protrusions extending length-wise along the outer surface of the inner mandrel tool.

6. The method of claim 1 , wherein the varying contours are configured to provide at least one of axial and hoop strain to the SMP apparatus, in its malleable state, when the SMP apparatus is driven toward the inner mandrel tool.

7. The method of claim 1 , wherein the inner mandrel tool is substantially cylindrical, with a radius “r” and a length “L”, wherein a total surface area of the outer surface is greater than 2π*r*L, due to the varying contours of the outer surface.

8. The method of claim 1 , further comprising:

sealing peripheral portions of the SMP apparatus to end portions or peripheral portions of the inner mandrel tool; and

inflating the SMP apparatus in a direction away from the inner mandrel tool when the SMP apparatus is in the malleable state, prior to the step of inducing the pressure differential that drives the SMP apparatus toward the inner mandrel tool.

9. A method of removing a shape memory polymer (SMP) apparatus from within a cured composite part, the method comprising:

triggering the SMP apparatus from a rigid state to a malleable state;

inducing a pressure differential that urges the SMP apparatus away from an inner mandrel tool when the SMP apparatus is in the malleable state;

triggering the SMP apparatus from the malleable state to the rigid state;

applying composite material onto the SMP apparatus in the rigid state;

curing the composite material into the cured composite part;

inducing a pressure differential that drives the SMP apparatus, in the malleable state, away from the cured composite part and toward the inner mandrel tool, wherein the inner mandrel tool comprises:

a wall with an outer surface and an inner surface, wherein the outer surface comprises varying contours, such that a surface area of the outer surface is great enough to prevent the SMP apparatus from folding over onto itself or creasing when driven toward the inner mandrel tool, wherein a maximum cross-sectional area of the wall is small enough to allow the inner mandrel tool clearance for removal from the cured composite part; and

removing the inner mandrel tool with the SMP apparatus resting thereon out of the cured composite part.

10. The method of claim 9 , wherein the wall has holes formed therethrough, wherein the step of inducing a pressure differential comprises applying vacuum via the holes of the wall to drive the SMP apparatus, in its malleable state, toward the outer surface of the wall.

11. The method of claim 9 , wherein the step of inducing a pressure differential comprises forcing air or gas through ports formed in a rigid external tool to which the SMP apparatus is sealed.

12. The method of claim 10 , wherein the inner mandrel tool further comprises a pressurization system configured for forcing a pressurized gas through the holes in the wall.

13. The method of claim 9 , wherein at least some of the varying contours are elongated, sinusoidal-shaped protrusions extending length-wise along the outer surface of the wall.

14. The method of claim 9 , wherein the varying contours are configured to provide at least one of axial and hoop strain to the SMP apparatus, in its malleable state, when the SMP apparatus is driven toward the inner mandrel tool.

15. The method of claim 9 , wherein the wall is substantially cylindrical, with a radius “r” and a length “L”, wherein a total surface area of the outer surface is greater than 2π*r*L, due to the protrusions extending from the outer surface.

16. The method of claim 9 , further comprising:

sealing peripheral portions of the SMP apparatus to end portions or peripheral portions of the inner mandrel tool prior to the step of inflating the SMP apparatus.

17. A method of removing a shape memory polymer (SMP) apparatus from within a cured composite part, the method comprising:

triggering the SMP apparatus from a rigid state to a malleable state;

inducing a pressure differential that drives the SMP apparatus, in the malleable state, away from the cured composite part and toward an inner mandrel tool, wherein the inner mandrel tool comprises:

an outer surface having varying contours such that a surface area of the outer surface is great enough to prevent the SMP apparatus from folding over onto itself or creasing when driven toward the inner mandrel tool, wherein a maximum straight line distance between points on the outer surface is small enough to allow the inner mandrel tool clearance for removal from the cured composite part, wherein the varying contours comprise protrusions, wherein at least some of the protrusions are elongated, sinusoidal-shaped protrusions having a staggered configuration relative to each other and extending length-wise along the outer surface of the inner mandrel tool; and

removing the inner mandrel tool with the SMP apparatus resting thereon out of the cured composite part.

18. The method of claim 17 , wherein the outer surface has holes formed therethrough, wherein the step of inducing a pressure differential comprises applying vacuum via the holes to drive the SMP apparatus, in its malleable state, toward the outer surface.

19. The method of claim 17 , wherein the step of inducing a pressure differential comprises forcing air or gas through ports formed in a rigid external tool to which the SMP apparatus is sealed.

20. The method of claim 18 , wherein the inner mandrel tool further comprises a pressurization system configured for forcing a pressurized gas through the holes for forming the SMP apparatus or consolidating the composite part during cure.

21. The method of claim 17 , wherein the varying contours are configured to provide at least one of axial and hoop strain to the SMP apparatus, in its malleable state, when the SMP apparatus is driven toward the inner mandrel tool.

22. The method of claim 17 , wherein the inner mandrel tool is substantially cylindrical, with a radius “r” and a length “L”, wherein a total surface area of the outer surface is greater than 2π*r*L, due to the varying contours of the outer surface.

23. The method of claim 17 , further comprising:

sealing peripheral portions of the SMP apparatus to end portions or peripheral portions of the inner mandrel tool; and

inflating the SMP apparatus in a direction away from the inner mandrel tool when the SMP apparatus is in the malleable state, prior to the step of inducing the pressure differential that drives the SMP apparatus toward the inner mandrel tool.

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 Sep 21, 2011
From: HAVENS, DAVID E.; EVERHART, MATTHEW C.; CABLE, KRISTIN MARIE; TRAXLER, ERIC W.; FIEGENBAUM, CARL RAY; PRIEST, JEFFREY W.; CASTER, KODI ELIZABETH ANN
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 026943/0503 →