IP Library Granted Patent US 10,703,049
Granted Patent B2
US 10,703,049 · App. 16/013,420 · Granted Jul 7, 2020

System and method for welding thermoplastic components to create composite structure

Inventor: Mark Anthony Wadsworth (Sedan, KS)
Assignee: Spirit AeroSystems, Inc.
B29C65/2053B29C65/30B29C66/43B29C66/721B29C66/91231
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Quick Facts
Patent No.
US 10,703,049
App. No.
16/013,420
Granted
Jul 7, 2020
Kind
B2
Abstract

A system and method for welding thermoplastic components by positioning and moving a heated plate between the components to melt their respective faying surfaces, and as the plate moves, pressing the components together so that the melted faying surfaces bond together as they cool and re-solidify, thereby creating a composite structure. The plate has a heated portion which is positioned between and heated to melt a portion of the first and second faying surfaces. A manipulator mechanism moves the plate along an interface from between the portion to between a series of subsequent portions of the first and second faying surfaces, thereby welding the thermoplastic components along the entire interface to create the composite structure. The heated portion may contact the faying surfaces and melt them through conduction, or may be suspended between them and melt them through radiation and convection.

Claims (28)

1. A system for welding a first thermoplastic component to a second thermoplastic component along an interface to create a composite structure, the system comprising:

a plate element having a heated portion configured to be positioned between a portion of a first faying surface of the first thermoplastic component and a second faying surface of the second thermoplastic component, wherein the heated portion is configured to be heated to an operating temperature which is sufficient to melt the portion of the first and second faying surfaces; and

a manipulator mechanism configured to move the plate element along the interface from between the portion of the first and second faying surfaces, which then cool and bond together, to between a series of subsequent portions of the first and second faying surfaces, and thereby weld the first thermoplastic component to the second thermoplastic component along the interface to create the composite structure.

2. The system of claim 1 , wherein the heated portion the plate element has a thickness of between 0.01 inches and 0.03 inches.

3. The system of claim 1 , wherein the heated portion of the plate element is heated using joule heating.

4. The system of claim 1 , further including a first temperature sensor configured to determine the operating temperature of the plate element, and a second temperature sensor configured to determine an adjacent temperature of the first and second thermoplastic components.

5. The system of claim 1 , wherein at least the heated portion of the plate element is in physical contact with the first and second faying surfaces, and melts the first and second faying surfaces through conduction.

6. The system of claim 5 , wherein a front portion of the plate element has a rake angle to control any excess melted thermoplastic material from the first and second faying surfaces.

7. The system of claim 6 , wherein the rake angle is between 10 degrees and 50 degrees.

8. The system of claim 1 , wherein at least the heated portion of the plate element is suspended between and not in physical contact with the first and second faying surfaces, and melts the first and second faying surfaces through radiation and convection.

9. The system of claim 8 , further including a spacer element configured to create a gap between the first and second faying surfaces, wherein at least the heated portion of the plate element is located in the gap.

10. The system of claim 9 , wherein the spacer element is an unheated front portion of the plate element.

11. The system of claim 9 , wherein the spacer element includes one or more circular rollers.

12. The system of claim 8 , further including an air nozzle configured to introduce a stream of air between at least the heated portion of the plate element and the first and second faying surfaces so as to enhance convection.

13. The system of claim 8 , further including one or more holes in the plate element to enhance convection.

14. The system of claim 1 , the manipulator mechanism further including a guide roller configured to guide movement of the plate element along the interface between the first and second faying surfaces.

15. The system of claim 1 , the manipulator mechanism further including a pressure roller configured to press the first and second faying surfaces together behind the plate element as the plate element is moved along the interface.

16. The system of claim 1 , the manipulator mechanism further including a cooling nozzle configured to deliver a cooling fluid to accelerate cooling of the first and second faying surfaces behind the plate element as the plate element is moved along the interface.

17. The system of claim 1 , the manipulator mechanism further including an inert gas nozzle configured to deliver an inert gas to displace oxygen around the heated portion of the plate element.

18. The system of claim 1 , further including a support surface configured to be positioned behind the first thermoplastic component, wherein the support surface is flexible so as to accommodate a deflection of the first thermoplastic component as the plate element is moved between the first and second faying surfaces.

19. A system for welding a first thermoplastic component to a second thermoplastic component along an interface to create a composite structure, the system comprising:

a plate element having a heated portion configured to be positioned between a portion of a first faying surface of the first thermoplastic component and a second faying surface of the second thermoplastic component, wherein the heated portion is configured to be joule heated to an operating temperature which is sufficient to melt the portion of the first and second faying surfaces,

wherein at least the heated portion of the plate element is in physical contact with the portion of the first and second faying surfaces, and melts the portion of the first and second faying surfaces through conduction; and

a manipulator mechanism configured to move the plate element along the interface from between the portion of the first and second faying surfaces, which then cool and bond together, to between a series of subsequent portions of the first and second faying surfaces, and thereby weld the first thermoplastic component to the second thermoplastic component along the interface to create the composite structure.

20. A system for welding a first thermoplastic component to a second thermoplastic component along an interface to create a composite structure, the system comprising:

a plate element having a heated portion configured to be positioned between a portion of a first faying surface of the first thermoplastic component and a second faying surface of the second thermoplastic component, wherein the heated portion is configured to be joule heated to an operating temperature which is sufficient to melt the portion of the first and second faying surfaces,

wherein at least the heated portion of the plate element is suspended between and not in physical contact with the portion of the first and second faying surfaces, and melts the portion of the first and second faying surfaces through radiation and convection; and

a manipulator mechanism configured to move the plate element along the interface from between the portion of the first and second faying surfaces, which then cool and bond together, to between a series of subsequent portions of the first and second faying surfaces, and thereby weld the first thermoplastic component to the second thermoplastic component along the interface to create the composite structure.

Assignments (15)
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: 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 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 20, 2018
From: WADSWORTH, MARK ANTHONY
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 046147/0026 →
Cited By (1)
US 12,709,077