IP Library Patent Application 16663430
Patent Application
App. No. 16/663,430

SYSTEM AND METHOD FOR THERMOPLASTIC WELDING USING AN INDUCED THERMAL GRADIENT

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Patent No.
US None
App. No.
16/663,430
Abstract

A system and method for thermoplastic composite welding comprising a cooling means and a heat source. The cooling means cools a heat-side laminate so as to create a thermal gradient in the heat-side laminate. The heat source heats the heat-side laminate after the cooling step is initiated but before the thermal gradient dissipates so that a first side of the heat-side laminate closer to the heat source does not deform as faying surfaces of the heat-side laminate and another laminate farther away from the heat source are welded together.

Claims (34)

1 . A system for thermoplastic composite welding a heat-side laminate having opposing first and second sides and an opposing laminate having opposing first and second sides together, the system comprising:

a cooling means configured to cool the heat-side laminate so as to create a thermal gradient in the heat-side laminate; and

a welding shoe configured to heat the heat-side laminate after the heat-side laminate is cooled but before the thermal gradient dissipates so that the first side of the heat-side laminate does not deform as the second side of the heat-side laminate and the first side of the opposing laminate are welded together.

2 . The system of claim 1 , wherein the cooling means includes a perforated plenum configured to disperse cooled fluid to the first side of the heat-side laminate.

3 . The system of claim 1 , wherein the cooling means includes a heat sink configured to contact the first side of the heat-side laminate.

4 . The system of claim 1 , wherein the welding shoe comprises an induction coil configured to heat the heat-side laminate via a magnetic field.

5 . The system of claim 1 , wherein the welding shoe comprises an elastomeric pressure pad configured to press the heat-side laminate and the opposing laminate together.

6 . The system of claim 5 , wherein the cooling means is the elastomeric pressure pad, wherein the elastomeric pressure pad is configured to function as a heat sink.

7 . A method of thermoplastic composite welding, the method comprising the steps of:

placing a heat-side laminate having opposing first and second sides adjacent to an opposing laminate having first and second sides;

cooling the heat-side laminate so as to create a thermal gradient in the heat-side laminate; and

heating the heat-side laminate after the cooling step is initiated but before the thermal gradient dissipates so that the first side of the heat-side laminate does not deform as the second side of the heat-side laminate and the first side of the opposing laminate are welded together.

8 . The method of claim 7 , wherein the step of cooling the heat-side laminate includes at least one of immersing the first side of the heat-side laminate in a cold fluid, spraying the first side of the heat-side laminate with a cold fluid, positioning a cooled heat sink near the first side of the heat-side laminate, and subjecting the first side of the heat-side laminate to a convective cooling jet.

9 . The method of claim 7 , the method further comprising the step of applying pressure to at least one of the heat-side laminate and the opposing laminate.

10 . The method of claim 9 , wherein the pressure is applied via an elastomeric pressure pad.

11 . The method of claim 9 , wherein the pressure is applied via a pressure application means, the method further comprising the steps of cooling the pressure application means and cooling the heat-side laminate via the cooled pressure application means before heating the heat-side laminate.

12 . The method of claim 11 , wherein the step of cooling the pressure application means is performed before the step of applying pressure.

13 . The method of claim 10 , wherein the step of heating the heat-side laminate is performed via a welding shoe having the elastomeric pressure pad.

14 . The method of claim 10 , wherein the heat sink includes magnetic flux control material, the heating step including induction welding the second side of the heat-side laminate and the first side of the opposing laminate together, wherein the induction welding includes controlling magnetic fields via the magnetic flux control material.

15 . The method of claim 7 , wherein the induction welding includes exposing at least the heat-side laminate to high-frequency alternating magnetic fields to induce eddy current heating near the second side of the heat-side laminate and the first side of the opposing laminate.

16 . The method of claim 7 , wherein the step of cooling the heat-side laminate includes the step of passing cooled fluid through an internal passage in a heat sink adjacent to the heat-side laminate.

17 . A method of thermoplastic composite welding, the method comprising the steps of:

placing a heat-side laminate having opposing first and second sides adjacent to an opposing laminate having opposing first and second sides;

cooling an elastomeric pressure pad;

cooling the heat-side laminate via the cooled elastomeric pressure pad so as to create a thermal gradient in the heat-side laminate; and

heating the heat-side laminate via a welding shoe after the step of cooling the heat-side laminate is initiated but before the thermal gradient dissipates so that the first side of the heat-side laminate does not deform as the second side of the heat-side laminate and the first side of the opposing laminate are welded together.

18 . The method of claim 17 , wherein the welding shoe comprises the elastomeric pressure pad, the step of cooling the heat-side laminate including drawing heat from the heat-side laminate to the elastomeric pressure pad.

19 . The method of claim 17 , wherein the step of cooling the elastomeric pressure pad includes submersing at least a portion of the welding shoe in a cooled fluid.

20 . The method of claim 17 , wherein the welding shoe repeatedly alternates between cooling the heat-side laminate and heating the heat-side laminate.

21 . A method of thermoplastic composite welding, the method comprising the steps of:

placing a heat-side laminate having opposing first and second sides adjacent to an opposing laminate having first and second sides;

cooling the heat-side laminate via a cold fluid so as to create a thermal gradient in the heat-side laminate;

applying pressure to the heat-side laminate via an elastomeric pressure pad; and

heating the heat-side laminate via high-frequency alternating magnetic fields to induce eddy currents near the second side of the heat-side laminate and the first side of the opposing laminate after the cooling step is initiated but before the thermal gradient dissipates so that the first side of the heat-side laminate does not deform as the second side of the heat-side laminate and the first side of the opposing laminate are welded together.

Assignments (10)
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 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 →
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 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 Oct 25, 2019
From: WADSWORTH, MARK ANTHONY
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 050822/0945 →