Remote detection of induction weld temperature

Patent metadata

Field	Value
Publication number	US-11235538-B2
Application number	US-202016986739-A
Country	US
Kind code	B2
Filing date	Aug 6, 2020
Priority date	Aug 6, 2019
Publication date	Feb 1, 2022
Grant date	Feb 1, 2022

Abstract

Systems and methods are provided for controlling welding. One embodiment is a method for controlling welding of a composite part. The method includes locating a linear fiber optic sensor along a composite part comprising a matrix of thermoplastic reinforced by fibers, measuring temperatures along the weld line via the linear fiber optic sensor, performing induction welding at the composite part along the weld line, determining a continuum of weld temperatures along the weld line, and controlling the induction welding based on the continuum of weld temperatures.

First claim

What is claimed is:

1. A method for controlling welding of a composite part, the method comprising:
locating a linear fiber optic sensor along a composite part comprising a matrix of thermoplastic reinforced by fibers;
measuring temperatures along a weld line via the linear fiber optic sensor;
performing induction welding at the composite part along the weld line;
determining a continuum of weld temperatures along the weld line; and
controlling the induction welding based on the continuum of weld temperatures,
wherein determining the continuum of weld temperatures along the weld line comprises:
determining sensor temperatures along the linear fiber optic sensor based on differences between a reference optical frequency shift and a weld optical frequency shift for each of multiple elements of the linear fiber optic sensor; and
determining a weld temperature from each sensor temperature, based on a known relationship between sensor temperatures and welding temperatures, and

wherein the known relationship is based on a material that the composite part is made from, a thickness of the composite part, a fiber orientation within the composite part, and a distance of the linear fiber optic sensor to the weld line.

2. The method of claim 1 wherein:
measuring the temperatures comprises measuring reference optical frequency shifts for a laser travelling from an end of the linear fiber optic sensor to elements within the linear fiber optic sensor before the induction welding is performed.

3. The method of claim 1 wherein:
induction welding along a line parallel to the linear fiber optic sensor.

4. The method of any of claim 1 wherein:
measuring temperatures along the weld line via the linear fiber optic sensor comprises measuring weld optical frequency shifts for a laser travelling from an end of the linear fiber optic sensor to elements within the linear fiber optic sensor while the induction welding is being performed.

5. The method of claim 4 wherein:
measuring the temperatures comprises measuring reference optical frequency shifts for a laser travelling from an end of the linear fiber optic sensor to elements within the linear fiber optic sensor before the induction welding is performed and
measuring temperatures is based on differences between reference optical frequency shifts and weld optical frequency shifts for elements of the linear fiber optic sensor.

6. The method of claim 1 wherein:
determining the continuum of weld temperatures along the weld line comprises determining a weld temperature at each of multiple locations that are separated by less than one millimeter from each other.

7. The method of claim 1 further comprising:
shielding elements of the linear fiber optic sensor from physical strain while performing the induction welding.

8. The method of claim 1 wherein:
the linear fiber optic sensor is disposed within the composite part.

9. A portion of an aircraft assembled according to the method of claim 1 .

10. The method of claim 1 , further comprising inferring a welding temperature at a weld interface based on a difference between a measured magnetic field strength and a threshold magnetic field strength during induction welding.

11. An apparatus for facilitating welding of a composite part, the apparatus comprising:
an end effector that generates an electromagnetic field which causes a weld line of a composite part to generate heat resulting in induction welding;
a linear fiber optic sensor disposed at the composite part along the weld line; and
a controller that measures temperatures along the weld line via the linear fiber optic sensor, determines a continuum of weld temperatures along the weld line, and controls the induction welding based on the continuum of weld temperatures,
wherein determines the continuum of weld temperatures along the weld line comprises:
determines sensor temperatures along the linear fiber optic sensor based on differences between a reference optical frequency shift and a weld optical frequency shift for each of multiple elements of the linear fiber optic sensor, and
determines a weld temperature from each sensor temperature based on a known relationship between sensor temperatures and welding temperatures, and

wherein the known relationship is based on a material that the composite part is made from, a thickness of the composite part, a fiber orientation within the composite part, and a distance of the linear fiber optic sensor to the weld line.

12. The apparatus of claim 11 wherein:
the controller determines the continuum of weld temperatures along the weld line by determining a weld temperature at each of multiple locations that are separated by less than one millimeter from each other.

13. The apparatus of claim 11 further comprising:
a cover that surrounds and shields elements of the linear fiber optic sensor from physical strain during the induction welding.

14. The apparatus of claim 11 wherein:
the weld line follows a contour, and the linear fiber optic sensor conforms to the contour.

15. The apparatus of claim 11 wherein:
the linear fiber optic sensor is disposed within the composite part.

16. The apparatus of claim 11 , further comprising a sensor to infer a welding temperature at a weld interface based on a difference between a measured magnetic field strength and a threshold magnetic field strength during induction welding.

17. A method for controlling welding of a composite part, the method comprising:
locating a linear fiber optic sensor along a composite part comprising a matrix of thermoplastic reinforced by fibers;
measuring reference optical frequency shifts for a laser travelling from an end of the linear fiber optic sensor to elements within the linear fiber optic sensor before induction welding;
performing induction welding at the composite part along a weld line;
measuring reference optical frequency shifts for a laser travelling from an end of the linear fiber optic sensor to elements within the linear fiber optic sensor during induction welding;
determining a continuum of weld temperatures along the weld line; and
controlling the induction welding based on the measured reference optical frequency shifts before and during induction welding,
wherein determining the continuum of weld temperatures along the weld line comprises:
determining sensor temperatures along the linear fiber optic sensor, based on differences between a reference optical frequency shift and a weld optical frequency shift for each of multiple elements of the linear fiber optic sensor, and
determining a weld temperature from each sensor temperature, based on a known relationship between sensor temperatures and welding temperatures, and

wherein the known relationship is based on a material that the composite part is made from, a thickness of the composite part, a fiber orientation within the composite part, and a distance of the linear fiber optic sensor to the weld line.

18. The method of claim 17 wherein:
determining a continuum of weld temperatures during induction welding based on the measured reference optical frequency shifts before and during induction welding.

19. The method of claim 17 wherein:
induction welding along a line parallel to the linear fiber optic sensor.

20. The method of claim 17 further comprising:
shielding elements of the linear fiber optic sensor from physical strain while performing the induction welding.

21. The method of claim 17 wherein:
determining the

Assignees

• Boeing Co

Inventors

• Buser Yannick Martijn
• Sachs Ulrich
• Alonso Pedro Pablo Martin
• Samalot Francis J
• Rubin Alexander

Classifications

• B29L2031/3076

  Aircrafts (blades, propellers B29L2031/08) · CPC title

• B29C65/3616

  comprising discontinuous fibre-reinforcements · CPC title

• B29C66/9121

  by measuring the temperature · CPC title

• G01K11/3206

  at discrete locations in the fibre, e.g. using Bragg scattering · CPC title

• B29C66/9192

  in explicit relation to another variable, e.g. temperature diagrams · CPC title