IP Library Granted Patent US 8,079,276
Granted Patent B2
US 8,079,276 · App. 12/194,725 · Granted Dec 20, 2011

Dynamic calibration assembly for a friction stir welding machine

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Quick Facts
Patent No.
US 8,079,276
App. No.
12/194,725
Granted
Dec 20, 2011
Kind
B2
Abstract

A calibration assembly for a friction stir welding machine having a rotatable pin tool with upper and lower shoulders. The calibration assembly includes: a force measuring component for placement between the upper and lower shoulders of the pin tool; an upper bearing for placement between the upper shoulder of the pin tool and the force measuring component for permitting relative rotation therebetween; and a lower bearing for placement between the lower shoulder of the pin tool and the force measuring component for permitting relative rotation therebetween. The upper and lower bearings permit the pin tool to be rotated relative to the force measuring component during a calibration procedure. This permits the force measuring component to measure the forces directly applied by the pin tool while the upper and lower shoulders are either stationary or rotated relative to the force measuring component.

Claims (32)

1. A calibration assembly for a friction stir welding machine having a rotatable pin tool with upper and lower shoulders, the calibration assembly comprising:

a force measuring component for placement between the upper and lower shoulders of the pin tool, wherein the force measuring component measures a force applied by the pin tool while the upper and lower shoulders are either stationary relative to the force measuring component, rotated together relative to the force measuring component, or rotated independently relative to one another;

an upper bearing for placement between the upper shoulder of the pin tool and the force measuring component for permitting relative rotation therebetween; and

a lower bearing for placement between the lower shoulder of the pin tool and the force measuring component for permitting relative rotation therebetween.

2. The calibration assembly of claim 1 , wherein the force measuring component is a load cell that is held stationary relative to the upper and lower shoulders of the pin tool.

3. The calibration assembly of claim 2 , further comprising a control device for receiving electrical force signals from the load cell and for converting the electrical force signals into force measurements.

4. The calibration assembly of claim 3 , further comprising a display coupled with the control device for displaying data representative of the force measurements.

5. The calibration assembly of claim 1 , wherein the force measuring component includes two spaced-apart beam load cells held stationary relative to the upper and lower shoulders of the pin tool.

6. The calibration assembly of claim 1 , further comprising an upper spherical washer for placement between the upper bearing and the force measuring component.

7. The calibration assembly of claim 1 , further comprising a lower spherical washer for placement between the lower bearing and the force measuring component.

8. A calibration assembly for a friction stir welding machine having a rotatable pin tool with upper and lower shoulders, the calibration assembly comprising:

a force measuring component placed between the upper and lower shoulders of the pin tool and held in a fixed position;

an upper bearing placed between the upper shoulder of the pin tool and the force measuring component for permitting relative rotation therebetween;

a lower bearing placed between the lower shoulder of the pin tool and the force measuring component for permitting relative rotation therebetween;

a control device coupled with the force measuring component for calculating a force applied by the pin tool while the upper and lower shoulders are either stationary relative to the force measuring component, rotated together relative to the force measuring component, or rotated independently of one another.

9. The calibration assembly of claim 8 , wherein the force measuring component is a load cell held stationary relative to the upper and lower shoulders of the pin tool.

10. The calibration assembly of claim 8 , wherein the force measuring component includes two spaced-apart beam load cells held stationary relative to the upper and lower shoulders of the pin tool.

11. The calibration assembly of claim 8 , further comprising a display coupled with the control device for displaying data representative of the force measurements.

12. The calibration assembly of claim 8 , further comprising an upper spherical washer for placement between the upper bearing and the force measuring component.

13. The calibration assembly of claim 8 , further comprising a lower spherical washer for placement between the lower bearing and the force measuring component.

14. A method for dynamically calibrating a friction stir welding machine, the method comprising:

placing a force measuring component between upper and lower shoulders of a pin tool of the friction stir welding machine;

placing an upper bearing between the upper shoulder of the pin tool and the force measuring component;

placing a lower bearing between the lower shoulder of the pin tool and the force measuring component;

applying forge forces to the pin tool to move the upper and lower shoulders toward one another so as to sandwich the force measuring component and upper and lower bearings between the upper and lower shoulders;

rotating at least one of the upper and lower shoulders relative to the force measuring component; and

measuring at least one force with the force measuring component while the upper shoulder or lower shoulder is rotated relative to the force measuring component.

15. The method of claim 14 , wherein the force measuring component is a load cell that is held stationary relative to the upper and lower shoulders of the pin tool.

16. The method of claim 14 , further comprising the step of placing an upper spherical washer for placement between the upper bearing and the force measuring component.

17. The method of claim 14 , further comprising the step of placing a lower spherical washer between the lower bearing and the force measuring component.

18. The method of claim 14 , further comprising the step of comparing the force to a reference force measurement.

19. The method of claim 14 , further comprising the step of displaying data representative of the force on a display.

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 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 →
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 →
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 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 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 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 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Apr 19, 2012
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT (INCLUDING AS SUCCESSOR COLLATERAL AGENT TO CITICORP NORTH AMERICA, INC.)
To: SPIRIT AEROSYSTEMS, INC. (FKA MID-WESTERN AIRCRAFT SYSTEMS, INC.)
Reel/Frame 028072/0314 →
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 →
PATENT SECURITY AGREEMENT Recorded Aug 24, 2009
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
Reel/Frame 023134/0318 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 20, 2008
From: SYLVA, GILBERT D.; ALLEN, CASEY D.; HIGH, DANNY R.
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 021415/0905 →