IP Library Granted Patent US 11,433,504
Granted Patent B1
US 11,433,504 · App. 16/295,976 · Granted Sep 6, 2022

Systems and methods for improving jet cutting performance via force sensing

Inventors: Charles D. Burnham (Southbury, CT); Mohamed A. Hashish (Bellevue, WA)
Assignee: Flow International Corporation
B24C7/0015B24C1/045B24C3/32B24C7/0023B24C7/0061
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Quick Facts
Patent No.
US 11,433,504
App. No.
16/295,976
Granted
Sep 6, 2022
Kind
B1
Abstract

Disclosed herein are systems and methods for improving the performance of a fluid jet cutting system by testing and adjusting characteristics of the system based on the effect of the characteristics on forces imparted by the system to a workpiece being cut. Also disclosed are systems and methods for monitoring and validating the performance of fluid jet cutting systems, and for diagnosing such systems. In some cases, the technologies described herein can be used to determine whether components of a fluid jet system require maintenance, or that characteristics of the system require adjustment.

Claims (32)

1. A method of assessing performance of a fluid jet system, the method comprising:

situating a workpiece at least partially within a working envelope of a cutting head of a fluid jet cutting system to be cut by the cutting head;

situating a coupon at least partially within the working envelope of the cutting head of the fluid jet cutting system to be cut by the cutting head;

forming one or more cuts in the workpiece using the cutting head of the fluid jet cutting system;

periodically interrupting the forming of the one or more cuts in the workpiece;

during at least one of the periodic interruptions, forming a sample cut in the coupon using the cutting head of the fluid jet cutting system;

while forming the sample cut in the coupon, measuring a history of reactive forces imparted by the fluid jet cutting system to the coupon; and

using the measured reactive forces to assess the performance of the fluid jet cutting system.

2. The method of claim 1 , wherein the history of measured reactive forces is used to determine whether a component of the fluid jet cutting system requires maintenance.

3. The method of claim 1 , wherein the history of measured reactive forces is used to determine whether a setting for a characteristic of the fluid jet cutting system requires adjustment.

4. The method of claim 1 , wherein situating the coupon at least partially within the working envelope of the cutting head of the fluid jet cutting system comprises situating the coupon on a baseplate at least partially within the working envelope of the cutting head which is coupled to a force measurement device.

5. The method of claim 1 , wherein measuring the history of reactive forces comprises measuring a horizontal component or a vertical component of net reactive forces imparted by the fluid jet cutting system to the coupon.

6. The method of claim 1 , wherein forming a sample cut in the coupon comprises piercing the coupon.

7. The method of claim 1 , wherein while forming the sample cut in the coupon, an abrasive flow rate of the fluid jet cutting system is zero.

8. The method of claim 7 , wherein while forming the one or more cuts in the workpiece, the abrasive flow rate is non-zero.

9. The method of claim 1 , wherein measuring the history of reactive forces imparted by the fluid jet cutting system to the coupon includes measuring reactive forces as a fluid jet generated by the system moves from a partially engaged condition to a fully engaged condition.

10. A method of assessing performance of a fluid jet system, the method comprising:

prior to forming one or more cuts in a workpiece with a cutting head of a fluid jet cutting system, forming a baseline cut in a coupon using the fluid jet system while moving the cutting head at an initial working speed;

while forming the baseline cut, measuring a corresponding baseline history of reactive forces imparted by the fluid jet system to the coupon;

periodically interrupting the forming of the one or more cuts in the workpiece;

during at least one of the periodic interruptions, forming a validation cut in the coupon using the fluid jet system while moving the cutting head at the initial working speed;

while forming the validation cut, measuring a corresponding validation history of reactive forces imparted by the fluid jet system to the coupon; and

comparing the validation history of reactive forces to the baseline history of reactive forces to assess the performance of the fluid jet system.

11. The method of claim 10 , wherein the periodic interruptions occur between successive cuts formed in the workpiece.

12. The method of claim 10 , wherein the periodic interruptions occur between forming cuts in successive parts of the workpiece.

13. The method of claim 10 , wherein the periodic interruptions occur at pre-determined intervals based on a geometry of the workpiece.

14. The method of claim 10 , wherein the validation history of reactive forces is used to determine whether a component of the fluid jet system requires maintenance.

15. The method of claim 14 , wherein the determination whether a component of the fluid jet system requires maintenance is based on exceeding a threshold discrepancy between an average or typical force of the validation history of reactive forces and an average or typical force of the baseline history of reactive forces.

16. The method of 15 , wherein the threshold discrepancy is between about a 5 percent discrepancy and about a 15 percent discrepancy.

17. The method of claim 10 , wherein the validation history of reactive forces is used to determine whether the initial working speed requires adjustment.

18. The method of claim 17 , wherein the determination whether the initial working speed requires adjustment is based on exceeding a threshold discrepancy between an average or typical force of the validation history of reactive forces and an average or typical force of the baseline history of reactive forces.

19. The method of claim 18 , wherein the threshold discrepancy is between about a 5 percent discrepancy and about a 15 percent discrepancy.

Assignments (2)
PATENT SECURITY AGREEMENT Recorded Sep 10, 2024
From: SHAPE TECHNOLOGIES GROUP, INC.,; FLOW INTERNATIONAL CORPORATION; DYNAMIC ROBOTIC SOLUTIONS, INC.; H2O JET, INC.; KMT WATERJET SYSTEMS, INC.
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 068922/0390 →
SECURITY INTEREST Recorded Sep 6, 2024
From: FLOW INTERNATIONAL CORPORATION
To: ATLANTIC PARK STRATEGIC CAPITAL FUND II, L.P., AS ADMINISTRATIVE AGENT
Reel/Frame 068882/0219 →