IP Library Granted Patent US 11,473,997
Granted Patent B2
US 11,473,997 · App. 17/717,370 · Granted Oct 18, 2022

Fuel, communications, and power connection systems and related methods

Inventors: Tony Yeung (Houston, TX); Ricardo Rodriguez-Ramon (Houston, TX); Patrick Thomson (Houston, TX)
Assignee: BJ Energy Solutions, LLC
G01M3/2815E21B34/08E21B43/2607E21B43/267E21B47/12F02C7/222F02C9/28F02C9/56G01M3/26
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Quick Facts
Patent No.
US 11,473,997
App. No.
17/717,370
Granted
Oct 18, 2022
Kind
B2
Abstract

Embodiments of systems and methods for supplying fuel, enabling communications, and conveying electric power associated with operation of a hydraulic fracturing unit of a plurality of hydraulic fracturing units are disclosed and may include a fuel line connection assembly configured to be connected to the first hydraulic fracturing unit and to supply fuel from a fuel source to a gas turbine engine connected to the hydraulic fracturing unit. A system also may include a communications cable assembly configured to be connected to the hydraulic fracturing unit and to enable data communications between the hydraulic fracturing unit and a data center or another hydraulic fracturing unit. A system further may include a power cable assembly configured to be connected to the hydraulic fracturing unit and to convey electric power between the hydraulic fracturing unit and a remote electrical power source or the plurality of hydraulic fracturing units.

Claims (115)

1. A method for pressure testing at least a portion of a fuel delivery system for supplying fuel from a fuel source to one or more gas turbine engines, the method comprising:

causing a first valve to be in an open condition, the first valve configured to one of facilitate flow communication or prevent flow communication between the fuel source and a first gas turbine engine of the one or more gas turbine engines;

causing a second valve to be in a closed condition, the second valve configured to one of facilitate flow communication or prevent flow communication between a filter configured to filter one or more of particulates or liquids from fuel and the first gas turbine engine;

causing a third valve to be in an open condition, the third valve configured to one of facilitate flow communication or prevent flow communication between a pressure source and the filter;

increasing pressure via the pressure source in the at least a portion of the fuel delivery system;

monitoring a signal indicative of pressure in the at least a portion of the fuel delivery system; and

based at least in part on the signal, determining whether the at least a portion of the fuel delivery system has a leak.

2. The method of claim 1 , further comprising initiating a timer, wherein increasing pressure is caused until a predetermined time has elapsed on the timer.

3. The method of claim 2 , wherein determining whether the at least a portion of the fuel delivery system has a leak comprises:

comparing the pressure in the at least a portion of the fuel delivery system at the end of the predetermined time to a predetermined pressure; and

determining one of:

the at least a portion of the fuel delivery system has a leak when the pressure in the at least a portion of the fuel delivery system is less than the predetermined pressure; or

the at least a portion of the fuel delivery system does not have a leak when the pressure in the at least a portion of the fuel delivery system is at least the predetermined pressure.

4. The method of claim 3 , wherein determining the at least a portion of the fuel delivery system does not have a leak further comprises:

initiating the timer and waiting for a second predetermined time to elapse; and

comparing the pressure in the at least a portion of the fuel delivery system at the second predetermined time to the predetermined pressure.

5. The method of claim 4 , wherein after waiting for the second predetermined time to elapse, the method further comprises determining one of:

the at least a portion of the fuel delivery system has a leak when the pressure in the at least a portion of the fuel delivery system is 5% or more less than the predetermined pressure; or

the at least a portion of the fuel delivery system does not have a leak when the pressure in the at least a portion of the fuel delivery system is within 5% of the predetermined pressure or greater.

6. The method of claim 1 , wherein increasing pressure via the pressure source in the at least a portion of the fuel delivery system comprises one or more of:

activating a compressor in flow communication with the at least a portion of the fuel delivery system; or

opening a valve of a pressurized cylinder in flow communication with the at least a portion of the fuel delivery system.

7. The method of claim 1 , further comprising generating a signal indicative of a leak when a determination of the at least a portion of the fuel delivery system has a leak occurs.

8. The method of claim 1 , further comprising:

initiating a timer;

ceasing the pressure testing after a predetermined time has elapsed;

causing a fourth valve to be in an open condition, the fourth valve configured to release pressure in the at least a portion of the fuel delivery system.

9. The method of claim 1 , wherein the fuel delivery system comprises a controller, and wherein the method comprises one or more of:

causing, via the controller, the first valve to be in the open condition;

causing, via the controller, the second valve to be in the closed condition;

causing, via the controller, the third valve to be in the open condition;

increasing, via the controller, the pressure via the pressure source;

monitoring, via the controller, the signal indicative of pressure, or

determining, via the controller, whether the at least a portion of the fuel delivery system has a leak.

10. A method for pressure testing at least a portion of a fuel delivery system for supplying fuel from a fuel source to one or more gas turbine engines, the fuel delivery system including a controller, the method comprising:

causing a first valve to be in an open condition via the controller, the first valve configured to one of facilitate flow communication or prevent flow communication between the fuel source and a first gas turbine engine of the one or more gas turbine engines;

causing a second valve to be in a closed condition via the controller, the second valve configured to one of facilitate flow communication or prevent flow communication between a filter configured to filter one or more of particulates or liquids from fuel and the first gas turbine engine;

causing a third valve to be in an open condition via the controller, the third valve configured to one of facilitate flow communication or prevent flow communication between a pressure source and the filter;

increasing pressure via the pressure source in the at least a portion of the fuel delivery system;

monitoring a signal indicative of pressure in the at least a portion of the fuel delivery system; and

based at least in part on the signal, determining whether the at least a portion of the fuel delivery system has a leak.

11. The method of claim 10 , further comprising initiating a timer, wherein increasing pressure is caused until a predetermined time has elapsed on the timer.

12. The method of claim 11 , wherein determining whether the at least a portion of the fuel delivery system has a leak comprises:

comparing the pressure in the at least a portion of the fuel delivery system at the end of the predetermined time to a predetermined pressure; and

determining one of:

the at least a portion of the fuel delivery system has a leak when the pressure in the at least a portion of the fuel delivery system is less than the predetermined pressure; or

the at least a portion of the fuel delivery system does not have a leak when the pressure in the at least a portion of the fuel delivery system is at least the predetermined pressure.

13. The method of claim 12 , wherein determining the at least a portion of the fuel delivery system does not have a leak further comprises:

initiating the timer and waiting for a second predetermined time to elapse; and

comparing the pressure in the at least a portion of the fuel delivery system at the second predetermined time to the predetermined pressure.

14. The method of claim 13 , wherein after waiting for the second predetermined time to elapse, the method further comprises determining one of:

the at least a portion of the fuel delivery system has a leak when the pressure in the at least a portion of the fuel delivery system is 5% or more less than the predetermined pressure; or

the at least a portion of the fuel delivery system does not have a leak when the pressure in the at least a portion of the fuel delivery system is within 5% of the predetermined pressure or greater.

15. The method of claim 10 , wherein increasing pressure via the pressure source in the at least a portion of the fuel delivery system comprises one or more of:

activating a compressor in flow communication with the at least a portion of the fuel delivery system; or

opening a valve of a pressurized cylinder in flow communication with the at least a portion of the fuel delivery system.

16. The method of claim 10 , further comprising generating a signal via the controller indicative of a leak when a determination of a leak occurs.

17. The method of claim 10 , further comprising:

initiating a timer;

ceasing the pressure testing after a predetermined time has elapsed;

causing a fourth valve to be in an open condition, the fourth valve configured to release pressure in the at least a portion of the fuel delivery system.

18. The method of claim 10 , further comprising one or more of:

increasing, via the controller, the pressure via the pressure source;

monitoring, via the controller, the signal indicative of pressure, and

determining, via the controller, whether the at least a portion of the fuel delivery system has a leak.

19. A method for pressure testing at least a portion of a fuel delivery system for supplying fuel from a fuel source to one or more gas turbine engines, the fuel delivery system including a controller, the method comprising:

causing a first valve to be in an open condition via the controller, the first valve configured to one of facilitate flow communication or prevent flow communication between the fuel source and a first gas turbine engine of the one or more gas turbine engines;

causing a second valve to be in a closed condition via the controller, the second valve configured to one of facilitate flow communication or prevent flow communication between a filter configured to filter one or more of particulates or liquids from fuel and the first gas turbine engine;

causing a third valve to be in an open condition via the controller, the third valve configured to one of facilitate flow communication or prevent flow communication between a pressure source and the filter;

increasing pressure via the pressure source in the at least a portion of the fuel delivery system, increasing pressure via the pressure source includes (a) activating a compressor in flow communication with the at least a portion of the fuel delivery system, or (b) opening a valve of a pressurized cylinder in flow communication with the at least a portion of the fuel delivery system;

monitoring a signal indicative of pressure in the at least a portion of the fuel delivery system;

based at least in part on the signal, determining whether the at least a portion of the fuel delivery system has a leak; and

generating a signal via the controller indicative of the leak.

20. The method of claim 19 , further comprising initiating a timer, wherein increasing pressure is caused until a predetermined time has elapsed on the timer.

21. The method of claim 20 , wherein determining whether the at least a portion of the fuel delivery system has a leak comprises:

comparing the pressure in the at least a portion of the fuel delivery system at the end of the predetermined time to a predetermined pressure; and

determining one of:

the at least a portion of the fuel delivery system has a leak when the pressure in the at least a portion of the fuel delivery system is less than the predetermined pressure; or

the at least a portion of the fuel delivery system does not have a leak when the pressure in the at least a portion of the fuel delivery system is at least the predetermined pressure.

22. The method of claim 21 , wherein determining the at least a portion of the fuel delivery system does not have a leak further comprises:

initiating the timer and waiting for a second predetermined time to elapse; and

comparing the pressure in the at least a portion of the fuel delivery system at the second predetermined time to the predetermined pressure.

23. The method of claim 22 , wherein after waiting for the second predetermined time to elapse, the method further comprises determining one of:

the at least a portion of the fuel delivery system has a leak when the pressure in the at least a portion of the fuel delivery system is 5% or more less than the predetermined pressure; or

the at least a portion of the fuel delivery system does not have a leak when the pressure in the at least a portion of the fuel delivery system is within 5% of the predetermined pressure or greater.

24. The method of claim 19 , further comprising:

initiating a timer;

ceasing the pressure testing after a predetermined time has elapsed;

causing a fourth valve to be in an open condition via the controller, the fourth valve configured to release pressure in the at least a portion of the fuel delivery system.

25. The method of claim 19 , further comprising one or more of:

increasing, via the controller, the pressure via the pressure source;

monitoring, via the controller, the signal indicative of pressure, and

determining, via the controller, whether the at least a portion of the fuel delivery system has a leak.

26. A method for pressure testing at least a portion of a fuel delivery system for supplying fuel from a fuel source to one or more gas turbine engines, the fuel delivery system including a controller, the method comprising:

causing a first valve to be in an open condition via the controller, the first valve configured to one of facilitate flow communication or prevent flow communication between the fuel source and a first gas turbine engine of the one or more gas turbine engines;

causing a second valve to be in a closed condition via the controller, the second valve configured to one of facilitate flow communication or prevent flow communication between a filter configured to filter one or more of particulates or liquids from fuel and the first gas turbine engine;

causing a third valve to be in an open condition via the controller, the third valve configured to one of facilitate flow communication or prevent flow communication between a pressure source and the filter;

increasing pressure via the pressure source in the at least a portion of the fuel delivery system, increasing pressure via the pressure source includes (a) activating a compressor in flow communication with the at least a portion of the fuel delivery system, or (b) opening a valve of a pressurized cylinder in flow communication with the at least a portion of the fuel delivery system;

monitoring via the controller a signal indicative of pressure in the at least a portion of the fuel delivery system;

based at least in part on the signal, determining via the controller whether the at least a portion of the fuel delivery system has a leak.

27. The method of claim 26 , further comprising initiating a timer, wherein increasing pressure is caused until a predetermined time has elapsed on the timer, and wherein determining whether the at least a portion of the fuel delivery system has a leak comprises:

comparing the pressure in the at least a portion of the fuel delivery system at the end of the predetermined time to a predetermined pressure; and

determining via the controller one of:

the at least a portion of the fuel delivery system has a leak when the pressure in the at least a portion of the fuel delivery system is less than the predetermined pressure; or

the at least a portion of the fuel delivery system does not have a leak when the pressure in the at least a portion of the fuel delivery system is at least the predetermined pressure.

28. The method of claim 27 , wherein determining the at least a portion of the fuel delivery system does not have a leak further comprises:

initiating the timer and waiting for a second predetermined time to elapse; and

comparing the pressure in the at least a portion of the fuel delivery system at the second predetermined time to the predetermined pressure.

29. The method of claim 28 , wherein after waiting for the second predetermined time to elapse, the method further comprises determining via the controller one of:

the at least a portion of the fuel delivery system has a leak when the pressure in the at least a portion of the fuel delivery system is 5% or more less than the predetermined pressure; or

the at least a portion of the fuel delivery system does not have a leak when the pressure in the at least a portion of the fuel delivery system is within 5% of the predetermined pressure or greater.

30. The method of claim 26 , further comprising:

initiating via a controller a timer;

ceasing the pressure testing after a predetermined time has elapsed;

causing a fourth valve to be in an open condition via the controller, the fourth valve configured to release pressure in the at least a portion of the fuel delivery system.

Assignments (4)
SECURITY INTEREST Recorded Sep 17, 2024
From: BJ ENERGY SOLUTIONS. LLC
To: ECLIPSE BUSINESS CAPITAL LLC. AS AGENT
Reel/Frame 068970/0125 →
SECURITY INTEREST Recorded Dec 13, 2022
From: BJ ENERGY SOLUTIONS, LLC
To: ECLIPSE BUSINESS CAPITAL LLC
Reel/Frame 062116/0333 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 11, 2022
From: YEUNG, TONY; RODRIGUEZ-RAMON, RICARDO; THOMSON, PATRICK
To: BJ SERVICES, LLC
Reel/Frame 059558/0880 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 11, 2022
From: BJ SERVICES, LLC
To: BJ ENERGY SOLUTIONS, LLC
Reel/Frame 059559/0001 →
Continuity (5)
Division 15929708 · May 18, 2020
Provisional Application 62704401 · May 8, 2020
Provisional Application 62900100 · Sep 13, 2019
Provisional Application 62900112 · Sep 13, 2019
Related Publication 20220236136A1 · Jul 28, 2022