Methods and systems for supplying fuel to gas turbine engines
Methods and systems for supply of fuel for a turbine-driven fracturing pump system used in hydraulic fracturing may be configured to identify when the supply pressure of primary fuel to a plurality of gas turbine engines of a plurality of hydraulic fracturing units falls below a set point, identify a gas turbine engine of the fleet of hydraulic fracturing units operating on primary fuel with highest amount of secondary fuel available, and to selectively transfer the gas turbine engine operating on primary fuel with the highest amount of secondary fuel from primary fuel operation to secondary fuel operation. Some methods and systems may be configured to transfer all gas turbine engines to secondary fuel operation and individually and/or sequentially restore operation to primary fuel operation and/or to manage primary fuel operation and/or secondary fuel operation for portions of the plurality of gas turbine engines.
1. A system for supplying fuel to a plurality of gas turbine engines, the system comprising:
a primary sensor associated with the plurality of gas turbine engines, the primary sensor configured to generate a primary signal indicative of an ability of a primary fuel source to supply an amount of primary fuel sufficient to operate the plurality of gas turbine engines at a first output;
a plurality of secondary sensors, each of the plurality of secondary sensors associated with each one of the plurality of gas turbine engines and configured to generate a secondary signal indicative of an amount of secondary fuel available from a plurality of secondary fuel supplies, each of the plurality of secondary fuel supplies associated with each of the plurality of gas turbine engines; and
a controller in communication with the primary sensor, each of the plurality of secondary sensors, and a plurality of primary valves, each of the plurality of primary valves configured to control flow communication between the primary fuel source and each one of the plurality of gas turbine engines, the controller configured to:
determine, based at least in part on the primary signal, that the primary fuel source is supplying an insufficient amount of the primary fuel to operate one or more of the plurality of gas turbine engines at the first output;
determine, based at least in part on the secondary signals, that the amount of the secondary fuel available from a first secondary fuel supply associated with a first gas turbine engine of the plurality of gas turbine engines is greater than the amount of the secondary fuel available from each of a remainder of the plurality of secondary fuel supplies associated with a remainder of the plurality of gas turbine engines;
cause a primary valve of the plurality of primary valves to inhibit flow communication between the primary fuel source and the first gas turbine engine of the plurality of gas turbine engines; and
cause supply of the secondary fuel from the first secondary fuel supply to the first gas turbine engine of the plurality of gas turbine engines.
2. The system of claim 1 , wherein the controller is further configured to:
determine, after causing the primary valve to inhibit flow communication between the primary fuel source and the first gas turbine engine of the plurality of gas turbine engines, based at least in part on the primary signal, whether the primary fuel source is supplying a sufficient amount of the primary fuel to operate the remainder of the plurality of gas turbine engines at the first output.
3. The system of claim 2 , wherein, when the controller determines the primary fuel source is not supplying the sufficient amount of the primary fuel to operate the remainder of the plurality of gas turbine engines at the first output, the controller is configured to:
determine, based at least in part on the secondary signals, that the amount of the secondary fuel available from a second secondary fuel supply associated with a second gas turbine engine of the plurality of gas turbine engines is greater than the amount of the secondary fuel available from each of a second remainder of the plurality of secondary fuel supplies associated with a second remainder of the plurality of gas turbine engines;
cause the primary valve of the plurality of primary valves to inhibit flow communication between the primary fuel source and the second gas turbine engine of the plurality of gas turbine engines; and
cause supply of the secondary fuel from the second secondary fuel supply to the second gas turbine engine of the plurality of gas turbine engines.
4. The system of claim 2 , wherein, when the controller determines the primary fuel source has sufficient capacity to operate the remainder of the plurality of gas turbine engines at the first output, the controller is configured to:
wait a period of time; and
one of:
(1) if, following the period of time, the controller determines that the primary fuel source continues to supply the sufficient amount of the primary fuel to operate the remainder of the plurality of gas turbine engines at the first output, cease supply of the secondary fuel from the first secondary fuel supply to the first gas turbine engine of the plurality of gas turbine engines; and
cause the primary valve of the plurality of primary valves to allow flow communication between the primary fuel source and the first gas turbine engine of the plurality of gas turbine engines; or
(2) if, following the period of time, the controller determines that the primary fuel source has insufficient capacity to operate the remainder of the plurality of gas turbine engines at the first output, cause the primary valve to inhibit flow communication between the primary fuel source and a second gas turbine engine of the plurality of gas turbine engines; and
cause supply of the secondary fuel from the second secondary fuel supply to the second gas turbine engine.
5. The system of claim 1 , wherein:
the primary sensor comprises a plurality of primary sensors, each of the plurality of primary sensors associated with each one of the plurality of gas turbine engines and configured to generate the primary signal indicative of the ability of the primary fuel source to supply the amount of the primary fuel sufficient to operate the plurality of gas turbine engines at the first output; and
the controller is configured to determine, based at least in part on the primary signals generated by the plurality of primary sensors, whether the primary fuel source has the ability to supply the amount of the primary fuel sufficient to operate the plurality of gas turbine engines at the first output.
6. The system of claim 5 , wherein the controller is configured to cause the plurality of primary valves to inhibit flow communication between the primary fuel source and the plurality of gas turbine engines.
7. A system for supplying fuel to a plurality of gas turbine engines, the system comprising:
a primary sensor associated with the plurality of gas turbine engines, the primary sensor configured to generate a primary signal indicative of an ability of a primary fuel source to supply an amount of primary fuel sufficient to operate the plurality of gas turbine engines at a first output; and
a controller in communication with the primary sensor and a plurality of primary valves, each of the plurality of primary valves configured to control flow communication between the primary fuel source and each one of the plurality of gas turbine engines, the controller configured to:
determine, based at least in part on the primary signal, that the primary fuel source does not have the ability to supply the amount of the primary fuel sufficient to operate the plurality of gas turbine engines at the first output;
cause one or more of the primary valves configured to control flow communication between the primary fuel source and the plurality of gas turbine engines to inhibit flow communication between the primary fuel source and the plurality of gas turbine engines;
cause supply of a secondary fuel from a plurality of secondary fuel supplies to each of the plurality of gas turbine engines, each of the plurality of secondary fuel supplies associated with each one of the plurality of gas turbine engines; and
cause operation of the plurality of gas turbine engines at the first output using the secondary fuel.
8. The system of claim 7 , wherein the controller is further configured to:
cause flow communication between the primary fuel source and one or more of the plurality of gas turbine engines; and
determine, based at least in part on the primary signal, whether the primary fuel source has the ability to supply the amount of the primary fuel sufficient to operate the one or more of the plurality of gas turbine engines at the first output.
9. The system of claim 8 , wherein the controller is further configured to:
based at least in part on determining that the primary fuel source has the ability to supply the amount of the primary fuel sufficient to operate the one or more of the plurality of gas turbine engines at the first output, cause flow communication between the primary fuel source and at least two of the plurality of gas turbine engines; and
determine, based at least in part on the primary signal, whether the primary fuel source has the ability to supply the amount of the primary fuel sufficient to operate the at least two gas turbine engines at the first output.
10. The system of claim 9 , wherein the controller is further configured to:
based at least in part on determining that the primary fuel source has the ability to supply the amount of the primary fuel sufficient to operate the at least two gas turbine engines at the first output, cause flow communication between the primary fuel source and at least three of the plurality of gas turbine engines; and
determine, based at least in part on the primary signal, whether the primary fuel source has the ability to supply the amount of the primary fuel sufficient to operate the at least three gas turbine engines at the first output.
11. The system of claim 7 , wherein the controller is further configured to:
cause sequential restoration of flow communication between the primary fuel source and each of the plurality of gas turbine engines until the controller determines, based at least in part on the primary signal, that the primary fuel source lacks the ability to supply the amount of the primary fuel sufficient to operate at the first output a first portion of the plurality of gas turbine engines to which flow communication with the primary fuel source has been restored; and
manage flow communication between the primary fuel source and each of the plurality of gas turbine engines, such that a second portion of the plurality of gas turbine engines is supplied with the primary fuel from the primary fuel source and a third portion of the plurality of gas turbine engines is supplied with the secondary fuel from a portion of the plurality of secondary fuel supplies associated with each of the third portion of the gas turbine engines, such that the plurality of gas turbine engines are operated at the first output.
12. The system of claim 11 , wherein the second portion of the plurality of gas turbine engines is a first number of gas turbine engines and the third portion of the plurality of gas turbine engines is a second number of gas turbine engines, and the first number and the second number equals a total number of the plurality of gas turbine engines, and wherein the controller is configured to periodically cause:
(1) a first subset of the second portion of the plurality of gas turbine engines to switch from using the primary fuel from the primary fuel source to each using the secondary fuel from the secondary fuel supply associated with each of the first subset of the second portion of the plurality of gas turbine engines; and
(2) a second subset of the third portion of the plurality of gas turbine engines to switch from using the secondary fuel from the secondary fuel supply associated with each of the second subset of the third portion of the plurality of gas turbine engines,
wherein a number of the plurality of gas turbine engines in the first subset is equal to a number of the plurality of the gas turbine engines in the second subset.
13. The system of claim 12 , wherein the controller is configured to manage flow communication between the primary fuel source and each of the plurality of gas turbine engines until the controller determines, based at least in part on the primary signal, that the primary fuel source is sufficiently supplying the primary fuel to operate the plurality of gas turbine engines at the first output.
14. The system of claim 7 , wherein:
the primary sensor comprises a plurality of primary sensors, each of the plurality of primary sensors associated with each one of the plurality of gas turbine engines and configured to generate the primary signal indicative of the ability of the primary fuel source to supply the amount of the primary fuel sufficient to operate each of the plurality of gas turbine engines at the first output; and
the controller is configured to determine, based at least in part on primary signals generated by the plurality of primary sensors, whether the primary fuel source lacks the ability to supply the amount of the primary fuel sufficient to operate each of the plurality of gas turbine engines at the first output.
15. The system of claim 11 , wherein the second portion of the plurality of gas turbine engines is the same number as the third portion of the plurality of gas turbine engines.