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A gas turbine health monitoring fuel system including a fuel splitter, a first and second fuel nozzle, a first and second fuel pump, and a common drive coupled to the first and second fuel pumps. The first and second fuel pumps are downstream from the fuel splitter. The first fuel nozzle is fluidly

A gas turbine health monitoring fuel system including a fuel splitter, a first and second fuel nozzle, a first and second fuel pump, and a common drive coupled to the first and second fuel pumps. The first and second fuel pumps are downstream from the fuel splitter. The first fuel nozzle is fluidly coupled to the first fuel pump by a first fuel stream. The second fuel nozzle is fluidly coupled to the second fuel pump by a second fuel stream. The common drive is configured to drive the first and second fuel pumps at a same speed. The controller system is configured to determine a first fuel pressure in the first fuel stream, determine a second fuel pressure in the second fuel stream, and identify a difference between the first and second fuel pressures.

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1. A gas turbine health monitoring fuel system comprising: a fuel splitter;a first fuel pump downstream from the fuel splitter;a first fuel nozzle fluidly coupled to the first fuel pump by a first fuel stream;a second fuel pump downstream from the fuel splitter;a second fuel nozzle fluidly coupled t

1. A gas turbine health monitoring fuel system comprising: a fuel splitter;a first fuel pump downstream from the fuel splitter;a first fuel nozzle fluidly coupled to the first fuel pump by a first fuel stream;a second fuel pump downstream from the fuel splitter;a second fuel nozzle fluidly coupled to the second fuel pump by a second fuel stream; a common drive coupled to the first and second fuel pumps and configured to drive the first and second fuel pumps at a same speed;a controller system configured to: identify a first fuel pressure in the first fuel stream;identify a second fuel pressure in the second fuel stream; anddetermine a difference between the first and second fuel pressures to diagnose if at least one of the fuel nozzles is faulty; anda primary fuel source configured to supply a primary fuel stream to the fuel splitter, wherein the controller system is further configured to: identify a primary fuel pressure in the primary fuel stream;compare the first fuel pressure to the primary fuel pressure;compare the second fuel pressure to the primary fuel pressure;identify a difference between at least one of the first and second fuel pressures and the primary fuel pressure; andnotify a user that at least one of the fuel nozzles is faulty. 2. The gas turbine health monitoring fuel system of claim 1, wherein the common drive is a rotatable shaft of a positive-displacement fuel pump system comprising the first and second fuel pumps. 3. The gas turbine health monitoring fuel system of claim 1, wherein the common drive comprises a plurality of gears. 4. The gas turbine health monitoring fuel system of claim 1, further comprising: an additional first fuel nozzle fluidly coupled to the first fuel pump by the first fuel stream; andan additional second fuel nozzle fluidly coupled to the second fuel pump by the second fuel stream. 5. The gas turbine health monitoring fuel system of claim 1, the controller system further configured to: determine if at least one fuel nozzle of the first and second fuel nozzles is improperly functioning based on the identified difference between the at least one of the first and second fuel pressures and the primary fuel pressure; andnotify a user that the at least one fuel nozzle is improperly functioning. 6. The gas turbine health monitoring fuel system of claim 5, the controller system further configured to identify a vapor lock condition in the gas turbine fuel system. 7. A fuel pressure sensing system for a gas turbine engine comprising: a first fuel splitter configured to split a primary fuel stream into a first and second stream;a first and second flow controller, wherein the first flow controller is configured to move the first stream at a first flow rate and the second flow controller is configured to move the second stream at the first flow rate;a first and second fuel nozzle respectively downstream from the respective first and second flow controllers;a first pressure sensor positioned downstream from the first flow controller and upstream from the first fuel nozzle, wherein the first pressure sensor is configured to sense a first fuel stream pressure between the first flow controller and the first fuel nozzle;a second pressure sensor positioned downstream from the second flow controller and upstream from the second fuel nozzle, wherein the second pressure sensor is configured to sense a second fuel stream pressure between the second flow controller and the second fuel nozzle;a primary fuel source configured to supply a primary fuel stream to the fuel splitter; anda controller system configured to: identify a primary fuel pressure in the primary fuel stream;compare the first fuel pressure to the primary fuel pressure;compare the second fuel pressure to the primary fuel pressure; andidentify a difference between at least one of the first and second fuel pressures and the primary fuel pressure; and at least one of: a common rotatable shaft coupled to the first and second flow controllers and configured to drive the first and second flow controllers at a same speed; andat least one gear coupled to the first and second flow controllers configured to drive the first and second flow controllers at the same speed; andnotify a user that at least one of the fuel nozzles is faulty. 8. The fuel pressure sensing system of claim 7, wherein the controller is further configured to determine if the first fuel stream pressure is different than the second fuel stream pressure. 9. The fuel pressure sensing system of claim 8, wherein the fuel pressure sensing system is configured to remove a vapor lock condition from one of the first and second fuel nozzles. 10. The fuel pressure sensing system of claim 7, further comprising: a primary flow controller configured to supply the flow splitter with the primary fuel stream; anda pressure sensor downstream from the primary flow controller and upstream from the flow splitter and configured to sense a primary fuel stream pressure of the primary fuel stream supplied to the flow splitter. 11. The fuel pressure sensing system of claim 10, further comprising a controller configured to: identify a difference between the first fuel stream pressure and the primary fuel stream pressure; andnotify a user that the first fuel nozzle is faulty. 12. The fuel pressure sensing system of claim 11, wherein the first and second flow controllers are respectively a first and second positive displacement pump driven at a same speed. 13. A method of determining fuel nozzle health using the gas turbine health monitoring fuel system of claim 1 comprising: monitoring the primary fuel pressure of the primary fuel stream before the primary fuel stream is divided into the first and second fuel stream;monitoring the first fuel pressure of the first fuel stream initially driven at a first speed, wherein the first fuel stream is initially driven at the first speed to supply the first fuel nozzle;monitoring the second fuel pressure of the second fuel stream initially driven at the first speed, wherein the second fuel stream is initially driven at the first speed to supply the second fuel nozzle;comparing the pressure of the first fuel stream and the pressure of the second fuel stream to the pressure of the primary fuel stream;identifying which of the first and second fuel nozzles is functioning improperly based on the comparing the pressure of the first fuel stream and the pressure of the second fuel stream to the pressure of the primary fuel stream; andnotifying a user that at least one of the fuel nozzles is faulty. 14. The method of claim 13, further comprising notifying a user which of the first and second fuel nozzles is functioning improperly based on the identifying which of the first and second fuel nozzles is functioning improperly. 15. The method of claim 13, further comprising comparing the first fuel pressure of the first fuel stream to the second fuel pressure of the second fuel stream to determine if at least one of the first and second fuel nozzles is functioning improperly. 16. The method of claim 13, further comprising: driving a first fuel stream flow controller at the first speed; anddriving a second fuel stream flow controller at the first speed, wherein the first fuel stream flow controller is coupled to the second fuel stream flow controller. 17. The method of claim 16, further comprising identifying a vapor lock condition in a fuel system based on the comparing the first fuel pressure of the first fuel stream to the primary fuel pressure of the primary fuel stream.