Systems and methods for selectively augmenting power output of a gas turbine engine

Patent metadata

Field	Value
Publication number	US-10801409-B2
Application number	US-201715658531-A
Country	US
Kind code	B2
Filing date	Jul 25, 2017
Priority date	Aug 2, 2016
Publication date	Oct 13, 2020
Grant date	Oct 13, 2020

Abstract

Systems and methods for augmenting power output when operating a load having relatively brief periods of high energy demand and high heat generation. A system comprises a gas turbine engine including a coolant injection assembly, an electrical generator coupled to the gas turbine engine, a high-energy operating load coupled to the electrical generator, and a cooling system adapted to provide cooling to the high-energy operating load. The cooling system is coupled and adapted to provide coolant to the coolant injection assembly of the gas turbine engine. A method comprises coupling the cooling system to the coolant injection assembly at the inlet of the gas turbine engine, selectively diverting at least a portion of the coolant of the cooling system to the coolant injection assembly, and spraying the diverted coolant into air entering the gas turbine engine.

First claim

What is claimed is:

1. A system for augmenting power output when operating a high-energy electrical load having periods of high energy demand and high heat generation, the system comprising:
a gas turbine engine including a coolant injection assembly, a compressor, a combustor, and a turbine:
an electrical generator coupled to the gas turbine engine;
the high-energy electrical load coupled to the electrical generator, the high-energy electrical load having the periods of high energy demand and high heat generation;
a cooling system adapted to provide cooling to the high-energy electrical load;
the cooling system comprising a coolant loop including:
a first heat exchanger in thermal contact with the at least one high-energy electrical load;
a second heat exchanger remote from the at least one high-energy electrical load;

wherein coolant is circulated through the coolant loop;
a diverting line fluidly coupling the coolant loop to the coolant injection assembly;
wherein the cooling system is coupled and adapted to provide coolant used in the coolant loop, via the diverting line, to the coolant injection assembly of the gas turbine engine, including, during the periods of high energy demand and high heat generation of the high-energy electrical load, selectively providing, via the diverting line, the coolant used in the coolant loop to the coolant injection assembly, wherein the coolant injection assembly injects the coolant into the intake of the gas turbine engine to increase the power output of the gas turbine engine to meet the high energy demand of the high-energy electrical load.

2. The system of claim 1 wherein the coolant injection assembly comprises a plurality of nozzles in fluid communication with the cooling system, the plurality of nozzles disposed circumferentially about and upstream of an inlet of the gas turbine engine.

3. The system of claim 2 further comprising a coolant mixer disposed between the cooling system and the plurality of nozzles, the coolant mixer adapted to mix coolant from the cooling system with at least one secondary fluid stream prior to the coolant passing through the plurality of nozzles.

4. The system of claim 1 , wherein the coolant injection assembly is adapted to serve as an intercooler.

5. A method of augmenting the power output of a gas turbine engine in an operating assembly, the operating assembly including an electrical generator coupled to the gas turbine engine and a high-energy electrical load having a cooling system, the method comprising:
transferring energy from the high-energy electrical load via the cooling system by passing a coolant through a heat exchanger coupled to the high-energy electrical load and transferring the transferred energy from the coolant by passing the coolant through a second heat exchanger, wherein the coolant circulates between the heat exchanger and the second heat exchanger in a coolant loop, the second heat exchanger being remote from the high-energy electrical load, and the high-energy electrical load having periods of high energy demand and high heat generation;
operating the gas turbine engine to supply mechanical energy to the electrical generator, the electrical generator converting the mechanical energy to electrical energy;
transferring the electrical energy to the high-energy electrical load;
coupling the cooling system of the high-energy electrical load to a coolant injection assembly at an inlet of the gas turbine engine via a diverter line coupled to the coolant loop;
during the periods of high energy demand and high heat generation of the high-energy electrical load, diverting, via the diverter line, at least a portion of the coolant of the cooling system from the coolant loop to the coolant injection assembly; and
spraying the diverted coolant into air entering the gas turbine engine to increase the power output of the gas turbine engine to meet the high energy demand of the high-energy electrical load.

6. The method of claim 5 , further comprising: mixing, prior to spraying the diverted coolant into air entering the gas turbine engine, the diverted coolant with a secondary flow of water.

7. The method of claim 5 , further comprising: mixing, prior to spraying the diverted coolant into air entering the gas turbine engine, the diverted coolant with a secondary flow of alcohol.

8. The method of claim 6 , wherein the resulting mixture of water and diverted coolant has a water-alcohol ratio of 2:1.

9. The method of claim 7 , wherein the resulting mixture of alcohol and diverted coolant has a water-alcohol ratio of 2:1.

10. The method of claim 5 , wherein the diverted coolant is sprayed into air entering the gas turbine engine at a rate of between 0.5 and 0.75 gallons per minute.

11. The method of claim 5 , further comprising the steps of determining environmental conditions proximate the gas turbine engine and operational power output of the turbine given the environmental conditions; comparing the operational power output to a required load and injecting the coolant based upon the comparison.

12. The method of claim 11 wherein the environmental conditions are selected from the group consisting of altitude, temperature and air density.

13. The method of claim 11 wherein the step of determining operational power output comprises accessing empirical operational data associated with the turbine engine.

14. A method of increasing the power output of a gas turbine engine in an operating assembly, the operating assembly including an electrical generator coupled to the gas turbine engine and a high-energy electrical load having a cooling system, the method comprising:
transferring energy from the high-energy electrical load via the cooling system by passing a coolant through a heat exchanger coupled to the high-energy electrical load and transferring the transferred energy from the coolant by passing the coolant through a second heat exchanger wherein the coolant circulates between the heat exchanger and the second heat exchanger in a coolant loop, the second heat exchanger being remote from the high-energy electrical load, and the high-energy electrical load having relatively brief periods of high energy demand and high heat generation;
operating the gas turbine engine to supply mechanical energy to the electrical generator, the electrical generator converting the mechanical energy to electrical energy;
transferring the electrical energy to the high-energy electrical load;
coupling the cooling system of the high-energy electrical load to a plurality of nozzles disposed upstream of an inlet of the gas turbine engine via a diverter line coupled to the coolant loop:
during the periods of high energy demand and high heat generation of the high-energy electrical load, selectively diverting, via the diverter line, at least a portion of the coolant of the cooling system from the coolant loop toward the plurality of nozzles;
blending the diverted coolant with one or both of water and alcohol to form a blended fluid; and
passing the blended fluid through the plurality of nozzles such that the blended fluid is entrained in air entering the gas turbine engine to increase the power output of the gas turbine engine to meet the high energy demand of the high-energy electrical load.

15. The method of claim 14 further comprising, prior to the step of passing the blended fluid through the plurality of nozzles:
determining an operational power limit of the gas turbine engine based on environmental conditions proximate the gas turbine engine;
determining the power output of the gas turbine engine; and
selectively passing the blend

Assignees

• Rolls Royce Nam Tech Inc

Inventors

• Eifert Andrew J

Classifications

• F02C3/305

  Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids (F01K21/04 takes precedence) · CPC title

• F41H13/0043

  Directed energy weapons, i.e. devices that direct a beam of high energy content toward a target for incapacitating or destroying the target · CPC title

• F05D2260/212

  by water injection · CPC title

• F05D2220/76

  an electrical generator · CPC title

• F02C7/04

  Air intakes for gas-turbine plants or jet-propulsion plants · CPC title