Grid scale energy storage systems using thermal storage coupled with gas turbine air and steam injection
The invention relates generally to an electrical power and storage system and more specifically to ways and methods of using a thermal storage medium as a heat source to heat compressed air from a power augmentation system for use in a gas turbine engine.
1. A method of operating a compressed air and thermal energy storage system at a gas turbine power plant, the gas turbine power plant including a gas turbine engine comprising a compressor, a combustor, and a turbine, the method comprising:
operating a multistage auxiliary compressor by way of a fueled engine situated upstream of the gas turbine engine to generate a supply of compressed air;
heating the supply of compressed air in a recuperator with exhaust of the fueled engine to form a heated supply of compressed air;
providing a thermal storage medium downstream of the recuperator, the thermal storage medium configured to be repeatedly thermally chargeable and dischargeable;
providing a pathway; the pathway configured to allow for the heated supply of compressed air to selectively bypass the thermal storage medium to form bypassed air;
thermally charging the thermal storage medium and heating at least a portion of the heated supply of compressed air with heat from the thermal storage medium to form thermal storage air; and,
injecting injection air into the gas turbine engine upstream of the combustor while the gas turbine engine is operational, the injection air comprising the thermal storage air and any bypassed air;
wherein the pathway is further configured to allow parts of each of the exhaust of the fueled engine and the supply of compressed air to selectively bypass the recuperator.
2. The method of claim 1 , wherein the fueled engine also drives a generator to generate electrical power.
3. The method of claim 1 , wherein a heating input to the thermal storage medium is electricity.
4. The method of claim 1 , wherein the heat to charge the thermal storage medium is steam from the gas turbine power plant.
5. The method of claim 1 , wherein the pathway is further configured to allow a part of at least one of the exhaust of the fueled engine and the supply of compressed air to selectively bypass the recuperator.
6. A method of operating a compressed air and thermal energy storage system at a gas turbine power plant, the gas turbine power plant comprising a compressor, a combustor, and turbine, the method comprising:
operating a multistage auxiliary compressor by way of a fueled engine to generate a supply of compressed air;
using a recuperator to heat the supply of compressed air with exhaust of the fueled engine to form heated recuperator air;
providing a thermal storage medium directly downstream of the recuperator, the thermal storage medium configured to be repeatedly thermally chargeable and dischargeable;
configuring the thermal storage medium to heat the heated recuperator air received directly from the recuperator to form thermal storage air;
providing a selectable bypass path to allow for the heated recuperator air to selectively bypass the thermal storage medium;
using the selectable bypass path to cause at least a portion of the heated recuperator air to bypass the thermal storage medium to form bypass air;
injecting injection air into a gas turbine engine upstream of the combustor while the gas turbine engine is operational, the injection air comprising the bypass air and any thermal storage air.
7. The method of claim 6 , wherein the thermal storage medium comprises a tank and a pump.
8. The method of claim 6 , wherein the thermal storage medium is stored at a first location and is thermally charged at a second location disparate from the first location.
9. A method of operating a compressed air and thermal energy storage system at a gas turbine power plant comprising:
operating a multistage auxiliary compressor by way of a fueled engine to generate a supply of compressed air;
heating at least a portion of the supply of compressed air in a recuperator with exhaust of the fueled engine to form a heated supply of compressed air;
providing a thermal storage medium directly downstream of the recuperator, the thermal storage medium configured to be repeatedly thermally chargeable and dischargeable;
providing a pathway; the pathway configured to allow for the heated supply of compressed air to selectively bypass the thermal storage medium to form bypassed air;
thermally charging the thermal storage medium and heating at least a portion of the heated supply of compressed air received directly from the recuperator with heat from the thermal storage medium to form thermal storage air; and,
injecting injection air into a gas turbine engine while the gas turbine engine is operational, the injection air comprising the thermal storage air and any bypassed air;
wherein, a compressor discharge bypass valve is usable to selectively cause at least a part of the supply of compressed air to bypass the recuperator.