Pumped thermal systems with variable stator pressure ratio control
The present disclosure provides pumped thermal energy storage systems that can be used to store electrical energy. A pumped thermal energy storage system of the present disclosure can store energy by operating as a heat pump or refrigerator, whereby net work input can be used to transfer heat from the cold side to the hot side. A working fluid of the system is capable of efficient heat exchange with heat storage fluids on a hot side of the system and on a cold side of the system. The system can extract energy by operating as a heat engine transferring heat from the hot side to the cold side, which can result in net work output. Systems of the present disclosure can employ solar heating for improved storage efficiency.
1. A system comprising:
a compressor comprising a plurality of adjustable stators, wherein an angle of each stator of the plurality is adjustable relative to the flow of a working fluid through the compressor, wherein a compression ratio across the compressor varies with the angle;
a hot side heat exchanger;
a turbine;
a cold side heat exchanger; and
a fluid path,
wherein the system is configured to operate in a charging mode in which energy is stored in the system and a discharging mode in which energy is discharged from the system, and
wherein the fluid path is configured to circulate the working fluid through, in sequence and in the same direction, the compressor, the hot side heat exchanger, the turbine, and the cold side heat exchanger when the system operates in the charging mode and when the system operates in the discharging mode.
2. The system of claim 1 , wherein the compressor further comprises:
a plurality of inlet guide vanes;
a plurality of rotors; and
a plurality of outlet guide vanes.
3. A system comprising:
a compressor;
a hot side heat exchanger;
a turbine comprising a plurality of adjustable stators, wherein an angle of each stator of the plurality is adjustable relative to the flow of a working fluid through the turbine, wherein an expansion ratio across the turbine varies with the angle;
a cold side heat exchanger; and
a fluid path,
wherein the system is configured to operate in a charging mode in which energy is stored in the system and a discharging mode in which energy is discharged from the system, and
wherein the fluid path is configured to circulate the working fluid through, in sequence and in the same direction, the compressor, the hot side heat exchanger, the turbine, and the cold side heat exchanger when the system operates in the charging mode and when the system operates in the discharging mode.
4. The system of claim 3 , wherein the turbine further comprises:
a plurality of inlet guide vanes;
a plurality of rotors; and
a plurality of outlet guide vanes.
5. A system comprising:
a compressor comprising a first plurality of adjustable stators, wherein a first angle of each stator of the first plurality is adjustable relative to the flow of a working fluid through the compressor, wherein a compression ratio across the compressor varies with the first angle;
a hot side heat exchanger;
a turbine comprising a second plurality of adjustable stators, wherein a second angle of each stator of the second plurality is adjustable relative to the flow of the working fluid through the turbine, wherein an expansion ratio across the turbine varies with the second angle;
a cold side heat exchanger; and
a fluid path,
wherein the system is configured to operate in a charging mode in which energy is stored in the system and a discharging mode in which energy is discharged from the system, and
wherein the fluid path is configured to circulate the working fluid through, in sequence and in the same direction, the compressor, the hot side heat exchanger, the turbine, and the cold side heat exchanger when the system operates in the charging mode and when the system operates in the discharging mode.
6. The system of claim 5 , wherein a first pressure of the working fluid at an outlet of the compressor is equal to a second pressure of the working fluid at an inlet of the turbine.
7. The system of claim 5 , wherein a first pressure of the working fluid at an inlet of the compressor is equal to a second pressure of the working fluid at an outlet of the turbine.
8. The system of claim 5 , wherein the compression ratio across the compressor is equal to the expansion ratio across the turbine.
9. The system of claim 5 , wherein the compression ratio across the compressor differs from the expansion ratio across the turbine by a fixed amount.