Cascaded recompression closed brayton cycle system
View Patent ↗The present disclosure is directed to a cascaded recompression closed Brayton cycle (CRCBC) system and method of operation thereof, where the CRCBC system includes a compressor for compressing the system fluid, a separator for generating fluid feed streams for each of the system's turbines, and separate segments of a heater that heat the fluid feed streams to different feed temperatures for the system's turbines. Fluid exiting each turbine is used to preheat the fluid to the turbine. In an embodiment, the amount of heat extracted is determined by operational costs.
1. A method of operating a cascaded recompression closed Brayton cycle system, comprising:
providing a first turbine feed stream to a first turbine operating at a first turbine operating temperature;
expanding the first turbine feed stream to form a first turbine discharge stream;
preheating the first turbine feed stream with the first turbine discharge stream in a first recuperator;
providing a second turbine feed stream to a second turbine operating at a second turbine operating temperature;
expanding the second turbine feed stream to form a second turbine discharge stream;
preheating the second turbine feed stream with the second turbine discharge stream in a second recuperator; and
combining the first turbine discharge stream and the second turbine discharge stream to form a compressor feed stream;
splitting the compressor feed stream to form a first compressor feed stream and a second compressor feed stream;
providing the first compressor feed stream to a first compressor where the first compressor feed stream is compressed to form a first compressor discharge stream, and
providing the second compressor feed stream to a second compressor where the second compressor feed stream is compressed to form a second compressor discharge stream;
combining the first and second compressor discharge streams to for a compressor discharge; and
splitting the compressor discharge to form the first and second turbine feed streams.
2. The method of claim 1 , further comprising:
heating the first compressor feed stream and the second compressor feed stream with one or more heaters after preheating the first compressor feed stream and the second compressor feed stream.
3. The method of claim 2 , wherein heating is by a single heater.
4. The method of claim 1 , further comprising: heating the first compressor discharge stream with the compressor feed stream.
5. The method of claim 1 , further comprising:
providing a third turbine feed stream to a third turbine operating at a third turbine operating temperature;
expanding the third turbine feed stream to form a third turbine discharge stream; and
preheating the third turbine feed stream with the third turbine discharge stream in a third recuperator.
6. The method of claim 1 , wherein the first turbine operating temperature is greater than the second turbine operating temperature.
7. The claim 6 , wherein the first turbine operating temperature is greater than the second turbine operating temperature, which is greater than the third turbine operating temperature.
8. The method of claim 1 , further comprising:
driving a shaft driven by the first and second turbines, wherein the shaft is coupled to a power generation unit.