Supercritical fluid systems
Supercritical fluid systems and aircraft power systems are described. The systems include a compressor, a turbine, and a generator. A primary working fluid flow path has a primary working fluid that passes through the compressor, a separator, the turbine, and back to the compressor. A secondary working fluid flow path having a secondary working fluid that passes through the generator, the compressor, the separator, and back to the generator. The primary working fluid and the secondary working fluid are compressed and mixed within the compressor to form a mixture of the two fluids and the separator separates the mixture of the two fluids to direct the primary working fluid back to the turbine and the secondary working fluid to the generator.
1. A supercritical fluid system comprising:
a compressor;
a turbine operably coupled to the compressor;
a generator operably coupled to the turbine and configured to generate power;
a primary working fluid flow path having a primary working fluid configured to pass through the compressor, a separator, the turbine, and back to the compressor; and
a secondary working fluid flow path having a secondary working fluid configured to pass through the generator, the compressor, the separator, and back to the generator,
wherein the primary working fluid and the secondary working fluid are compressed and mixed within the compressor to form a mixture of the two fluids, and
wherein the separator is configured to separate the primary working fluid from the secondary working fluid from the mixture of the two fluids and direct the primary working fluid back to the turbine along the primary working fluid flow path and the secondary working fluid along the secondary working fluid flow path to the generator.
2. The supercritical fluid system of claim 1 , wherein the secondary working fluid is hydrogen.
3. The supercritical fluid system of claim 1 , wherein the secondary working fluid is helium.
4. The supercritical fluid system of claim 1 , wherein the compressor and the turbine are part of a waste heat recovery system of a gas turbine engine.
5. The supercritical fluid system of claim 1 , wherein the mixture of the two fluids within the compressor has a uniform pressure and a uniform temperature at an outlet of the compressor.
6. The supercritical fluid system of claim 1 , wherein the mixture is generated within the compressor.
7. The supercritical fluid system of claim 1 , wherein the separator is a cyclone separator or a gravity separator.
8. The supercritical fluid system of claim 1 , wherein the separator is a membrane separator.
9. The supercritical fluid system of claim 1 , further comprising a recuperating heat exchanger arranged along the primary working fluid flow path.
10. The supercritical fluid system of claim 1 , wherein the generator includes a rotor, wherein the secondary working fluid flow path passes along the rotor to provide cooling thereto.
11. The supercritical fluid system of claim 10 , wherein the secondary working fluid is configured to prevent entrainment of the primary working fluid around the rotor.
12. The supercritical fluid system of claim 1 , wherein the compressor is a shrouded blade compressor and the secondary working fluid is directed to provide cooling to shrouded blades of the shrouded blade compressor.
13. The supercritical fluid system of claim 1 , wherein the turbine is a shrouded blade turbine and the secondary working fluid is directed to provide cooling to shrouded blades of the shrouded blade turbine.
14. The supercritical fluid system of claim 1 , further comprising a cooling heat exchanger arranged along the secondary working fluid flow path between the separator and the generator.
15. The supercritical fluid system of claim 1 , wherein the compressor, the generator, and the turbine are part of an industrial generator.
16. An aircraft power system comprising:
at least one engine; and
a supercritical fluid system comprising:
a compressor;
a turbine operably coupled to the compressor;
a generator operably coupled to the turbine and configured to generate power;
a primary working fluid flow path having a primary working fluid configured to pass through the compressor, a separator, the turbine, and back to the compressor; and
a secondary working fluid flow path having a secondary working fluid configured to pass through the generator, the compressor, the separator, and back to the generator,
wherein the primary working fluid and the secondary working fluid are compressed and mixed within the compressor to form a mixture of the two fluids, and
wherein the separator is configured to separate the primary working fluid from the secondary working fluid from the mixture of the two fluids and direct the primary working fluid back to the turbine along the primary working fluid flow path and the secondary working fluid along the secondary working fluid flow path to the generator.
17. The aircraft power system of claim 16 , wherein the supercritical fluid system is configured as a waste heat recovery system for the at least one engine.
18. The aircraft power system of claim 16 , wherein the secondary working fluid is hydrogen.
19. The aircraft power system of claim 16 , wherein the secondary working fluid is helium.
20. The aircraft power system of claim 16 , wherein the supercritical fluid system is configured to generate power for the aircraft.