Supersonic vapor compression and heat rejection cycle
View Patent ↗Method and apparatus for cooling a fuel cell stack. The cooling system uses vaporization cooling of the fuel stack and supersonic vapor compression of the vaporized coolant to significantly increase the temperature and pressure of the liquid coolant flowing through a heat exchanger. By increasing the heat rejection temperature of the coolant delivered to the heat exchanger, the heat transfer area of the heat exchanger can be reduced and the mass flow rate of coolant can also be reduced. The increased fluid pressure is used to circulate the coolant through the cooling system, thereby eliminating the circulation pump associated with conventional systems.
1. A system for heat transfer comprising:
a heat source having a coolant circulating through a coolant path;
a first heat exchanger;
a first fluid pathway providing fluid communication between an outlet of said heat source coolant path and an inlet to said first heat exchanger;
a second fluid pathway providing fluid communication between an outlet of said first heat exchanger and an inlet of said heat source coolant path;
said coolant flowing through said first and second fluid pathways such that a portion of said coolant flowing through said heat source coolant path vaporizes as a result of heat transferred from said heat source;
means for separating a vapor stream from said coolant discharged from said heat source coolant path; and
vapor compression means for accelerating said vapor stream to supersonic velocity and directing a liquid stream from said second fluid pathway into contact with said supersonic vapor stream for causing compression of said vapor, resulting in a high temperature, high pressure liquid coolant that flows directly into said inlet of said heat exchanger and through said first heat exchanger for rejecting heat to a heat sink and circulating said coolant through said system.
2. The heat transfer system of claim 1 , further comprising a means for splitting said liquid stream from said liquid coolant in said second fluid pathway.
3. The heat transfer system of claim 1 further comprising an intermediate heat exchanger having an inlet receiving said liquid stream from said separator means and an outlet in fluid communication with said liquid inlet of said nozzle/ejector unit.
4. The heat transfer system of claim 1 further comprising an upstream heat exchanger having an inlet in fluid communication with said outlet of said nozzle/ejector unit and an outlet in fluid communication with said inlet of said first heat exchanger.
5. The heat transfer system of claim 4 wherein heat rejected from said upstream heat exchanger is used to heat said vapor stream prior to delivery of said vapor stream to said vapor inlet of said nozzle/ejector unit.
6. The heat transfer system of claim 4 further comprising a pressure regulator valve disposed in said first fluid pathway between said outlet of said upstream heat exchanger and said inlet of said first heat exchanger.
7. The heat transfer system of claim 1 further comprising a pressure regulator valve disposed in said second fluid pathway between first heat exchanger and said heat source.
8. The heat transfer system of claim 1 further comprising an additional heat exchanger having an inlet in fluid communication with an outlet of said separator means and an outlet in fluid communication with said liquid inlet of said nozzle/ejector unit.
9. The heat transfer system of claim 1 further comprising a pump disposed in said second fluid pathway between said first heat exchanger and said fuel cell.
10. The heat transfer system of claim 1 wherein said vapor compression means is a nozzle/ejector unit that comprises:
a valve body defining a vapor chamber in fluid communication with said vapor inlet, an expansion chamber, and an acceleration chamber; and
a nozzle member extending into said valve body and including a central flow passage having a first end in fluid communication with said liquid inlet and a second end defining said liquid nozzle, said liquid nozzle is oriented to discharge a liquid jet into said acceleration chamber of said valve body;
said vapor nozzle is defined by a restricted area formed between said valve body and said nozzle member, said vapor nozzle is located between said vapor chamber and said expansion chamber such that said vapor stream is drawn through said vapor nozzle from said vapor chamber and accelerated to supersonic velocity due to expansion of said vapor in said expansion chamber.
11. The heat transfer system of claim 10 wherein said supersonic vapor stream surrounds and impinges on said liquid jet and acts to accelerate said liquid jet to a subsonic velocity.
12. The heat transfer system of claim 1 wherein said heat source is a fuel cell.