Reverse brayton cycle with bladeless turbo compressor for automotive environmental cooling

Patent metadata

Field	Value
Publication number	US-9464638-B2
Application number	US-201313875188-A
Country	US
Kind code	B2
Filing date	May 1, 2013
Priority date	May 1, 2012
Publication date	Oct 11, 2016
Grant date	Oct 11, 2016

Abstract

An automotive cabin cooling system uses a bladeless turbocompressor driven by automobile engine exhaust to compress incoming ambient air. The compressed air is directed to an intercooler where it is cooled and then to another bladeless turbine used as an expander where the air cools as it expands and is directed to the cabin interior. Excess energy may be captured by an alternator couple to the expander turbine. The system employs no chemical refrigerant and may be further modified to include another intercooler on the output of the expander turbine to isolate the cooled cabin environment.

First claim

What is claimed is:

1. An apparatus for cooling an automotive cabin, comprising:
a bladeless turbocompressor including a first turbine receiving engine combustion gases which drive a first bladeless impeller coupled to a second bladeless impeller of a compressor, the compressor receiving air which is then compressed by the second bladeless impeller;
an intercooler coupled to receive and cool the compressed air from the compressor; and
a second turbine receiving the cooled, compressed air from the intercooler, the second turbine having a third bladeless impeller uncoupled from the first bladeless impeller and the second bladeless impeller and driven by the cooled, compressed air, the cooled, compressed air expanding and becoming further cooled thereby.

2. The apparatus of claim 1 , wherein each of the first, second and third bladeless impellers comprises a plurality of planar discs spaced apart in a stack on a common shaft having fluid passages cut therethrough near the central shaft.

3. The apparatus of claim 2 , wherein spacing between the plurality of planar discs enables laminar fluid flow of the air to develop beginning at a boundary layer between the air and planar surfaces of the planar discs.

4. The apparatus of claim 2 , wherein spacing between the plurality of planar discs is such that choked flow does not occur.

5. The apparatus of claim 1 , wherein the first bladeless impeller is coupled to a second bladeless impeller by a common shaft.

6. The apparatus of claim 1 , wherein the air received by the compressor is ram air directed in from outside the vehicle.

7. The apparatus of claim 1 , further comprising a heat exchanger receiving the air from the second turbine and heating it by cooling automotive cabin air passed over it, the heat exchanger then returning the air to the compressor in a closed cycle.

8. The apparatus of claim 1 , further comprising an alternator coupled to third bladeless impellor of the second turbine for generating electrical power.

9. The apparatus of claim 1 , further comprising a drier for reducing moisture content from the air prior to being received by the compressor.

10. The apparatus of claim 9 , further comprising a recuperator for reducing temperature of the air prior to being received by the compressor and raising the temperature of the air after being expanded by the second turbine.

11. A method for cooling an automotive cabin, comprising:
receiving engine combustion gases in a first turbine of a bladeless turbocompressor to drive a first bladeless impeller coupled to a second bladeless impeller of a compressor;
receiving and compressing air in the compressor by the second bladeless impeller;
receiving and cooling the compressed air from the compressor with an intercooler; and
receiving and expanding the cooled, compressed air from the intercooler in a second turbine, the second turbine having a third bladeless impeller uncoupled from the first bladeless impeller and the second bladeless impeller and driven by the cooled, compressed air, the cooled, compressed air expanding and becoming further cooled thereby.

12. The method of claim 11 , wherein each of the first, second and third bladeless impellers comprises a plurality of planar discs spaced apart in a stack on a common shaft having fluid passages cut therethrough near the central shaft.

13. The method of claim 12 , wherein spacing between the plurality of planar discs enables laminar fluid flow of the air to develop beginning at a boundary layer between the air and planar surfaces of the planar discs.

14. The method of claim 12 , wherein spacing between the plurality of planar discs is such that choked flow does not occur.

15. The method of claim 11 , wherein the first bladeless impeller is coupled to a second bladeless impeller by a common shaft.

16. The method of claim 11 , wherein the air received by the compressor is ram air directed in from outside the vehicle.

17. The method of claim 11 , further comprising receiving and heating the air from the second turbine by cooling automotive cabin air passed over it in a heat exchanger and then returning the air to the compressor in a closed cycle.

18. The method of claim 11 , further comprising generating electrical power from an alternator coupled to third bladeless impellor of the second turbine.

19. The method of claim 11 , further comprising reducing moisture content from the air in a drier prior to being received by the compressor.

20. The method of claim 19 , further comprising reducing temperature of the air in a recuperator prior to being received by the compressor and raising the temperature of the air after being expanded by the second turbine.

21. An apparatus for cooling an automotive cabin, comprising:
a first bladeless means for driving a second bladeless means from received engine combustion gases, the second bladeless means for compressing received air driven by the first bladeless means;
a cooling means for cooling the compressed air from the compressor; and
a third bladeless means for expanding the received cooled, compressed air from the cooling means, the third bladeless means uncoupled from the first bladeless means and the second bladeless means and driven by the cooled, compressed air, the cooled, compressed air expanding and becoming further cooled thereby.

Assignees

• Cepeda-Rizo Juan
• Ganapathi Gani B
• California Inst Of Techn

Inventors

• Cepeda-Rizo Juan
• Ganapathi Gani B

Classifications

• F04D29/58 Primary

  Cooling (of machines or engines in general F01P); Heating; Diminishing heat transfer {(for the motor of air-pump units F04D25/082; cooling of shafts or bearings F04D29/04)} · CPC title

• F25B9/004 Primary

  the refrigerant being air · CPC title

• B60H1/3204

  using compression (B60H1/3233 takes precedence) · CPC title