Transcritical turbine and method of operation

• US 6,644,062 B1
• Filed: 10/15/2002
• Issued: 11/11/2003
• Est. Priority Date: 10/15/2002
• Status: Expired due to Term

• Current Assignee: Energent Incorporated (Rodan Energy Solutions Inc.)
• Original Assignee: Energent Incorporated (Rodan Energy Solutions Inc.)
• Inventors: Hays, Lance G.
• Primary Examiner(s): DOERRLER, WILLIAM CHARLES
• Application Number:
  US10/270,468
• Time in Patent Office: 392 Days
• Field of Search: 624/01, 624/02, 624/98, 624/67, 62/87, 621/16
• US Class Current: 62/402
• CPC Class Codes: F01D 15/08 Adaptations for driving, or combinations with, pumps
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: F25B 1/10 with multi-stage compression with cascade operation F25B7/00
• CPC Class Codes: F25B 11/02 as expanders F25B9/06 takes precedence
• CPC Class Codes: F25B 2309/061 with cycle highest pressure above the supercritical pressure
• CPC Class Codes: F25B 2400/0401 for the compressor
• CPC Class Codes: F25B 2400/12 Inflammable refrigerants
• CPC Class Codes: F25B 9/008 the refrigerant being carbon dioxide

Abstract

A process employing a rotary axial turbine, and a nozzle, that includes providing a working fluid expansible from a characteristic supercritical region into the wet region, expanding the fluid from said supercritical region into the wet region via the nozzle and turbine blades, and providing an output shaft driven by the turbine.

Claims

1. A process employing a rotary axial turbine having rotor blades, and a nozzle, that includes

a) providing a working fluid expansible from a characteristic supercritical region into the wet region,

b) expanding said fluid from said supercritical region into said wet region via said nozzle and turbine blades,

c) and providing an output shaft driven by the turbine,

d) the nozzle operated to produce condensation droplets,

e) and collecting a substantial fraction of the said condensation droplets on the axial flow structure of the turbine, said structure including concave blade surfaces and a shroud extending about tips defined by the blades, the bulk of the liquid leaving the turbine rotor with a swirl path extending about and lengthwise of the turbine axis.

2. The process of claim 1 which is employed in a refrigeration system.

3. The process of claim 1 which is employed in a heat pump system.

4. The process of claim 1 including providing a compressor operating to compress said fluid prior to said expanding, the compressor receiving rotary input via said shaft.

5. The process of claim 4 wherein the compressor is operated to increase the working fluid pressure, thereby reducing the power required to increase the working fluid pressure in a subsequent compression stage, prior to said expanding.

6. The process of claim 1 including directing a stream of liquid formed by said collected droplets away from the axial turbine structure so as to avoid a second contact with said structure that would otherwise result in energy losses.

7. The process of claim 1 including providing an electric generator driven by said shaft.

8. The process of claim 1 wherein the working fluid includes carbon dioxide.

9. The process of claim 1 wherein the working fluid includes one of the following:

a) isobutane

b) propane

c) butane

d) ammonia.

19. The process of claim 1 wherein the bulk of the droplets are in sub-micron size range, said droplets directed to flow with a fluid gas phase through the turbine transferring force to axial flow structure defined by the turbine.

10. The method of operating an axial flow turbine having rotor blades rotating at high velocity about an axis, and employing a working fluid capable of two-phase flow, that includes

a) vaporizing said fluid

b) compressing said vaporized fluid to a supercritical state, in a turbine driven boost compressor stage and in a subsequent main, compressor stage,

c) cooling the compressed vaporized fluid while maintaining it in said supercritical state,

d) providing and operating a nozzle to receive and expand said compressed vaporized fluid to a pressure and temperature in the wet region of the fluid characterized by formation of liquid phase droplets of the fluid in a two-phase flow from the nozzle, the bulk of the droplets being less than 1 micron in cross section,

e) directing said two-phase flow toward the turbine blades whereby the flow is turned in the spaces between the blades and directed to flow axially of the turbine rotor as well as outwardly away from said axis, reducing the swirl of the flow leaving the blades, and operable to produce torque transferable to the rotor to act in the direction of rotor rotation,

f) and subsequently vaporizing said flow that leaves the blades pursuant to step a).

11. The method of claim 10 wherein said fluid consists of one or more of the following:

i) carbon dioxide

ii) isobutane

iii) propane

iv) butane

v) ammonia.

12. The method of claim 10 including providing a shroud to extend about said blades and against which a portion of the flow is centrifuged.

13. The method of claim 10 including providing an evaporator in which said step a) is carried out, and providing an auxiliary liquid or gas stream passed to the evaporator to transfer heat to the working fluid for evaporating same.

14. The method of claim 10 including providing a heat exchanger in which said step c) is carried out, and providing an auxiliary liquid or gas stream passed to the heat exchanger to cool the compressed working fluid also passed to the heat exchanger.

15. The method of claim 13 including providing a heat exchanger in which said step c) is carried out, and providing an auxiliary liquid or gas stream passed to the heat exchanger to cool the compressed working fluid also passed to the heat exchanger.

16. An axial flow turbine with rotor blades to receive a two-phase flow of fluid, that comprises:

a) an expansion nozzle contoured to expand the high pressure, supercritical fluid to a lower pressure in the wet region, producing a high velocity directed flow of gas and sub-micron liquid droplets, or of supersaturated

b) axial flow blades, attached to a rotor, directed to receive the high velocity flow and turn it, generating torque on the rotor,

c) surfaces oriented to receive liquid from the turned flow and direct it away from the moving rotor,

d) an exit duct to remove the gas and liquid flow from surfaces and from the moving rotor,

e) and a shaft attached to the rotor to transfer the generated torque to a load,

f) the turbine rotor having an overall diameter less than 1.5 inches, and an operating angular velocity in excess of 90,000 RPM.

17. The turbine of claim 16 wherein the turbine has a stationary body within which said rotor and nozzles are located.

18. The turbine of claim 17 including a rotary compressor in said body and coupled to said shaft.