Expansion turbine for cryogenic rectification system

• US 5,460,003 A
• Filed: 06/14/1994
• Issued: 10/24/1995
• Est. Priority Date: 06/14/1994
• Status: Expired due to Fees

• Current Assignee: Praxair Technology Incorporated (Linde Plc)
• Original Assignee: Praxair Technology Incorporated (Linde Plc)
• Inventors: Nenov, Neno T.
• Primary Examiner(s): KILNER, CHRISTOPHER B
• Application Number:
  US08/260,272
• Time in Patent Office: 497 Days
• Field of Search: 62/39, 62/36, 62/40, 415/186, 415/191, 415/208.3, 415/211.1
• US Class Current: 62/651
• CPC Class Codes: F01D 15/00 Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
• CPC Class Codes: F01D 9/045 for radial flow machines or engines
• CPC Class Codes: F25B 9/06 using expanders F25B9/10 takes precedence
• CPC Class Codes: F25J 2200/72 Refluxing the column with at least a part of the totally condensed overhead gas
• CPC Class Codes: F25J 2240/02 Expansion of a process fluid in a work-extracting turbine (i.e. isentropic expansion), e.g. of the feed stream
• CPC Class Codes: F25J 2290/10 Mathematical formulae, modeling, plot or curves; Design methods
• CPC Class Codes: F25J 3/04284 using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams F25J3/04333 takes precedence
• CPC Class Codes: F25J 3/04296 Claude expansion, i.e. expanded into the main or high pressure column
• CPC Class Codes: F25J 3/04309 of nitrogen
• CPC Class Codes: F25J 3/04381 using work extraction by mechanical coupling of compression and expansion so-called companders
• CPC Class Codes: F25J 3/044 using a single pressure main column system only F25J3/0446, F25J3/04624, F25J3/04636 take precedence
• CPC Class Codes: F25J 3/04412 in a classical double column flowsheet, i.e. with thermal coupling by a main reboiler-condenser in the bottom of low pressure respectively top of high pressure column
• CPC Class Codes: F25J 3/04866 Construction and layout of air fractionation equipments, e.g. valves, machines F25J5/00 takes precedence
• CPC Class Codes: Y10S 62/91 Expander

Abstract

A turboexpander, particularly suited for use in a cryogenic rectification system, comprises a center housing rotatably supporting an elongated shaft to opposite ends of which are mounted a turbine wheel within a turbine housing and a compressor wheel within a compressor housing or a brake within a load housing. The turbine wheel has circumferentially spaced turbine blades. Process fluid is introduced so as to flow through annular nozzles or guide vanes which encompass the turbine wheel. The guide vanes direct the process fluid through the turbine blades and each extends between a leading edge more distant from the turbine wheel and a trailing edge less distant from the turbine wheel. Each guide vane is substantially uncontoured between its leading edge and the trailing edge and is substantially thicker at the leading edge than at the trailing edge. A thermal shield thermally isolates the turbine housing and the process fluid within the turbine housing from the central housing and the lubricant within said central housing. A labyrinth seal construction along the length of the shaft between the bearings and the turbine housing prevents migration of the lubricant along the shaft into the turbine housing and prevents migration of the process fluid out of the turbine housing along the shaft and into the central housing. Sealing gas may also be provided to the labyrinth seal construction as an additional expedient to prevent migration of the lubricant along the shaft and of the process fluid out of the turbine. Superior performance is achieved by the relative dimensioning of certain components.

Claims

1. A turboexpander capable of producing refrigeration, comprising:

a center housing extending between first and second ends;

a turbine housing attached to said first end of said center housing;

a shaft having a longitudinal axis mounted on said center housing for rotation about said longitudinal axis, said shaft having a first end extending into said turbine housing and a second end supporting a load;

a turbine wheel having an outer periphery mounted on said first end of said shaft and within said turbine housing for rotation with said shaft, said turbine wheel having a plurality of circumferentially spaced turbine blades thereon, each of said turbine blades extending between locations proximate said outer periphery of said turbine wheel and locations proximate said longitudinal axis;

said turbine housing defining inlet means for receiving process fluid at a region distant from said longitudinal axis and for discharging the process fluid toward said turbine blades; and

annular nozzle means intermediate said inlet means and said turbine wheel and encompassing said turbine wheel for directing the process fluid from said inlet means toward and through said turbine blades, said nozzle means including a plurality of guide vanes, each of said guide vanes extending between a leading edge more distant from said turbine wheel and a trailing edge less distant from said turbine wheel, the maximum distance between said trailing edges of said guide vanes and said outer periphery of said turbine wheel being in the range of approximately 1% to 4% of the turbine wheel radius.

2. The turboexpander as set forth in claim 1, wherein the distance between said leading edge and said trailing edge of said guide vanes is a chord and wherein said chord is in the range of approximately 5% to 15% of the turbine wheel diameter.

3. The turboexpander as set forth in claim 2, wherein each of said guide vanes is substantially uncontoured between said leading edge and said trailing edge and has a substantially greater thickness at said leading edge than at said trailing edge.

4. The turboexpander as set forth in claim 3, wherein the thickness of each of said guide vanes at said leading edge is in the range of approximately 0.05 inch to 0.15 inch;

and wherein the thickness of each of said guide vanes at said trailing edge is in the range of approximately 0.01 inch to 0.10 inch.

5. The turboexpander as set forth in claim 1, including:

bearing means on said central housing for rotatably supporting said shaft;

means for delivering lubricant into and away from said bearing means; and

thermal shield means for thermally isolating said turbine housing and the process fluid within said turbine housing from said central housing and the lubricant within said central housing.

6. The turboexpander as set forth in claim 5, including:

labyrinth seal means along the length of said shaft between said bearing means and said turbine housing to prevent migration of the lubricant along said shaft into said turbine housing and to prevent migration of the process fluid out of said turbine housing along said shaft and into said central housing.

7. The turboexpander as set forth in claim 6, including:

means for providing sealing gas to said labyrinth seal means and means for withdrawing sealing gas from said labyrinth seal means as an additional expedient to prevent migration of the lubricant along said shaft into said turbine housing and to prevent migration of the process fluid out of said turbine housing along said shaft and into said central housing.

8. The turboexpander as set forth in claim 1, including:

a compressor housing on said second end of said center housing, said second end of said shaft extending into said compressor housing; and

a compressor wheel mounted on said second end of said shaft and within said compressor housing for rotation with said shaft.

9. The turboexpander as set forth in claim 1, including:

a loading device housing attached to said second end of said center housing, said second end of said shaft extending into said loading device housing.

10. A turboexpander capable of producing refrigeration, comprising:

a center housing extending between first and second ends;

a turbine housing attached to said first end of said center housing;

a shaft having a longitudinal axis mounted on said center housing for rotation about said longitudinal axis, said shaft having a first end extending into said turbine housing and a second end supporting a load;

a turbine wheel having an outer periphery mounted on said first end of said shaft and within said turbine housing for rotation with said shaft, said turbine wheel having a plurality of circumferentially spaced turbine blades thereon, each of said turbine blades extending between locations proximate said outer periphery of said turbine wheel and locations proximate said longitudinal axis;

said turbine housing defining inlet means for receiving process fluid at a region distant from said longitudinal axis and for discharging the process fluid toward said turbine blades; and

annular nozzle means intermediate said inlet means and said turbine wheel and encompassing said turbine wheel for directing the process fluid from said inlet means toward and through said turbine blades, said nozzle means including a plurality of guide vanes, each of said guide vanes extending between a leading edge more distant from said turbine wheel and a trailing edge less distant from said turbine wheel, the distance between said leading edge and said trailing edge being a chord, said chord being in the range of approximately 5% to 15% of the turbine wheel diameter.

11. A system comprising:

(a) a main heat exchanger; and

(b) a turboexpander in fluid communication with said main heat exchanger, wherein said turboexpander includes;

a center housing extending between first and second ends;

a turbine housing attached to said first end of said center housing;

a shaft having a longitudinal axis mounted on said center housing for rotation about said longitudinal axis, said shaft having a first end extending into said turbine housing and a second end supporting a load;

a turbine wheel having an outer periphery mounted on said first end of said shaft and within said turbine housing for rotation with said shaft, said turbine wheel having a plurality of circumferentially spaced turbine blades thereon, each of said turbine blades extending between locations proximate said outer periphery of said turbine wheel and locations proximate said longitudinal axis;

said turbine housing defining inlet means for receiving process fluid at a region distant from said longitudinal axis and for discharging the process fluid toward said turbine blades; and

annular nozzle means intermediate said inlet means and said turbine wheel and encompassing said turbine wheel for directing the process fluid from said inlet means toward and through said turbine blades, said nozzle means including a plurality of guide vanes, each of said guide vanes extending between a leading edge more distant from said turbine wheel and a trailing edge less distant from said turbine wheel, maximum distance between said trailing edges of said guide vanes and said outer periphery of said turbine wheel being in the range of approximately 1% to 4% of the turbine wheel radius.

12. The system as set forth in claim 11, wherein the distance between said leading edge and said trailing edge is a chord and wherein said chord is in the range of approximately 5% to 15% of the turbine wheel diameter.

13. The system as set forth in claim 11, including:

a rectification column system;

means for passing fluid from said turboexpander to said rectification column system; and

means for recovering product from said rectification column system.

14. The system as set forth in claim 13, including:

means for passing waste fluid from said rectification column system to said main heat exchanger; and

means for withdrawing waste fluid from said main heat exchanger.

15. The system at set forth in claim 11, including:

a rectification column system;

means for passing fluid from said main heat exchanger to said rectification column system;

means for recovering product from said rectification column system;

means for passing waste fluid from said rectification column system to said main heat exchanger or said turboexpander; and

means for passing fluid or waste fluid from said turboexpander to said main heat exchanger.

16. The system as set forth in claim 11, including:

a rectification column system located between said main heat exchanger and said turboexpander to receive feed from said main heat exchanger and to send waste fluid to said turboexpander;

means for recovering product from said rectification column system; and

means for passing waste fluid from said turboexpander to said main heat exchanger or said rectification column.

17. A method for producing product by the cryogenic rectification of feed air comprising:

(a) cooling feed air and passing the cooled feed air into a rectification column system;

(b) separating the feed air by cryogenic rectification in the rectification column system into product fluid and into waste fluid;

(c) withdrawing waste fluid from the rectification column system and passing the withdrawn waste fluid to a turboexpander;

(d) operating said turboexapander at 40% to 85% efficiency to expand said waste fluid to generate refrigeration;

(e) passing the expanded waste fluid in indirect heat exchange with feed air to carry out the cooling of step (a); and

(f) recovering product from the rectification column system;

wherein the turboexchanger comprises;

a center housing extending between first and second ends;

a turbine housing attached to said first end of said center housing;

a shaft having a longitudinal axis mounted on said center housing for rotation about said longitudinal axis, said shaft having a first end extending into said turbine housing and a second end supporting a load;

a turbine wheel having an outer periphery mounted on said first end of said shaft and within said turbine housing for rotation with said shaft, said turbine wheel having a plurality of circumferentially spaced turbine blades thereon, each of said turbine blades extending between locations proximate said outer periphery of said turbine wheel and locations proximate said longitudinal axis;

said turbine housing defining inlet means for receiving process fluid at a region distant from said longitudinal axis and for discharging the process fluid toward said turbine blades; and

annular nozzle means intermediate said inlet means and said turbine wheel and encompassing said turbine wheel for directing the process fluid from said inlet means toward and through said turbine blades, said nozzle means including a plurality of guide vanes, each of said guide vanes extending between a leading edge more distant from said turbine wheel and a trailing edge less distant from said turbine wheel, the maximum distance between said trailing edges of said guide vanes and said outer periphery of said turbine wheel being in the range of approximately 1% to 4% of the turbine wheel radius.

20. The method as set forth in claim 17 wherein the distance between said leading edge and said trailing edge of said guide vanes is a chord and wherein said chord is in the range of approximately 5% to 15% of the turbine wheel diameter.

23. The method as set forth in claim 17 wherein said product is nitrogen.

18. A method for producing product by the cryogenic rectification of feed air comprising:

(a) cooling feed air and passing the cooled feed air through a turboexpander;

(b) operating said turboexpander at 40% to 85% efficiency to expand the cooled feed air to generate refrigeration;

(c) passing the feed air into a rectification column system;

(d) separating the feed air by cryogenic rectification in the rectification column system into product fluid and into waste fluid;

(e) withdrawing waste fluid from the rectification column system and passing the waste fluid in indirect heat exchange with feed air to carry out the cooling of step (a); and

(f) recovering product from the rectification column system;

wherein the turboexchanger comprises;

a center housing extending between first and second ends;

a turbine housing attached to said first end of said center housing;

a shaft having a longitudinal axis mounted on said center housing for rotation about said longitudinal axis, said shaft having a first end extending into said turbine housing and a second end supporting a load;

a turbine wheel having an outer periphery mounted on said first end of said shaft and within said turbine housing for rotation with said shaft, said turbine wheel having a plurality of circumferentially spaced turbine blades thereon, each of said turbine blades extending between locations proximate said outer periphery of said turbine wheel and locations proximate said longitudinal axis;

said turbine housing defining inlet means for receiving process fluid at a region distant from said longitudinal axis and for discharging the process fluid toward said turbine blades; and

annular nozzle means intermediate said inlet means and said turbine wheel and encompassing said turbine wheel for directing the process fluid from said inlet means toward and through said turbine blades, said nozzle means including a plurality of guide vanes, each of said guide vanes extending between a leading edge more distant from said turbine wheel and a trailing edge less distant from said turbine wheel, the maximum distance between said trailing edges of said guide vanes and said outer periphery of said turbine wheel being in the range of approximately 1% to 4% of the turbine wheel radius.

21. The method as set forth in claim 18 wherein the distance between said leading edge and said trailing edge of said guide vanes is a chord and wherein said chord is in the range of approximately 5% to 15% of the turbine wheel diameter.

24. The method as set forth in claim 18 wherein said product is nitrogen.

19. A method for producing product by the cryogenic rectification of feed air comprising:

(a) cooling feed air in a main heat exchanger and passing the cooled feed air into either a rectification column system or into a turboexpander operating at 65% to 85% efficiency;

(b) passing the feed air from either the rectification column system and/or the turboexpander opeating at 65% to 85% efficiency to the main heat exchanger;

(c) withdrawing waste fluid from the main heat exchanger; and

(d) recovering product from the rectification column system;

wherein the turboexchanger comprises;

a center housing extending between first and second ends;

a turbine housing attached to said first end of said center housing;

a shaft having a longitudinal axis mounted on said center housing for rotation about said longitudinal axis, said shaft having a first end extending into said turbine housing and a second end supporting a load;

a turbine wheel having an outer periphery mounted on said first end of said shaft and within said turbine housing for rotation with said shaft, said turbine wheel having a plurality of circumferentially spaced turbine blades thereon, each of said turbine blades extending between locations proximate said outer periphery of said turbine wheel and locations proximate said longitudinal axis;

said turbine housing defining inlet means for receiving process fluid at a region distant from said longitudinal axis and for discharging the process fluid toward said turbine blades; and

annular nozzle means intermediate said inlet means and said turbine wheel and encompassing said turbine wheel for directing the process fluid from said inlet means toward and through said turbine blades, said nozzle means including a plurality of guide vanes, each of said guide vanes extending between a leading edge more distant from said turbine wheel and a trailing edge less distant from said turbine wheel, the maximum distance between said trailing edges of said guide vanes and said outer periphery of said turbine wheel being in the range of approximately 1% to 4% of the turbine wheel radius.

22. The method as set forth in claim 19 wherein the distance between said leading edge and said trailing edge of said guide vanes is a chord and wherein said chord is in the range of approximately 5% to 15% of the turbine wheel diameter.

25. The method as set forth in claim 19 wherein said product is one of:

(1) oxygen;

(2) oxygen and nitrogen; and

(3) oxygen, nitrogen and argon.