Internal combustion engine system having a power turbine with a broad efficiency range

• US 7,694,518 B2
• Filed: 08/14/2007
• Issued: 04/13/2010
• Est. Priority Date: 08/14/2007
• Status: Active Grant

• Current Assignee: Deere & Company
• Original Assignee: Deere & Company
• Inventors: Whiting, Todd Mathew, Vuk, Carl Thomas
• Primary Examiner(s): Denion; Thomas E
• Assistant Examiner(s): DAVIS, MARY ALICE
• Application Number:
  US11/838,645
• Publication Number:
  US 20090047121A1
• Time in Patent Office: 973 Days
• Field of Search: 606/02, 415/120, 415/151, 415/156, 415/159, 415/116, 415/184, 415/185, 415/186, 415/205, 415/208.3, 415/208.5, 415/211.1
• US Class Current: 60/602
• CPC Class Codes: F01D 17/148 by means of rotatable members, e.g. butterfly valves
• CPC Class Codes: F01D 9/026 Scrolls for radial machines or engines
• CPC Class Codes: F02B 37/025 Multiple scrolls or multiple gas passages guiding the gas to the pump drive
• CPC Class Codes: F02C 6/12 Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

An engine system incorporating an air breathing, reciprocating internal combustion engine having an inlet for air and an exhaust for products of combustion. A centripetal turbine receives products of the combustion and has a housing in which a turbine wheel is rotatable. The housing has first and second passages leading from the inlet to discrete, approximately 180°, portions of the circumference of the turbine wheel. The passages have fixed vanes adjacent the periphery of the turbine wheel and the angle of the vanes in one of the passages is different than those in the other so as to accommodate different power levels providing optimum approach angles between the gases passing the vanes and the blades of the turbine wheel. Flow through the passages is controlled by a flapper valve to direct it to one or the other or both passages depending upon the load factor for the engine.

Claims

1. A centripetal turbine comprising:

a housing having an inlet for high velocity gases and an outlet;

a turbine wheel rotatable in said housing, said turbine wheel having a plurality of blades extending at least radially inward from the turbine wheel periphery;

said housing having first and second passages leading from the inlet to discrete and separate portions around the periphery of said turbine wheel;

said housing having fixed vanes in said passages adjacent the periphery of said turbine wheel wherein said fixed vanes in said first and second passages have different angles with respect to said turbine housing; and

said housing having a device to selectively permit flow through said first passage, said second passage and both passages.

2. A centripetal turbine as claimed in claim 1, wherein said first and second passages are circumferentially spaced from one another.

3. A centripetal turbine as claimed in claim 2, wherein said first and second passages each occupy about 180°

of the periphery of said turbine wheel.

4. A centripetal turbine as claimed in claim 1, wherein said first and second passages have unequal flow area.

5. A centripetal turbine as claimed in claim 1, wherein said passages are circumferentially spaced around the periphery of said turbine wheel with the first passage being closer to said inlet and the vanes in the first passage have an angle that is closer to the radial direction than the angle of the vanes in the second passage.

6. A centripetal turbine wheel as claimed in claim 1, wherein said device for selectively permitting flow is a flapper valve.

7. A centripetal turbine as claimed in claim 6, wherein said flapper valve comprises a trailing edge pivotal downstream of a leading edge and said flapper valve is pivotal between three positions, one of which blocks flow to the first passage, another of which blocks flow to the second passage and a third position in between the first and second positions to permit flow through both said first and second passages.

8. A centripetal turbine as claimed in claim 1, wherein said selected flow device comprises a rotary valve pivotable about its axis to selectively permit flow through said first passage, said second passage and both passages.

9. A centripetal turbine as claimed in claim 1, wherein said turbine wheel blades have axial outlet portions extending from and connected with the inlet portions said turbine blades.

10. A centripetal turbine as claimed in claim 1, further comprising a load driven by said turbine.

11. A centripetal turbine as claimed in claim 10, wherein said load is a compressor for pressurizing fluid.

12. A centripetal turbine as claimed in claim 11, wherein said load is a generator driven by said turbine.

13. An internal combustion engine system comprising:

an air breathing reciprocating internal combustion engine having an inlet for air and an exhaust for products of combustion;

at least one centripetal turbine receiving products of combustion in the form of high velocity gases from said exhaust, said turbine comprising;

a housing having an inlet receiving said high velocity gases and an outlet;

a turbine wheel rotatable in said housing, said turbine wheel having a plurality of blades extending at least radially inward from the turbine wheel periphery;

said housing having first and second passages leading from the turbine inlet to discrete and separate portions around the periphery of said turbine wheel;

said housing having fixed vanes in said passages adjacent the periphery of said turbine wheel wherein said fixed vanes in said first and second passages have different angles with respect to said turbine housing; and

said housing having a device to selectively permit flow through said first passage, said second passage and both passages.

14. A centripetal turbine as claimed in claim 13, wherein said first and second passages are circumferentially spaced from one another.

15. A centripetal turbine as claimed in claim 14, wherein said first and second passages each occupy about 180°

of the periphery of said turbine wheel.

16. A centripetal turbine as claimed in claim 13, wherein said first and second passages have unequal flow area.

17. A centripetal turbine as claimed in claim 13, wherein said passages are circumferentially spaced around the periphery of said turbine wheel with the first passage being closer to said inlet and the vanes in the first passage have an angle that is closer to the radial direction than the angle of the vanes in the second passage.

18. A centripetal turbine wheel as claimed in claim 13, wherein said device for selectively permitting flow is a flapper valve.

19. A centripetal turbine as claimed in claim 18, wherein said flapper valve comprises a trailing edge pivotal downstream of a leading edge and said flapper valve is pivotal between three positions, one of which blocks flow to the first passage, another of which blocks flow to the second passage and a third position in between the first and second positions to permit flow through both said first and second passages.

20. A centripetal turbine as claimed in claim 13, wherein said selected flow device comprises a rotary valve pivotable about its axis to selectively permit flow through said first passage, said second passage and both passages.

21. A centripetal turbine as claimed in claim 13, wherein said turbine wheel blades have axial outlet portions extending from and connected with the inlet portions said turbine blades.

22. A centripetal turbine as claimed in claim 13, further comprising a load driven by said turbine.

23. A centripetal turbine as claimed in claim 22, wherein said load is a compressor for pressurizing fluid.

24. A centripetal turbine as claimed in claim 22, wherein said load is a generator driven by said turbine.