Turbocharger having divided housing with integral valve

• US 20090000296A1
• Filed: 06/29/2007
• Published: 01/01/2009
• Est. Priority Date: 06/29/2007
• Status: Abandoned Application

• Current Assignee: Caterpillar Incorporated
• Original Assignee: Caterpillar Incorporated
• Inventors: Reisdorf, Paul William, Pierpont, David Andrew
• Application Number:
  US11/819,780
• Publication Number:
  US 20090000296A1
• Time in Patent Office: Days
• US Class Current: 60/602
• CPC Class Codes: F01D 17/145 by means of valves, e.g. for steam turbines valves in general F16K
• CPC Class Codes: F01D 17/165 for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line F01D17/167 takes precedence
• CPC Class Codes: F01D 9/026 Scrolls for radial machines or engines
• CPC Class Codes: F01N 13/107 More than one exhaust manifold or exhaust collector
• 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

A turbocharger is provided having a turbine wheel and a housing configured to at least partially enclose the turbine wheel. The housing may have a first turbine volute including a first inlet and a second turbine volute having a second inlet. The first and second volutes may be configured to communicate a first and second fluid flow with the turbine wheel. The housing may also have a wall member axially separating the first and second turbine volutes. In addition, the housing may have a valve configured to selectively allow fluid in the first inlet to communicate with fluid in the second inlet.

Claims

1. A turbocharger, comprising:

a turbine wheel; and

a housing configured to at least partially enclose the turbine wheel and having;

a first turbine volute having a first inlet and configured to communicate a first fluid flow with the turbine wheel;

a second turbine volute having a second inlet and configured to communicate a second fluid flow with the turbine wheel;

a wall member axially separating the first and second turbine volutes; and

a valve configured to selectively allow fluid in the first inlet to communicate with fluid in the second inlet.

2. The turbocharger of claim 1, wherein the first volute has a smaller cross-sectional area than the second volute, and the first inlet has a smaller cross-sectional area than the second inlet.

3. The turbocharger of claim 2, wherein the housing further includes a first plurality of annularly disposed vane members associated with at least one of the first or second turbine volutes.

4. The turbocharger of claim 3, wherein the first plurality of annularly disposed vane members is associated with the first turbine volute and the housing further includes a second plurality of annularly disposed vane members associated with the second turbine volute.

5. The turbocharger of claim 2, further including a pressure sensor configured to sense a parameter indicative of a pressure of the exhaust flowing through the first inlet.

6. The turbocharger of claim 5, further including a controller configured to adjust the valve in response to the sensed exhaust pressure.

7. The turbocharger of claim 2, further including a flow sensor configured to sense a parameter indicative of a flow of the exhaust flowing through the first inlet.

8. The turbocharger of claim 7, further including a controller configured to adjust the valve in response to the sensed exhaust flow.

9. A method of operating a turbocharger, comprising:

simultaneously receiving a plurality of exhaust flows into the turbocharger at separate axially offset locations; and

selectively allowing the exhaust flows to communicate with each other upon entering the turbine.

10. The method of claim 9, wherein the exhaust flows have different flow rates or pressures.

11. The method of claim 10, further including sensing a flow rate or pressure of one of the exhaust flows and selectively allowing the plurality of exhaust flows to communicate with each other based on the sensed flow rate or pressure.

12. The method of claim 11, further including simultaneously and radially redirecting both of the first and second flows of exhaust at a plurality of finite annular locations.

13. The method of claim 12, wherein the annular locations are spaced substantially equally about the periphery of a turbine wheel.

14. A power system, comprising:

a power source having a plurality of combustion chambers and being configured to produce a power output and a flow of exhaust gases;

a first exhaust passageway associated with at least a first of the plurality of combustion chambers;

a second exhaust passageway associated with at least a second of the plurality of combustion chambers;

an exhaust gas recirculation loop configured to direct exhaust gas to an intake of the power source; and

a turbocharger in fluid communication with the first and second exhaust passageways, the turbocharger including;

a turbine wheel; and

a housing configured to at least partially enclose the turbine wheel and having;

a first turbine volute having a first inlet and configured to fluidly communicate exhaust with the turbine wheel;

a second turbine volute having a second inlet and configured to fluidly communicate exhaust with the turbine wheel;

a wall member axially separating the first and second turbine volutes; and

a valve configured to selectively allow exhaust in the first inlet to communicate with exhaust in the second inlet.

15. The power system of claim 14, wherein the first volute has a smaller cross-sectional area than the second volute, and the first inlet has a smaller cross-sectional area than the second inlet.

16. The power system of claim 15, wherein the first exhaust passageway is fluidly connected to the exhaust gas recirculation loop.

17. The power system of claim 16, further including a pressure sensor or flow rate sensor configured to sense a parameter indicative of a pressure of the exhaust flowing through the first inlet.

18. The power system of claim 17, further including a controller configured to adjust the valve in response to the sensed exhaust pressure or flow rate.

19. The power system of claim 18, wherein the housing further including a first plurality of annularly disposed vane members associated with at least one of the first and second turbine volutes.

20. The power system of claim 19, wherein the first plurality of annularly disposed vane members is associated with the first turbine volute and the housing further includes a second plurality of annularly disposed vane members associated with the second turbine volute.