Exhaust pulse energy divider

• US 9,206,732 B2
• Filed: 02/24/2011
• Issued: 12/08/2015
• Est. Priority Date: 02/26/2010
• Status: Active Grant

• Current Assignee: International Engine Intellectual Property Company, LLC (Volkswagen AG)
• Original Assignee: International Engine Intellectual Property Company, LLC (Volkswagen AG)
• Inventors: Gottemoller, Paul, Zagone, John, Cattani, Luis C, Bartkowicz, Michael D, Burke, Jim
• Primary Examiner(s): Bogue, Jesse
• Assistant Examiner(s): OLSZEWSKI, THOMAS JOHN
• Application Number:
  US13/636,943
• Publication Number:
  US 20130167527A1
• Time in Patent Office: 1,748 Days
• Field of Search: 606/02, 606/15, 606/051, 602/80, 123/568.17, 123/65.E, 415/205, 415/211.1, 415/184, 415/151
• US Class Current: 1/1
• CPC Class Codes: F01D 17/105 by passing part of the fluid
• CPC Class Codes: F01D 9/026 Scrolls for radial machines or engines
• CPC Class Codes: F02B 27/04 in exhaust systems only, e.g. for sucking-off combustion gases
• CPC Class Codes: F02B 37/18 by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
• CPC Class Codes: F02B 37/183 Arrangements of bypass valves or actuators therefor
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: F05D 2240/12 Fluid guiding means, e.g. vanes
• CPC Class Codes: Y10T 137/0536 Highspeed fluid intake means [e.g., jet engine intake]

Abstract

An exhaust gas turbocharger housing (10) for an engine includes a main turbine housing portion (14) and a throat portion (12) defining an exhaust gas passageway (20) that is in upstream fluid communication with the main turbine housing. The exhaust passageway (20) communicates exhaust gases (EG) to the main turbine housing portion (14). A flow divider (22) generally bisects the exhaust gas passageway (20) forming a first inlet passageway (24A) and a second inlet passageway (24B). A flow hole (26) is disposed through the flow divider (22) for permitting the fluid communication of exhaust gas (EG) from the first inlet passageway (24A) to the second inlet passageway (24B).

Claims

1. An exhaust gas turbocharger housing for an engine, comprising:

an undivided main turbine housing portion;

a throat portion defining an exhaust gas passageway in upstream fluid communication with the undivided main turbine housing for communicating exhaust gases to the undivided main turbine housing portion;

a flow divider disposed within the throat portion, which flow divider does not extend into the main turbine housing and which generally bisects the exhaust gas passageway forming a first inlet passageway and a second inlet passageway for communicating exhaust gases to the undivided main turbine housing;

a flow hole through the flow divider for permitting the fluid communication of exhaust gas from the first inlet passageway to the second inlet passageway; and

a single wastegate disposed on one of the first or second inlet passageways and in fluid communication with the atmosphere and one of the first or second inlet passageways.

2. The housing of claim 1 further comprising an inlet surface of the throat portion that is generally transverse to the exhaust gas passageway.

3. The housing of claim 2 wherein the flow divider is generally flush with the inlet surface.

4. A method of wasting exhaust gas in a throat portion of a turbocharger turbine housing, the throat portion defining an exhaust gas passageway for the fluid communication of exhaust gas from an engine to an undivided main turbine housing portion, the method comprising the steps of:

dividing the exhaust gas passageway into a first inlet passageway and a second inlet passageway with a flow divider having a flow opening permitting the fluid communication between the two inlet passageways;

providing a wastegate port in one of the first inlet passageway or the second inlet passageway of the throat portion;

opening the wastegate port disposed in one of the first inlet passageway and the second inlet passageway; and

wasting exhaust gas from both the first inlet passageway and the second inlet passageway, wherein at least a portion of the exhaust gas flows through the flow opening to the wastegate port.

5. The method of claim 4 further comprising providing a single wastegate port on the throat portion.

6. The method of claim 4 further comprising the step of generally aligning the flow opening and the wastegate port along the length of the flow divider.

7. The method of claim 4 further comprising extending the flow divider from an inlet surface of the throat portion, wherein the inlet surface is generally transverse to the exhaust passageway.

8. The method of claim 4 further comprising extending the flow divider to the main turbine housing portion.