Exhaust gas diverter for divided volute turbocharger of internal combustion engine

• US 5,146,754 A
• Filed: 02/08/1991
• Issued: 09/15/1992
• Est. Priority Date: 02/08/1991
• Status: Expired due to Fees

• Current Assignee: Jacobs Brake Technology Corporation
• Original Assignee: Jacobs Brake Technology Corporation
• Inventors: Meistrick, Zdenek S., Jain, Adish, Pitzi, Vincent J.
• Primary Examiner(s): KOCZO JR, MICHAEL
• Application Number:
  US07/652,652
• Time in Patent Office: 585 Days
• Field of Search: 60/602, 137/625.41, 137/625.47, 137/625.48, 415/151
• US Class Current: 60/602
• CPC Class Codes: F02B 37/025 Multiple scrolls or multiple gas passages guiding the gas to the pump drive
• CPC Class Codes: F02B 37/22 by varying cross-section of exhaust passages or air passages , e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits F02B37/24 takes precedence
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A diverter for a divided volute turbocharger has a rotatable diverter member in one volute passageway of the turbocharger. The diverter member is rotatable between a first position in which the flow of gas through the associated volute passageway is unimpeded by the diverter member, and a second position in which the diverter member blocks the associated volute passageway and causes the gas from that passageway to flow through an interconnection passageway into the other volute passageway. If desired, the diverter member may block the interconnection passageway while the diverter member is in the first position.

Claims

1. A divided volute turbocharger diverter disposed between the exhaust manifold of an internal combustion engine and the turbine of the turbocharger comprising:

first and second volute passageways;

an interconnection passageway interconnecting said first and second volute passageways; and

a diverter member disposed in only said first of said first and second volute passageways, said diverter member being rotatable about an axis between (1) a first position in which said diverter member leaves said first volute passageway substantially unobstructed and substantially closes said interconnection passageway, thereby allowing exhaust gas to flow from said exhaust manifold to said turbine via both of said first and second volute passageways, and (2) a second position in which said diverter member blocks said first volute passageway downstream from said interconnection passageway and opens said interconnection passageway so that gas from said exhaust manifold in said first volute passageway is diverted from said first volute passageway through said interconnection passageway into said second volute passageway and is thereby added to the gas flowing from said exhaust manifold to said turbine via said second volute passageway.

3. The apparatus defined in claim 1 wherein said diverter member comprises:

a first end member disposed adjacent a first side wall of said first volute passageway;

a second end member disposed adjacent an opposite second side wall of said first volute passageway, said first and second end members being substantially concentric with said axis; and

a gate member extending between said first and second end members adjacent one side of the peripheries of said first and second end members.

4. The apparatus defined in claim 3 wherein when said diverter member is in said first position, said gate member is substantially parallel to the flow of gas in said first volute passageway but out of that flow adjacent a third side wall of said first volute passageway, and when said diverter member is in said second position, said gate member extends completely across said first volute passageway in order to block the flow of gas in said first volute passageway.

2. The apparatus defined in claim wherein said axis is transverse to the flow of gas in said first volute passageway when said diverter member is in said first position.

5. A divided volute turbocharger diverter comprising:

first and second volute passageways;

an interconnection passageway interconnecting said first and second volute passageways; and

a diverter member disposed in said first volute passageway, said diverter member being rotatable about an axis between a first position in which said diverter member leaves said first volute passageway substantially unobstructed, and a second position in which said diverter member blocks said first volute passageway downstream from said interconnection passageway so that gas from said first volute passageway flows through said interconnection passageway into said second volute passageway, wherein said diverter member comprises;

a first end member disposed adjacent a first side wall of said first volute passageway;

a second end member disposed adjacent an opposite second side wall of said first volute passageway, said first and second end members being substantially concentric with said axis; and

a gate member extending between said first and second end members adjacent one side of the peripheries of said first and second end members, wherein said interconnection passageway is connected to said first volute passageway via a first aperture formed in said first side wall of said first volute passageway, wherein said first end member has a second aperture which registers with said first aperture when said diverter member is in said second position, and wherein said first end member blocks said first aperture when said diverter member is in said first position.