Dual volute turbocharger and system including the same

Patent metadata

Field	Value
Publication number	US-11028765-B2
Application number	US-202016790087-A
Country	US
Kind code	B2
Filing date	Feb 13, 2020
Priority date	Feb 15, 2019
Publication date	Jun 8, 2021
Grant date	Jun 8, 2021

Abstract

A system includes a dual volute turbocharger and a controller. The dual volute turbocharger includes a turbine housing. The turbine housing includes a wall, a valve seat, and an interior surface defining a turbine housing interior, a first volute, a second volute, and a turbine housing outlet. The dual volute turbocharger also includes at least one valve member engageable with at least one of the valve seat and the wall of the turbine housing. The at least one valve member and the wall of the turbine housing collectively define a first cross-sectional flow area. The at least one valve member and the valve seat of the turbine housing collectively define a second cross-sectional flow area. The controller is adapted to control the at least one valve member to have an area ratio constant operating range according to a brake-specific fuel consumption of the internal combustion engine.

First claim

What is claimed is:

1. A system comprising:
a dual volute turbocharger for receiving exhaust gas from an internal combustion engine and for delivering compressed air to the internal combustion engine, said dual volute turbocharger comprising,
a turbine housing comprising,
an interior surface defining,
a turbine housing interior adapted to receive a turbine wheel,
a first volute adapted for fluid communication with the internal combustion engine and said turbine housing interior for delivering exhaust gas from the internal combustion engine to said turbine housing interior,
a second volute adapted for fluid communication with the internal combustion engine and said turbine housing interior for delivering exhaust gas from the internal combustion engine to said turbine housing interior, and
a turbine housing outlet in fluid communication with said turbine housing interior for discharging exhaust gas from said turbine housing interior,

a wall separating said first volute from said second volute, and
a valve seat, and

at least one valve member engageable with at least one of said wall and said valve seat of said turbine housing for controlling exhaust gas flow from said first and second volutes to said turbine housing interior, with said at least one valve member and said wall of said turbine housing collectively defining a first cross-sectional flow area and said at least one valve member and said valve seat of said turbine housing collectively defining a second cross-sectional flow area; and

a controller adapted to control the at least one valve member to have an area ratio constant (C AR ) operating range according to a brake-specific fuel consumption (BSFC) of the internal combustion engine, with the C AR defined by the equation:
C AR =first cross-sectional flow area/(ρ power *second cross-sectional flow area), where ρ power is the power density of the internal combustion engine in kW/L.

2. The system as set forth in claim 1 , wherein said at least one valve member is further defined as a first valve member and a second valve member, wherein said wall and said valve seat collectively define a valve cavity, wherein said first valve member and said wall of said turbine housing collectively define said first cross-sectional flow area and said valve seat of said turbine housing and at least one of said first and second valve members collectively define said second cross-sectional flow area, and wherein said dual volute turbocharger further comprises,
a valve assembly for controlling exhaust gas flow from said first and second volutes to said turbine housing interior, said valve assembly comprising,
the first valve member engageable with said wall of said turbine housing and disposed about and extending along an axis between a first end adapted to be proximal said wall of said turbine housing and a second end spaced from said first end and adapted to be distal said wall of said turbine housing, with said first valve member movable between a first position where said first valve member is disposed in said valve cavity and adjacent said wall of said turbine housing for restricting exhaust gas from flowing between said first and second volutes, a second position where said first valve member is disposed in said valve cavity and spaced from said wall of said turbine housing for allowing exhaust gas to flow between said first and second volutes, and a third position where said first valve member is disposed outside of said valve cavity for allowing exhaust gas from said first and second volutes to bypass said turbine housing interior,
the second valve member engageable with said valve seat and coupled to said first valve member, with said second valve member movable between a first position where said second valve member is engaged with said valve seat of said turbine housing for restricting exhaust gas from said first and second volutes from bypassing said turbine housing interior, and a second position where said second valve member is disengaged with said valve seat of said turbine housing for allowing exhaust gas from said first and second volutes to bypass said turbine housing interior, and
a valve shaft coupled to at least one of said first and second valve members for moving said first valve member between said first, second, and third positions and said second valve member between said first and second positions.

3. The system as set forth in claim 2 , wherein said first valve member defines a valve interior between said first and seconds ends, and wherein said valve assembly further comprises a biasing member disposed in said valve interior, with said biasing member configured to bias said first valve member into one of said first and second positions when said second valve member is in said first position.

4. The system as set forth in claim 2 , wherein said first valve member has an outer contour configured to reduce wear of said valve assembly.

5. The system as set forth in claim 4 , wherein said outer contour of said first valve member includes a protrusion configured to be engageable with said wall of said turbine housing when said first valve member is in said first position.

6. The system as set forth in claim 3 , wherein said second valve member comprises a base coupled to and disposed about said valve shaft and a projection extending from said base and about said valve shaft into said valve interior.

7. The system as set forth in claim 6 , wherein said biasing member is disposed about said projection of said second valve member.

8. The system as set forth in claim 6 , wherein said second valve member further comprises a lip extending radially from said projection with respect to said axis.

9. The system as set forth in claim 8 , wherein said biasing member is disposed between and in contact with said lip of said second valve member and said second end of said first valve member.

10. The system as set forth in claim 2 , wherein said valve assembly includes an actuator operably coupled to said valve shaft for moving said valve shaft to move said first valve member between said first, second, and third positions and said second valve member between said first and second positions.

11. The system as set forth in claim 1 , wherein said at least one valve member is further defined as a first valve member and a second valve member, wherein said first valve member and said wall of said turbine housing collectively define said first cross-sectional flow area and said second valve member and said valve seat of said turbine housing collectively define said second cross-sectional flow area, and wherein said dual volute turbocharger further comprises,
a first valve assembly for controlling exhaust gas flow between said first and second volutes, said first valve assembly comprising,
the first valve member of the first valve assembly engageable with said wall of said turbine housing and disposed about and extending along an axis between a first end adapted to be proximal said wall of said turbine housing and a second end spaced from said first end and adapted to be distal said wall of said turbine housing, with said first valve member of the first valve assembly movable between a first position where said first valve member of the first valve assembly is adjacent said wall of said turbine housing for restricting exhaust gas from flowing between said first and second volutes, and a second position where said first valve member of the first valve assembly is spaced from said wall of said turbine housing for allowing exhaust gas to flow between said first and second volutes, and
a first valve shaft coupled to said first valve member of the first valve assembly for moving said first valve member o

Assignees

• Borgwarner Inc

Inventors

• Cola Michael Daniel
• Weiske Sascha
• Sonigra Mehul

Classifications

• F01D9/026

  Scrolls for radial machines or engines · CPC title

• F16K11/04

  comprising only lift valves · CPC title

• F02D23/00

  Controlling engines characterised by their being supercharged · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F02B37/025 Primary

  Multiple scrolls or multiple gas passages guiding the gas to the pump drive · CPC title