Rotatable diverter valve

Patent metadata

Field	Value
Publication number	US-9926840-B2
Application number	US-201515548573-A
Country	US
Kind code	B2
Filing date	Feb 3, 2015
Priority date	Feb 3, 2015
Publication date	Mar 27, 2018
Grant date	Mar 27, 2018

Abstract

A turbine ( 32 ) section of a turbocharger ( 30 ) includes a turbine wheel ( 37 ) disposed in a turbine housing ( 33 ), the turbine housing ( 33 ) defining a gas inlet ( 34 ), a volute configured to direct gas from the inlet ( 34 ) to the turbine ( 32 ) wheel, and a gas outlet. A rotary diverter valve ( 100, 200 ) is disposed in the gas inlet ( 34 ) upstream of the volute, and provides three modes of controlling exhaust gas flow about the turbocharger ( 30 ).

First claim

What is claimed is:

1. A cylindrical rotary valve configured to control fluid flow through a fluid passage, the valve comprising
a first end,
a second end that is opposed to the first end,
a side surface that extends between the first end and the second end,
a first inlet opening formed in the side surface,
a first outlet opening formed in the side surface,
a first valve passage that connects the first inlet opening to the first outlet opening,
a second inlet opening formed in the side surface,
a second outlet opening formed in the side surface, and
a second valve passage that connects the second inlet opening to the second outlet opening,

wherein
the second valve passage is separate from the first valve passage,
the first inlet opening, the first outlet opening, and the second inlet opening are each disposed between the first end and a mid portion of the valve, and
the second outlet opening is disposed between the mid portion and the second end.

2. The valve of claim 1 wherein the first inlet opening and the first outlet opening are on opposed sides of the valve.

3. The valve of claim 1 , wherein the first inlet opening is generally axially aligned with, and circumferentially spaced apart from, the second inlet opening.

4. The valve of claim 1 wherein the second inlet opening is circumferentially spaced apart from the second outlet opening.

5. The valve of claim 1 wherein the valve comprises
a third inlet opening formed in the side surface,
a third outlet opening formed in the side surface, and
a third passage that connects the third inlet opening to the third outlet opening,
wherein the third inlet opening and the third outlet opening are disposed between the first end and the mid portion of the valve.

6. The valve of claim 1 wherein at least one of the first inlet opening and the second inlet opening is generally rectangular in shape.

7. A turbocharger comprising
a turbine section including a turbine housing and turbine wheel disposed in the turbine housing, the turbine housing defining a gas inlet, a volute configured to direct gas from the inlet to the turbine wheel, and a gas outlet; and
a rotary valve disposed in the gas inlet in such a manner that a rotational axis of the valve extends transverse to a direction of gas flow through the inlet, the valve comprising:
a first end,
a second end that is opposed to the first end,
a side surface that extends between the first end and the second end,
a longitudinal axis that extends through the first and second ends and coincides with the rotational axis of the valve,
a first inlet opening formed in the side surface,
a first outlet opening formed in the side surface,
a first valve passage that connects the first inlet opening to the first outlet opening,
a second inlet opening formed in the side surface,
a second outlet opening formed in the side surface, and
a second passage that connects the second inlet opening to the second outlet opening,

wherein
the second passage is separate from the first passage, and
the first inlet opening, the first outlet opening, and the second inlet opening are each positioned so as to communicate with the gas inlet for certain rotational orientations of the valve, and the second outlet opening is positioned so as to be able to communicate with the gas outlet for certain rotational orientations of the valve.

8. The turbocharger of claim 7 , wherein the valve is configured to provide three modes of operation of the turbocharger, including
a fully open mode that corresponds to a first rotational orientation of the valve, in which all the exhaust gas flows through the valve to the turbine wheel,
a wastegated mode that corresponds to a second rotational orientation of the valve, in which a portion of the exhaust gas is redirected around the turbine wheel to the exhaust outlet, and
a backpressured mode that corresponds to a third rotational orientation of the valve, in which the exhaust inlet is at least partially obstructed.

9. The turbocharger of claim 8 , wherein when the valve is in the first rotational orientation, the first inlet opening is aligned with the gas inlet and faces toward an upstream direction relative to a direction of gas flow, the first outlet opening is aligned with the gas inlet and faces toward a downstream direction relative to a direction of gas flow, and the second inlet opening is obstructed.

10. The turbocharger of claim 8 , wherein when the valve is in the second rotational orientation, the second inlet opening is aligned with the gas inlet and faces toward an upstream direction relative to a direction of gas flow, the second outlet opening is aligned with the gas outlet, and the first inlet opening is at least partially obstructed.

11. The turbocharger of claim 7 , further comprising an actuator that is connected to the valve first end and configured to control a rotational position of the valve about the longitudinal axis.

12. The turbocharger of claim 7 wherein the first inlet opening and the first outlet opening are on opposed sides of the valve.

13. The turbocharger of claim 7 , wherein the first inlet opening is generally axially aligned with, and circumferentially spaced apart from, the second inlet opening.

14. The turbocharger of claim 7 wherein the second inlet opening is circumferentially and axially spaced apart from the second outlet opening.

15. The turbocharger of claim 7 wherein the valve comprises
a third inlet opening formed in the side surface,
a third outlet opening formed in the side surface,
a third passage that connects the third inlet opening to the third outlet opening,
wherein the third inlet opening and the third outlet opening are disposed between the first end and the mid portion of the valve.

Assignees

• Borgwarner Inc

Inventors

• Mawer James
• Shoghi Kiumars
• Birnie Steve
• Rylance Sean

Classifications

• F16K11/085

  with cylindrical plug · CPC title

• F02B37/183 Primary

  Arrangements of bypass valves or actuators therefor · CPC title

• F16K11/076

  with sealing faces shaped as surfaces of solids of revolution · CPC title

• F02M26/10

  having means to increase the pressure difference between the exhaust and intake system, e.g. venturis, variable geometry turbines, check valves using pressure pulsations or throttles in the air intake or exhaust system · CPC title

• F02M26/05

  High pressure loops, i.e. wherein recirculated exhaust gas is taken out from the exhaust system upstream of the turbine and reintroduced into the intake system downstream of the compressor · CPC title