Wastegate valve

Patent metadata

Field	Value
Publication number	US-11560832-B2
Application number	US-202017135512-A
Country	US
Kind code	B2
Filing date	Dec 28, 2020
Priority date	Jul 9, 2014
Publication date	Jan 24, 2023
Grant date	Jan 24, 2023

Abstract

A wastegate valve for a bypass path for a turbocharger in an internal combustion engine, the wastegate valve comprises a valve seat defining a plane which is non-orthogonal to the principal flow axis for gases flowing along the bypass path and a valve member pivotable from an open position to a closed position, wherein in the closed position the valve member is seated on the valve seat, and in a fully open position the valve member is positioned to direct gases exiting the bypass path onto a leading face of a catalytic converter monolith for heating the monolith.

First claim

The invention claimed is:

1. An exhaust system for an internal combustion engine, comprising:
a turbocharger having a turbine,
a bypass path arranged to allow exhaust gas to bypass the turbine, the bypass path having an inlet end and an outlet end including a valve seat, the bypass path having walls near the outlet defining a bypass path principal flow axis between the ends, wherein the valve seat defines a plane that is non-orthogonal to the bypass path principal flow axis, an angle between the plane defined by the valve seat and the walls of the bypass path being greater than 90° and up to 135°,
a wastegate valve element,
a chamber, and
a catalytic converter,
wherein the bypass path is selectively closable by the wastegate valve element to prevent exhaust gas flowing from the engine from bypassing the turbocharger and thereby enter the chamber when the wastegate valve element is seated in a closed condition on the valve seat and
wherein the bypass path is selectively openable by the wastegate valve element when the wastegate valve element is in an open condition away from the valve seat to allow exhaust gas flowing from the engine to bypass the turbocharger, exhaust gas exiting the bypass path along the bypass path principal flow axis being diverted by the wastegate valve element along a different flow axis within the chamber to impinge directly upon a leading face of the catalytic converter,
wherein exhaust gas exiting the turbine is directed along a second principal flow axis to impinge directly upon the leading face of the catalytic converter,
wherein a plane defined by the wastegate valve element is parallel to the second principal flow axis, and
wherein the different flow axis of the diverted gases exiting the outlet end of the bypass path is parallel to the plane defined by the wastegate valve element and the second principal flow axis of the gases exiting the turbine of the turbocharger.

2. The exhaust system as claimed in claim 1 , wherein the wastegate valve element is pivotable, at its fully open position, to an open angle with respect to the plane defined by the valve seat, wherein the angle is from 30° to 70°.

3. The exhaust system as claimed in claim 2 , wherein the open angle is from 36° to 63°.

4. The exhaust system as claimed in claim 3 , wherein the open angle is from 40° to 50°.

5. The exhaust system as claimed in claim 1 , wherein the wastegate valve element is pivotable, at its fully open position, to an open angle of 0° to 60°, with respect to the bypass path principal flow axis.

6. The exhaust system as claimed in claim 5 , wherein the open angle is in a range from 45° to 60°.

7. The exhaust system as claimed in claim 1 , wherein the bypass path is provided, at least in part, by a conduit, the valve seat being provided on a distal end of the conduit.

8. The exhaust system as claimed in claim 7 , wherein the bypass path is arranged to protrude into the chamber.

9. The exhaust system as claimed in claim 1 , wherein the wastegate valve element pivots into or towards a center of the chamber downstream of the bypass path.

10. The exhaust system according to claim 1 , comprising an actuator to open and close the wastegate valve element, wherein the actuator is selected from an electric actuator, a vacuum actuator and a mechanical actuator.

11. The exhaust system according to claim 1 , wherein the plane defined by the valve seat is non-parallel to the leading face of the catalytic converter.

12. The exhaust system as claimed in claim 1 , wherein the turbocharger is a twin scroll turbocharger.

13. The exhaust system as claimed in claim 1 , wherein the angle is in a range from 105° to 120°.

14. The exhaust system as claimed in claim 1 , wherein the angle is 113°.

Assignees

• Jaguar Land Rover Ltd

Inventors

• Albrecht Matthew
• Schlarb Guido

Classifications

• F02B37/183 Primary

  Arrangements of bypass valves or actuators therefor · CPC title

• F01N2340/06

  Arrangement of the exhaust apparatus relative to the turbine of a turbocharger · CPC title

• F01N3/2006

  Periodically heating or cooling catalytic reactors, e.g. at cold starting or overheating (by electrically controlling the supply of combustible mixture or its constituents only F02D41/0235) · CPC title

• F02B37/18

  by bypassing exhaust {from the inlet to the outlet of turbine or to the atmosphere} · CPC title

• F01N3/2892

  Exhaust flow directors or the like, e.g. upstream of catalytic device · CPC title