Rotary turbine bypass valve

Patent metadata

Field	Value
Publication number	US-11536192-B2
Application number	US-201816639869-A
Country	US
Kind code	B2
Filing date	Aug 22, 2018
Priority date	Aug 22, 2017
Publication date	Dec 27, 2022
Grant date	Dec 27, 2022

Abstract

A rotary turbine bypass valve comprises a valve chamber positioned at a junction of an inlet port, an outlet port and a bypass port, the inlet port configured for fluid communication with a flow of exhaust gas from an engine, the outlet port configured for fluid communication with an inlet of a turbine, and the bypass port configured for fluid communication with an exhaust aftertreatment device; and a valve rotor supported for rotation, about a valve axis, within the valve chamber. The valve rotor is rotatable about the valve axis between a first position in which the valve rotor permits gas flow through the bypass port and a second position in which the valve rotor blocks gas flow through the bypass port. The valve rotor is eccentric such that it includes a seal portion which is a portion of the valve rotor within the valve chamber which is furthest radially spaced from the valve axis; and as the valve rotor moves from the first position to the second position the seal portion moves towards the bypass port such that the radial separation between the valve rotor and the bypass port decreases to a minimum when the valve rotor is in the second position in which the seal portion is adjacent the bypass port.

First claim

The invention claimed is:

1. A rotary turbine bypass valve comprising:
a valve chamber positioned at a junction of an inlet port, an outlet port and a bypass port, the inlet port configured for fluid communication with a flow of exhaust gas from an engine, the outlet port configured for fluid communication with an inlet of a turbine, and the bypass port configured for fluid communication with an exhaust aftertreatment device; and
a valve rotor supported for rotation, about a valve axis, within the valve chamber;
wherein the valve rotor is rotatable about the valve axis between a first position in which the valve rotor permits gas flow through the bypass port and a second position in which the valve rotor blocks gas flow through the bypass port;
wherein the valve rotor is eccentric such that it includes a seal portion which is a portion of the valve rotor within the valve chamber which is furthest radially spaced from the valve axis; and as the valve rotor moves from the first position to the second position the seal portion moves towards the bypass port such that the radial separation between the valve rotor and the bypass port decreases to a minimum when the valve rotor is in the second position in which the seal portion is adjacent the bypass port;
wherein the seal portion comprises a rotor seal feature sized and shaped to cooperate with the bypass port to plug the bypass port when the valve rotor is in the second position; and
wherein the rotor seal feature comprises a raised sealing face which has a shape corresponding to that of an opening of the bypass port, the raised sealing face plugging the bypass port when the valve rotor is in the second position.

2. A valve according to claim 1 , wherein the valve chamber is defined by a housing, and the valve rotor comprises at least one spindle, the or each spindle being supported by the housing such that the or each spindle lies along the valve axis, and such that the valve rotor is rotatable relative to the housing about the or each spindle.

3. A valve according to claim 1 , wherein the valve rotor comprises a recess, said recess defining at least a portion of a flow passage between the inlet port and outlet port when the valve rotor is in the second, position.

4. A valve according to claim 1 , wherein the turbine forms part of a turbocharger.

5. A valve according to claim 1 wherein a portion of a wall defining the valve chamber includes an abradable material, such that, when the valve rotor is in the second position, the valve rotor contacts the abradable material to form a seal therewith.

6. A valve according to claim 5 wherein the abradable material is located adjacent the bypass port.

7. A valve according to either claim 5 , wherein the abradable material is located between the bypass port and the outlet port.

8. A valve according to claim 1 , wherein the valve rotor comprises an abradable material which contacts a wall of the valve chamber when the valve rotor is in the second position to form a seal.

9. A valve according to claim 8 , wherein the seal portion of the valve rotor comprises said abradable material of the valve rotor.

10. A valve according to claim 8 , wherein the valve rotor comprises two separate regions of abradable material, a first region of abradable material located on a first side of the bypass port when the valve rotor is in the second position, and a second region located on a second side of the bypass port when the valve rotor is in the second position.

11. An engine arrangement comprising an engine, a turbine and a valve according to claim 1 .

Assignees

• Cummins Ltd

Inventors

• Daniels Robin
• Williamson Gareth
• Deacon Ross
• Al-Kazaz Laith
• Morton Thomas
• Parry Christopher
• Goodyear Richard
• Holden Mark R
• Keating Jon-Luke
• Ali Waqas
• Bywater John
• Roberts Thomas

Classifications

• F02B37/183 Primary

  Arrangements of bypass valves or actuators therefor · CPC title

• F16K11/085

  with cylindrical plug · CPC title

• F16K11/0853

  having all the connecting conduits situated in a single plane perpendicular to the axis of the plug · CPC title

• F16K5/184

  with the plugs or parts of the plugs mechanically pressing the seals against the housing · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title