Rotary valve

Patent metadata

Field	Value
Publication number	US-11549600-B2
Application number	US-201917293170-A
Country	US
Kind code	B2
Filing date	Nov 11, 2019
Priority date	Nov 13, 2018
Publication date	Jan 10, 2023
Grant date	Jan 10, 2023

Abstract

A rotary turbine bypass valve comprises a valve chamber and a valve rotor. The chamber is positioned at a junction of an inlet port, an outlet port and a bypass port. The inlet port is configured to receive exhaust gas, the outlet port is configured to fluidly communicate with a turbine inlet, and the bypass port is configured to fluidly communicate with an exhaust aftertreatment device.
The rotor comprises a first and second recess, the first recess defining a primary flow passage, the second recess defining a secondary flow passage. The rotor is rotatable between a first position in which the rotor substantially blocks exhaust gas flow through the bypass port and a second position in which the rotor permits such. The secondary flow passage is configured to selectively permit fluid communication between the inlet port and the bypass port when the primary flow passage is partially blocked.

First claim

What is claimed:

1. A rotary turbine bypass valve for an engine arrangement, the 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 to fluidly communicate with a flow of exhaust gas from an engine, the outlet port configured to fluidly communicate with an inlet of a turbine, and the bypass port configured to fluidly communicate with an exhaust aftertreatment device; and
a valve rotor supported for rotation, about a valve axis, within the valve chamber, the valve rotor comprising a first recess and a second recess, the first recess defining at least part of a primary flow passage, the second recess defining at least part of a secondary flow passage;
wherein the valve rotor is rotatable about the valve axis between a first position in which the valve rotor substantially blocks exhaust gas flow through the bypass port and a second position in which the valve rotor permits exhaust gas flow through the bypass port;
wherein the secondary flow passage is configured to selectively permit fluid communication between the inlet port and the bypass port when the primary flow passage is at least partially blocked;
wherein the second recess is one of two second recesses forming part of a secondary arrangement, and the first recess is one of two first recesses forming part of a primary arrangement; and
wherein the second recesses are smaller than the first recesses.

2. The rotary turbine bypass valve claim 1 , wherein at least one of the second recesses spans at least a portion of an outer circumference of the valve rotor.

3. The rotary turbine bypass valve of claim 1 , wherein at least one of the second recesses opposes a corresponding first recess.

4. The rotary turbine bypass valve of claim 1 , wherein at least one of the first and at least one of the second recesses are separated by a barrier.

5. The rotary turbine bypass valve of claim 4 , wherein the barrier defines a chord of the valve rotor.

6. The rotary turbine bypass valve of claim 1 , wherein the valve rotor is movable about the valve axis to selectively open and close the primary flow passage whilst the secondary flow passage remains open.

7. The rotary turbine bypass valve of claim 1 , wherein the secondary flow passage is configured to selectively provide fluid communication between the inlet port and the bypass port when the primary flow passage is substantially blocked.

8. The rotary turbine bypass valve claim 1 , wherein at least one of the second recesses has a non-uniform depth.

9. The rotary turbine bypass valve of claim 1 , wherein both of the second recesses have substantially the same shape.

10. The rotary turbine bypass valve of claim 1 , wherein the second recesses have substantially the same depths.

11. The rotary turbine bypass valve of claim 1 , wherein the second recesses have different depths.

12. The rotary turbine bypass valve of claim 1 , wherein the second recesses are circumferentially aligned.

13. The rotary turbine bypass valve of claim 1 , wherein the second recesses are circumferentially offset.

14. The rotary turbine bypass valve of claim 1 , wherein the first and/or second arrangements are symmetrically disposed about a length of the valve rotor.

15. The rotary turbine bypass valve according to claim 1 , wherein the turbine forms part of a turbocharger.

16. An engine arrangement comprising an engine, a turbine and the rotary turbine bypass valve according to claim 1 .

17. A method of operating the rotary turbine bypass valve of claim 1 , wherein the rotary turbine bypass valve exhibits the following flow regimes in order as the valve rotor rotates from a position in which the outlet port is substantially blocked, the method comprising:
(i) substantially blocking the outlet port with the valve rotor during a complete turbine bypass regime;
(ii) substantially blocking the inlet port during a braking regime;
(iii) at least partially blocking the primary flow passage during a thermal management regime, wherein during the thermal management regime the secondary flow passage permits fluid communication between the inlet port and the bypass port;
(iv) substantially blocking the bypass port and opening the inlet port and the outlet port during a 100% turbine regime; and
(v) opening the outlet port and at least partially opening the bypass port during a wastegate regime.

18. The method of claim 17 , wherein the rotational position of the valve rotor is adjusted from the position of step (iii) to increase or reduce the extent of the blockage of the primary flow passage to adjust a temperature and/or pressure of the exhaust gas in the inlet port.

Assignees

• Cummins Ltd

Inventors

• Willey Donald E
• Brookes Matthew

Classifications

• F01N2340/06

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

• F01N2240/36

  an exhaust flap · CPC title

• F01N3/021

  by means of filters · CPC title

• F02B37/025

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

• F02D9/06

  Exhaust brakes · CPC title