Variable geometry turbine

• US 10,570,812 B2
• Filed: 10/09/2015
• Issued: 02/25/2020
• Est. Priority Date: 10/10/2014
• Status: Active Grant

• Current Assignee: Cummins Limited (Cummins Incorporated)
• Original Assignee: Cummins Limited (Cummins Incorporated)
• Inventors: Hill, Lisa Jane, Parker, John F., Bywater, John
• Primary Examiner(s): Laurenzi, Mark A
• Assistant Examiner(s): Kebea, Jessica L
• Application Number:
  US15/518,089
• Publication Number:
  US 20180252152A1
• Time in Patent Office: 1,600 Days
• CPC Class Codes: F01D 17/143 the shiftable member being a wall, or part thereof of a radial diffuser
• CPC Class Codes: F02B 37/183 Arrangements of bypass valves or actuators therefor
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A variable geometry turbine having a turbine wheel, an inlet passageway, a movable wall member being moveable axially to vary the width of the inlet passageway, an annular seal being mounted to the movable wall member or an adjacent housing member to provide a seal between adjacent surfaces of the movable wall member and housing member respectively, wherein a bypass passage is provided in the other of said movable wall member or housing member, extending from an inlet bypass port to an outlet bypass port, said ports being spaced from each other and provided in said adjacent surface of said other of the movable wall member or housing member, arranged such that as the movable wall member moves axially, the annular seal moves axially relative to the ports to vary the flow that may pass from a region of the cavity inboard of the seal, through the bypass passage.

Claims

1. A variable geometry turbine comprising:

a turbine wheel supported in a housing for rotation about a turbine axis;

an annular primary inlet passageway extending radially inwards towards the turbine wheel, the primary inlet passageway being defined between a surface of a radial wall of a moveable wall member and a surface of a facing wall of the housing;

the moveable wall member being mounted within an annular cavity provided within the housing, the movable wall member being moveable axially to vary the width of the primary inlet passageway;

an annular seal being mounted to one of the movable wall member and an adjacent housing member to provide a seal between adjacent surfaces of the movable wall member and adjacent housing member respectively;

wherein a bypass passage is provided in the other of said movable wall member and adjacent housing member, the bypass passage extending from an inlet bypass port to an outlet bypass port, said inlet and outlet bypass ports being axially spaced from each other and provided in said adjacent surface of said other of the movable wall member and adjacent housing member;

a secondary inlet passageway fluidly connecting a region of the cavity outboard of the seal to the turbine wheel such that flow in the secondary inlet passageway bypasses at least a portion of the primary inlet passageway;

the bypass passage and the annular seal being arranged such that as the movable wall member moves axially, the annular seal moves axially relative to the inlet and outlet bypass ports so as to vary the extent of flow that may pass from a region of the cavity inboard of the seal, through the bypass passage to the secondary inlet passageway.

2. The variable geometry turbine according to claim 1 wherein the movable wall member is axially movable relative to the facing wall of the housing, between first and second configurations, wherein in the first configuration the seal is positioned relative to the inlet and outlet bypass ports such that flow may pass from the region of the cavity inboard of the seal to the secondary inlet passageway, via the bypass passage and in the second configuration the seal is positioned relative to the inlet and outlet bypass ports such that flow is substantially prevented from passing from the region of the cavity inboard of the seal to the secondary inlet passageway, via the bypass passage.

3. The variable geometry turbine according to claim 2 wherein when the movable wall member is in the first configuration, the movable wall member is in a first position relative to the facing wall of the housing.

4. The variable geometry turbine according to claim 3 wherein when the movable wall member is in the first position, the seal is provided at least partially outboard of the inlet bypass port such that it does not cover the inlet bypass port or only partially covers the inlet bypass port.

5. The variable geometry turbine according to claim 3 wherein when the movable wall member is in the first position, the seal is provided at least partially inboard of the outlet bypass port such that it does not cover the outlet bypass port or only partly covers an inboard portion of the outlet bypass port.

6. The variable geometry turbine according to claim 3 wherein when the movable wall member is in the first position, the seal is disposed axially between the inlet and outlet bypass ports.

7. The variable geometry turbine according to claim 1 wherein the inlet and outlet bypass ports are axially separated by a section of said other of said movable wall member and said adjacent housing member.

8. The variable geometry turbine according to claim 1 wherein the outlet bypass port has a cross-sectional area that is the same, or greater than, the cross-sectional area of the inlet bypass port.

9. The variable geometry turbine according to claim 2 wherein when the movable wall member is in the second configuration, the movable wall member is in a second position relative to the facing wall of the housing.

10. The variable geometry turbine according to claim 1 wherein the bypass passage forms a passage that is enclosed between the inlet and outlet ports.

11. The variable geometry turbine according to claim 1 wherein the bypass passage comprises an inlet passage that fluidly connects the inlet bypass port to a bypass chamber and an outlet passage that fluidly connects the bypass chamber to the outlet bypass port.

12. The variable geometry turbine according to claim 1 wherein the seal is mounted to the movable wall member, with the bypass passage provided in said adjacent housing member, the inlet and outlet bypass ports being provided in said adjacent surface of the adjacent housing member.

13. The variable geometry turbine according to claim 1 wherein the seal is mounted to the adjacent housing member, with the bypass passage provided in the movable wall member, the inlet and outlet bypass ports being provided in said adjacent surface of the movable wall member.

14. The variable geometry turbine according to claim 1 wherein the adjacent housing member comprises an axially extending annular sleeve.

15. The variable geometry turbine according to claim 1 wherein the bypass passage forms a first bypass feature, wherein a second bypass feature, defining a bypass flow path, is provided in said other of said moveable wall member and said adjacent housing member, and is arranged such that as the movable wall member moves axially, the annular seal moves axially relative to the second bypass feature so as to vary the extent of flow that may pass from the region of the cavity inboard of the seal, through the bypass flow path to the secondary inlet passageway.

16. The variable geometry turbine according to claim 15 wherein the second bypass feature comprises a slot or recess, provided in said other of said movable wall member and said adjacent housing member, that defines said bypass flow path.

17. The variable geometry turbine according to claim 16 wherein the movable wall member is axially movable relative to the facing wall of the housing, between third and fourth configurations, wherein in the third configuration the seal is positioned relative to the second bypass feature such that flow may pass from a region of the cavity inboard of the seal to the secondary inlet passageway, via the second bypass flow path and in the fourth configuration the seal is positioned relative to the second bypass feature such that flow is substantially prevented from passing from the region of the cavity inboard of the seal to the secondary inlet passageway, via the second bypass flow path.

18. The variable geometry turbine according to claim 1 wherein a particulate filter is provided in the bypass passage such that flow passing through the bypass passage passes through the particulate filter, with the particulate filter being contacted by particulate matter flowing through the particulate filter.

19. The turbocharger comprising a variable geometry turbine according to claim 1 and a compressor comprising a housing defining an inlet and an outlet, and a chamber between the inlet and outlet, within which an impeller wheel is rotatably mounted such that rotation of the impeller wheel compresses air received through the inlet and passes the compressed air to the outlet, wherein the turbine wheel of the turbine is coupled to the impeller wheel so as to drivably rotate the impeller wheel.

20. A method of operating an engine system comprising an internal combustion engine and a turbocharger wherein the turbocharger comprises a variable geometry turbine according to claim 1 and a compressor comprising a housing defining an inlet and an outlet, and a chamber between the inlet and outlet, within which an impeller wheel is rotatably mounted such that rotation of the impeller wheel compresses air received through the inlet and passes the compressed air to the outlet, wherein the turbine wheel of the turbine is coupled to the impeller wheel so as to drivably rotate the impeller wheel and the turbocharger is arranged such that exhaust gas from the internal combustion engine drivably rotates the turbine wheel of the turbine, wherein the movable wall member is moved between first and second configurations when the engine system is operated in an engine braking mode, a thermal regeneration mode or an exhaust gas heating mode.