Variable turbine geometry assembly

Patent metadata

Field	Value
Publication number	US-2023175414-A1
Application number	US-202117542791-A
Country	US
Kind code	A1
Filing date	Dec 6, 2021
Priority date	Dec 6, 2021
Publication date	Jun 8, 2023
Grant date	—

Abstract

A variable turbine geometry assembly includes an adjustment ring extending along and rotatable about an axis, at least one vane lever coupled to the adjustment ring, and at least one vane coupled to the at least one vane lever. The variable turbine geometry assembly also includes a biasing member coupled to the adjustment ring at a first circumferential location on the adjustment ring and coupled to the adjustment ring at a second circumferential location on the adjustment ring. The biasing member extends from the first circumferential location to the second circumferential location. The biasing member is operably in contact with the at least one vane lever between the first circumferential location and the second circumferential location to bias the at least one vane lever toward the adjustment ring and to reduce vibration between the adjustment ring and the at least one vane lever.

First claim

1 . A variable turbine geometry assembly for controlling flow of exhaust gas to a turbine wheel of a turbocharger, said variable turbine geometry assembly comprising:
an adjustment ring extending along and rotatable about an axis; at least one vane lever coupled to said adjustment ring; at least one vane coupled to said at least one vane lever, with said at least one vane moveable with respect to said adjustment ring when said adjustment ring rotates about said axis; and a biasing member,
coupled to said adjustment ring at a first circumferential location on said adjustment ring,
coupled to said adjustment ring at a second circumferential location different from said first circumferential location on said adjustment ring,
extending from said first circumferential location on said adjustment ring to said second circumferential location on said adjustment ring, and
operably in contact with said at least one vane lever between said first circumferential location and said second circumferential location to bias said at least one vane lever toward said adjustment ring and to reduce vibration between said adjustment ring and said at least one vane lever.

2 . The variable turbine geometry assembly as set forth in claim 1 , wherein said biasing member is in direct contact with said at least one vane lever.

3 . The variable turbine geometry assembly as set forth in claim 1 , wherein said biasing member extends from said first circumferential location to said second circumferential location circumferentially about a majority of said adjustment ring.

4 . The variable turbine geometry assembly as set forth in claim 1 , wherein said biasing member includes at least one planar portion extending parallel to said adjustment ring and at least one contact portion extending axially away from said at least one planar portion toward said at least one vane lever, said at least one contact portion operably in contact with said at least one vane lever.

5 . The variable turbine geometry assembly as set forth in claim 4 , wherein said at least one contact portion is disposed between an adjacent pair of said planar portions.

6 . The variable turbine geometry assembly as set forth in claim 4 , wherein said at least one contact portion is generally U-shaped.

7 . The variable turbine geometry assembly as set forth in claim 1 , wherein said biasing member is coupled to said adjustment ring at a third circumferential location on said adjustment ring.

8 . The variable turbine geometry assembly as set forth in claim 1 , wherein said at least one vane lever is further defined as a plurality of vane levers, wherein said at least one vane is further defined as a plurality of vanes, and wherein said biasing member is operably in contact with at least two of said vane levers.

9 . The variable turbine geometry assembly as set forth in claim 1 , wherein said at least one vane lever is further defined as a plurality of vane levers, wherein said at least one vane is further defined as a plurality of vanes, and wherein said biasing member is operably in contact with at least three of said vane levers.

10 . The variable turbine geometry assembly as set forth in claim 1 , wherein said variable turbine geometry assembly further comprises an adjustment projection coupled to said adjustment ring and extending axially away from said adjustment ring, and wherein said adjustment projection is disposed circumferentially between said first circumferential location and said second circumferential location.

11 . The variable turbine geometry assembly as set forth in claim 1 , wherein said biasing member is further defined as a wire spring.

12 . The variable turbine geometry assembly as set forth in claim 1 , wherein said at least one vane lever has a contact surface facing away from said adjustment ring, and wherein said biasing member is operably in contact with said contact surface to reduce vibration between said adjustment ring and said at least one vane lever.

13 . The variable turbine geometry assembly as set forth in claim 12 , wherein said contact surface of said at least one vane lever is indented axially into said at least one vane lever to seat said biasing member.

14 . The variable turbine geometry assembly as set forth in claim 12 , wherein said biasing member includes at least one planar portion extending parallel to said adjustment ring and at least one contact portion extending axially away from said at least one planar portion toward said at least one vane lever, said at least one contact portion of said biasing member operably in contact with said contact surface of said at least one vane lever.

15 . A turbocharger comprising said variable turbine geometry assembly as set forth in claim 1 and further comprising,
a shaft extending along said axis between a first shaft end and a second shaft end spaced from said first shaft end along said axis;
a turbine wheel coupled to said first shaft end of said shaft;
a compressor wheel coupled to said second shaft end of said shaft; and
a turbine housing defining a turbine housing interior, with said turbine wheel disposed in said turbine housing interior.

16 . A variable turbine geometry assembly for controlling flow of exhaust gas to a turbine wheel of a turbocharger, said variable turbine geometry assembly comprising:
an adjustment ring extending along and rotatable about an axis; at least one vane lever coupled to said adjustment ring, said at least one vane lever having,
a first lever end coupled to said adjustment ring,
a second lever end defining a pin aperture,
an inner lever surface facing said adjustment ring and extending parallel to said adjustment ring, and
an axial stop extending axially away from said inner lever surface toward said adjustment ring and configured to limit axial movement of said at least one vane lever,
a pin disposed in said pin aperture defined by said second lever end of said at least one lever; at least one vane coupled to said pin, with said at least one vane moveable with respect to said adjustment ring when said adjustment ring rotates about said axis; and a biasing member coupled to said adjustment ring and operably in contact with said at least one vane lever to bias said at least one vane lever toward said adjustment ring and to reduce vibration between said adjustment ring and said at least one vane lever.

17 . The variable turbine geometry assembly as set forth in claim 16 , wherein said at least one vane lever has a contact surface facing away from said adjustment ring, and wherein said biasing member is operably in contact with said contact surface.

18 . The variable turbine geometry assembly as set forth in claim 17 , wherein said contact surface of said at least one vane lever is indented axially into said at least one vane lever to seat said biasing member.

19 . The variable turbine geometry assembly as set forth in claim 16 , wherein said axial stop has a first stop surface facing said adjustment ring, a second stop surface facing said axis, and a third stop surface opposite said first stop surface facing away from said axis.

20 . A variable turbine geometry assembly for controlling flow of exhaust gas to a turbine wheel of a turbocharger, said variable turbine geometry assembly comprising:
an adjustment ring extending along and rotatable about a first axis; at least one vane lever coupled to said adjustment ring; and at least one vane coupled to said at least one vane lever, with said at least one vane moveable with resp

Assignees

• Borgwarner Inc

Inventors

• Cavagnaro Augustine
• Morgan Elias
• Williams Greg
• Kennedy Donald Michael
• Hastings Sean
• Grabowska David George
• King Matthew

Classifications

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F01D17/16 Primary

  by means of nozzle vanes · CPC title

• F02B39/00 Primary

  Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00 · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F02B37/24

  by using pumps or turbines with adjustable guide vanes · CPC title