Variable turbine geometry vane lever

Patent metadata

Field	Value
Publication number	US-10619508-B2
Application number	US-201715803363-A
Country	US
Kind code	B2
Filing date	Nov 3, 2017
Priority date	Nov 3, 2017
Publication date	Apr 14, 2020
Grant date	Apr 14, 2020

Abstract

A variable turbine geometry assembly is provided for controlling flow of exhaust gas to a turbine wheel of a turbocharger. The variable turbine geometry assembly includes a base structure, vanes, vane levers, and an adjustment ring. The vanes are distributed circumferentially around the base structure and are pivotable relative to the base structure to vary an effective inlet area. The vane levers are for pivoting the vanes. The vane levers each include an inner portion coupled to one of the vanes and an outer portion extending from the inner portion. The adjustment ring is selectively rotatable about a central axis to pivot the vanes. The adjustment ring includes apertures that are each associated with and have received therein the outer portion of one of the vane levers. The outer portion of each of the vane levers includes an outer surface that is non-parallel with the central axis.

First claim

What is claimed is:

1. A variable turbine geometry assembly for controlling flow of exhaust gas to a turbine wheel of a turbocharger, the variable turbine geometry assembly comprising:
a base structure;
vanes distributed circumferentially around the base structure and pivotable relative to the base structure to vary an effective inlet area;
vane levers for pivoting the vanes, the vane levers each including an inner portion coupled to one of the vanes and an outer portion extending from the inner portion; and
an adjustment ring that is selectively rotatable about a central axis to pivot the vanes, the adjustment ring including enclosed apertures that are each associated with and have received therein the outer portion of one of the vane levers;
wherein the outer portion of each of the vane levers includes an outermost surface that is non-parallel with the central such that the outer portion tapers towards an outer circumferential surface of the aperture receiving the vane lever to reduce wear and/or cause lower-magnitude impacts between the vane levers and the adjustment ring.

2. The variable turbine geometry assembly of claim 1 , wherein a cross-sectional area of the outer portion of each of the vane levers received in one of the apertures varies moving parallel with the central axis.

3. The variable turbine geometry assembly of claim 1 , wherein the outermost surface of each of the vane levers is tapered relative to the central axis.

4. The variable turbine geometry assembly of claim 1 , wherein the outer circumferential surface of each aperture faces radially inward toward the outermost surface of the vane lever received therein.

5. The variable turbine geometry assembly of claim 4 , wherein the outer circumferential surface of each of the apertures extends parallel with the central axis.

6. The variable turbine geometry assembly of claim 4 , wherein a nominal radial gap is formed between the outer circumferential surface of the aperture and the outermost surface of the vane lever received therein.

7. The variable turbine geometry assembly of claim 4 , wherein the apertures each include a first radially-extending surface and a second radially extending surface that extend radially inward from the outer circumferential surface and that engage, respectively, a first radially-extending surface and a second radially-extending surface of the outer portion of the vane lever received therein.

8. The variable turbine geometry assembly of claim 1 , wherein the inner portion extends radially relative to the central axis, and the outer portion extends axially relative to the central axis.

9. A variable turbine geometry assembly for controlling flow of exhaust gas to a turbine wheel of a turbocharger, the variable turbine geometry assembly comprising:
a base structure;
vanes distributed circumferentially around the base structure and pivotable relative to the base structure to vary an effective inlet area;
vane levers for pivoting the vanes, the vane levers each including an inner portion coupled to one of the vanes and an outer portion extending from the inner portion; and
an adjustment ring that is selectively rotatable about a central axis to pivot the vanes, the adjustment ring including apertures that are each associated with and have received therein the outer portion of one of the vane levers;
wherein the outer portion of each of the vane levers includes an outer surface that is non-parallel with the central axis, wherein the outer surface of each of the vane levers is tapered relative to the central axis, wherein the outer portion of each of the vane levers includes an axial portion that includes the outer surface and that extends axially through the aperture associated therewith, and the outer surface extends at a constant angle over a majority of an axial dimension thereof, the constant angle being a non-zero angle measured relative to the central axis.

10. The variable turbine geometry assembly of claim 9 , wherein the base structure is positioned forward of the inner portion of the vane levers, and the outer surface of each of the vane levers is tapered radially outward moving forward.

11. The variable turbine geometry assembly of claim 10 , wherein the outer surface of each of the vane levers is tapered at a radially outermost region thereof.

12. The variable turbine geometry assembly of claim 9 , wherein the outer surface of each of the vane levers is tapered with a substantially constant profile over a majority of a circumferential dimension thereof.

13. A turbocharger comprising:
a turbine wheel;
a turbine housing containing the turbine wheel and having an inlet and an outlet for exhaust gas to flow, respectively, to and from the turbine wheel; and
a variable turbine geometry assembly comprising:
a base structure;
vanes distributed circumferentially around the base structure and pivotable relative to the base structure to vary an effective inlet area for exhaust gas to flow from the inlet to the turbine wheel;
vane levers for pivoting the vanes, the vane levers each including an inner portion coupled to one of the vanes and an outer portion extending from the inner portion; and
an adjustment ring that is selectively rotatable about a central axis to pivot the vanes, the adjustment ring including apertures that are each associated with and have received therein the outer portion of one of the vane levers associated therewith, each aperture being defined by an inner surface, an outer surface, and first and second opposing radially surfaces connecting the inner surface and the outer surface;
wherein the outer portion of each of the vane levers includes an outermost surface that is non-parallel with the central axis such that the outer portion tapers towards the outer surface of the aperture receiving the vane lever to reduce wear and/or cause lower magnitude impacts between the vane levers and the adjustment ring.

14. The turbocharger of claim 13 , wherein a cross-sectional area of the outer portion of each of the vane levers received in one of the apertures varies moving parallel with the central axis.

15. The turbocharger of claim 13 , wherein the outer surface of each aperture faces radially inward toward the outermost surface of the vane lever received therein.

16. A turbocharger comprising:
a turbine wheel;
a turbine housing containing the turbine wheel and having an inlet and an outlet for exhaust gas to flow, respectively, to and from the turbine wheel; and
a variable turbine geometry assembly comprising:
a base structure;
vanes distributed circumferentially around the base structure and pivotable relative to the base structure to vary an effective inlet area for exhaust gas to flow from the inlet to the turbine wheel;
vane levers for pivoting the vanes, the vane levers each including an inner portion coupled to one of the vanes and an outer portion extending from the inner portion; and
an adjustment ring that is selectively rotatable about a central axis to pivot the vanes, the adjustment ring including apertures that are each associated with and have received therein the outer portion of one of the vane levers associated therewith;

wherein the outer portion of each of the vane levers includes an outer surface that is non-parallel with the central axis, wherein the outer portion of each of the vane levers includes an axial portion that includes the outer surface and that extends axially through the aperture of the adjustment ring associated therewith, and the outer surface is tapered at a constant angle over a majority of an axial dimension thereof, the constant

Assignees

• Borgwarner Inc

Inventors

• King Matthew
• Norsworthy Josh
• Morgan Eli

Classifications

• F05D2220/40

  in turbochargers · CPC title

• F01D17/165

  for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line (F01D17/167 takes precedence) · CPC title

• F02B37/24

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

• F02C6/12

  Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure · CPC title

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title