Method for making a twin-vaned nozzle ring assembly for a turbocharger with twin-scroll turbine housing for directing exhaust gases from each scroll onto turbine wheel in interleaved fashion

Patent metadata

Field	Value
Publication number	US-11248488-B2
Application number	US-201916421703-A
Country	US
Kind code	B2
Filing date	May 24, 2019
Priority date	Mar 12, 2019
Publication date	Feb 15, 2022
Grant date	Feb 15, 2022

Abstract

A twin-vaned nozzle ring for a turbine nozzle of a turbocharger nozzle ring is made by assembling the nozzle ring from three separately formed parts. A center part includes a first ring of circumferentially spaced first vanes and a second ring of circumferentially spaced second vanes, the first and second rings being axially spaced and integrally joined to each other. The first vanes are circumferentially offset from the second vanes, and exits from the first vane passages are radially aligned with and circumferentially interleaved with exits from the second vane passages. First and second side walls are provided as separate parts. Finally, the first side wall is joined to a distal or outer face of the first ring, and the second side wall is joined to a distal face of the second ring to complete the assembly.

First claim

What is claimed is:

1. A method for making a twin-vaned nozzle ring assembly for a turbine nozzle of a turbocharger, the method comprising the steps of:
(a) providing a first side wall as a ring-shaped part;
(b) providing a second side wall as a ring-shaped part, the second side wall being formed separately from the first side wall;
(c) providing a nozzle ring separately from the first and second side walls, wherein the nozzle ring is provided to have a first vane ring comprising first vanes circumferentially spaced about a circumference of the nozzle ring and is provided to have a second vane ring comprising second vanes circumferentially spaced about the circumference of the nozzle ring, the first and second vane rings being axially spaced and integrally joined to each other, the first vane ring defining first vane passages between circumferentially successive first vanes and extending from first vane passage entrances at leading edges of the first vanes to first vane passage exits at trailing edges of the first vanes, the second vane ring defining second vane passages between circumferentially successive second vanes and extending from second vane passage entrances at leading edges of the second vanes to second vane passage exits at trailing edges of the second vanes, wherein the first vanes are circumferentially offset from the second vanes, the first vane passage entrances are axially spaced apart from the second vane passage entrances, and the first vane passage exits coincide in axial extent and axial location with the second vane passage exits and are circumferentially interleaved with the second vane passage exits; and
(d) joining the first side wall to a distal face of the first vane ring, and joining the second side wall to a distal face of the second vane ring.

2. The method of claim 1 , wherein step (a) comprises providing the first side wall to include a plurality of depressed vane receptacles in a face of the first side wall that confronts the distal face of the first vane ring, each said depressed vane receptacle receiving a distal end of a respective first vane.

3. The method of claim 1 , wherein step (b) comprises providing the second side wall to include a plurality of depressed vane receptacles in a face of the second side wall that confronts the distal face of the second vane ring, each said depressed vane receptacle receiving a distal end of a respective second vane.

4. The method of claim 1 , wherein step (c) comprises making the nozzle ring by an injection molding process.

5. The method of claim 4 , wherein the injection molding process comprises a metal injection molding (MIM) process.

6. The method of claim 1 , wherein the first side wall and the first vane ring each is provided to define a plurality of circumferentially spaced pin receptacles, the pin receptacles of the first side wall being aligned with the pin receptacles of the first vane ring, and wherein step (d) comprises press-fitting pins into the pin receptacles of the first vane ring and into the pin receptacles of the first side wall.

7. The method of claim 1 , wherein the second side wall and the second vane ring each is provided to define a plurality of circumferentially spaced pin receptacles, the pin receptacles of the second side wall being aligned with the pin receptacles of the second vane ring, and wherein step (d) comprises press-fitting pins into the pin receptacles of the second vane ring and into the pin receptacles of the second side wall.

8. The method of claim 1 , wherein the first vane ring is provided to include a plurality of circumferentially spaced pins projecting from the distal face of the first vane ring, and the first side wall is provided to include a plurality of circumferentially spaced pin receptacles, and wherein step (d) comprises inserting the pins of the first vane ring into the pin receptacles of the first side wall and affixing the pins therein.

9. The method of claim 8 , wherein the step of affixing the pins in the pin receptacles comprises riveting the pins.

10. The method of claim 1 , wherein the second vane ring is provided to include a plurality of circumferentially spaced pins projecting from the distal face of the second vane ring, and the second side wall is provided to include a plurality of circumferentially spaced pin receptacles, and wherein step (d) comprises inserting the pins of the second vane ring into the pin receptacles of the second side wall and affixing the pins therein.

11. The method of claim 10 , wherein the step of affixing the pins in the pin receptacles comprises riveting the pins.

Assignees

• Garrett Transportation I Inc

Inventors

• Eckl Filip
• Pribyl Petr
• Skara Petr

Classifications

• F02B37/025

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

• F05D2220/40

  in turbochargers · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F01D9/041

  using blades (F01D5/148 takes precedence) · CPC title

• F01D13/02 Primary

  Working-fluid interconnection of machines or engines · CPC title