Systems for a turbocharger

Patent metadata

Field	Value
Publication number	US-11060416-B2
Application number	US-201916264174-A
Country	US
Kind code	B2
Filing date	Jan 31, 2019
Priority date	Jan 31, 2019
Publication date	Jul 13, 2021
Grant date	Jul 13, 2021

Abstract

Various methods and systems are provided for a radial turbocharger. In one example, the turbocharger comprises a turbine case housing a turbine wheel and a compressor case housing a compressor wheel, the turbine case including a vaneless turbine nozzle integrated into the turbine case, a bearing case surrounding a shaft connecting the turbine wheel to the compressor wheel and arranged between the turbine case and compressor case, a plurality of long bolts arranged around a circumference of the turbine case, and a plurality of slots arranged around a circumference of the turbine case, a slot length of each slot extending in a radial direction and adapted to receive a dowel pin having a diameter smaller than the slot length, where each dowel pin, via a corresponding slot, couples the bearing case to the turbine case.

First claim

The invention claimed is:

1. A turbocharger, comprising:
a turbine case housing a turbine wheel and a compressor case housing a compressor wheel, the turbine case including a vaneless turbine nozzle integrated into the turbine case and the turbine case including a first flange;
a bearing case surrounding a shaft connecting the turbine wheel to the compressor wheel and arranged between the turbine case and compressor case, the bearing case including a second flange, wherein the first flange and the second flange have face-sharing contact with one another, wherein a thermal relief groove is depressed into a face of the second flange that has face-sharing contact with the first flange; and
a plurality of fasteners arranged around a circumference of the turbine case, each fastener of the plurality of fasteners extending parallel to the shaft and from an outer face of a compressor end of the bearing case, through the bearing case, and into the turbine case; and
a water jacket surrounding the shaft and extending into a portion of the second flange.

2. The turbocharger of claim 1 , wherein the bearing case is water-cooled via the water jacket, the water jacket including a plurality of extending portions, each extending outward from the annular portion, relative to the shaft, and spaced apart from adjacent extending portions of the plurality of extending portions, where outer ends of the extending portions are spaced apart from an outer surface of the bearing case to create a supporting region for coupling the bearing case to the first flange of the turbine case.

3. The turbocharger of claim 2 , wherein each fastener of the plurality of fasteners is positioned between a different pair of adjacent extending portions of the plurality of extending portions and wherein the water jacket further includes smooth, curved transitions between each extending portion of the plurality of extending portions and the annular portion.

4. The turbocharger of claim 2 , wherein the thermal relief groove is arranged adjacent to one extending portion of the plurality of extending portions, and wherein the turbine case is not actively cooled.

5. The turbocharger of claim 1 , wherein the turbine wheel extends radially across the turbine case, to the nozzle, and extends inward, in an axial direction, past the nozzle.

6. The turbocharger of claim 1 , wherein the turbine nozzle is molded together as one piece with a remainder of the turbine case.

7. The turbocharger of claim 1 , wherein the bearing case includes a cartridge journal bearing surrounding a central-portion of the shaft and a thrust bearing surrounding another portion of the shaft arranged outside the journal bearing, relative to an axial direction, on a compressor-side of the shaft.

8. The turbocharger of claim 1 , further comprising a plurality of slots arranged around a circumference of the turbine case, a slot length of each slot extending in a radial direction and adapted to receive a dowel pin having a diameter smaller than the slot length, where each dowel pin, via a corresponding slot, couples the bearing case to the turbine case.

9. The turbocharger of claim 8 , wherein the diameter of each dowel pin is sized to engage with opposing sides of the corresponding slot, the sides arranged in a direction of the slot length of the corresponding slot.

10. The turbocharger of claim 8 , wherein the plurality of slots includes two sets of two slots with slot lengths oriented in a same direction.

11. A turbocharger, comprising:
a turbine case housing a turbine wheel and a compressor case housing a compressor wheel of a compressor, the turbine case including a vaneless turbine nozzle integrated together as one piece with a remainder of the turbine case, wherein the turbine case includes a first flange;
a water-cooled bearing case surrounding a shaft connecting the turbine wheel to the compressor wheel and arranged between and in face-sharing contact with each of the turbine case and compressor case, the water-cooled bearing case including a water jacket surrounding the shaft, the water jacket including an annular portion and a plurality of extending portions extending radially outward from the annular portion, relative to the shaft, and spaced apart from one another around a circumference of the annular portion, wherein the water-cooled bearing case includes a second flange, wherein the first flange and the second flange have face-sharing contact with one another, wherein a thermal relief groove is depressed into a face of the second flange that has face-sharing contact with the first flange, and wherein the water jacket extends into a portion of the second flange; and
a plurality of fasteners arranged around a circumference of the turbine case, each fastener of the plurality of fasteners extending parallel to the shaft and from an outer face of a compressor end of the bearing case, through the bearing case, outside of the annular portion of the water jacket, and into the turbine case, where each fastener is positioned between a different pair of adjacent extending portions of the water jacket.

12. The turbocharger of claim 11 , wherein the bearing case extends between the turbine wheel and compressor wheel and wherein first flange of the turbine case is an annular flange extending into the bearing case, toward the compressor, the first flange arranged at a position that is radially outward, relative to the shaft, of the turbine wheel and the annular portion of the water jacket, and axially between the turbine nozzle and plurality of extending portions of the water jacket.

13. The turbocharger of claim 12 , wherein the bearing case has an outer diameter that extends past a radial position of the turbine nozzle and wherein additional material of the bearing case, forming the second flange, is arranged between the outer diameter and ends of the plurality of extending portions of the water jacket, the second flange adapted to support the first flange of the turbine case.

14. The turbocharger of claim 13 , further comprising a plurality of pinned slot connections arranged around a circumference of the turbocharger, between the first flange of the turbine case and the second flange of the bearing case, where the first flange includes a plurality of spaced apart slots, each adapted to receive a pin coupling the second flange to the first flange.

15. The turbocharger of claim 14 , wherein the thermal relief groove is spaced apart from an adjacent pinned slot connection, the thermal relief groove positioned proximate to an extending portion of the plurality of extending portions, and wherein the turbine case is not actively cooled.

16. The turbocharger of claim 15 , wherein each fastener of the plurality of fasteners extends into the first flange of the turbine case and wherein each of the plurality of fasteners, pinned slot connections, and extending portions are arranged at a same radial position around the circumference of the turbocharger.

17. The turbocharger of claim 11 , wherein a thickness of the turbine case is thicker in a region surrounding the turbine wheel than a remainder of the turbine case.

18. A turbocharger, comprising:
a non-actively cooled turbine case housing a turbine wheel and a compressor case housing a compressor wheel;
a water-cooled bearing case surrounding a shaft connecting the turbine wheel to the compressor wheel and arranged between the turbine case and compressor case;
a plurality of slots arranged around a circumference of the turbine case, each slot including a slot length and a slot diameter, the slot length longer

Assignees

• Transp Ip Holdings Llc

Inventors

• Homison Christopher Joseph
• Kobielski Louis
• Loringer Daniel Edward
• Scott Richard
• Johnson Lukas
• Vaughn Jared
• Kulkarni Raghav

Classifications

• F05D2230/60

  Assembly methods · CPC title

• F01D25/12

  Cooling · CPC title

• F05D2260/31

  Retaining bolts or nuts · CPC title

• F05D2240/14

  Casings or housings protecting or supporting assemblies within · CPC title

• F16C17/02

  for radial load only · CPC title