Compressor wheel, method of making the same, and turbocharger including the same

Patent metadata

Field	Value
Publication number	US-10436211-B2
Application number	US-201615236747-A
Country	US
Kind code	B2
Filing date	Aug 15, 2016
Priority date	Aug 15, 2016
Publication date	Oct 8, 2019
Grant date	Oct 8, 2019

Abstract

A turbocharger includes a turbine housing defining a turbine housing interior, a turbine wheel disposed within the turbine housing interior, a shaft coupled to and rotatable by the turbine wheel, a compressor housing defining a compressor housing interior and a flow path, and a compressor wheel disposed within the compressor housing interior and coupled to the shaft. The compressor wheel has a hub coupled to the shaft, and a plurality of impeller blades extending radially from the hub. The plurality of impeller blades define an inducer end having an inducer diameter, and an exducer end having an exducer diameter greater than the inducer diameter. The inducer diameter and the exducer diameter establish a compressor trim. The compressor wheel also has a compressor wheel shroud disposed about the plurality of impeller blades. The compressor wheel shroud encloses the plurality of impeller blades to define a shroud interior.

First claim

What is claimed is:

1. A compressor wheel for use in a turbocharger for a vehicle, said compressor wheel comprising:
a hub having a hub length extending along a axis, with said hub presenting an outer hub surface concentric about said axis, and with said hub having a first hub end and a second hub end spaced from said first hub end along said hub length;
a plurality of impeller blades extending radially from said outer hub surface, with each of said impeller blades having a root portion coupled to said hub and a tip portion spaced radially about said axis from said root portion, with said plurality of impeller blades defining an inducer end having an inducer diameter (ID) adjacent said first hub end, and an exducer end having an exducer diameter (ED) adjacent said second hub end that is greater than said inducer diameter, and with said inducer diameter (ID) and said exducer diameter (ED) establishing a compressor trim; and
a compressor wheel shroud disposed about and configured to be rotatable with said plurality of impeller blades, with said compressor wheel shroud enclosing said plurality of impeller blades to define a shroud interior;
wherein said compressor wheel shroud further defines multiple shroud bleed slots at said first hub end for allowing air to radially flow into and out of said shroud interior with respect to said axis.

2. The compressor wheel as set forth in claim 1 , wherein said compressor wheel shroud is coupled to said tip portion of said plurality of impeller blades.

3. The compressor wheel as set forth in claim 1 , wherein said compressor wheel shroud defines a first shroud diameter adjacent said first end of said hub, and a second shroud diameter adjacent said second end of said hub, with said second shroud diameter being greater than said first shroud diameter.

4. The compressor wheel as set forth in claim 3 , wherein said compressor wheel shroud has a concave configuration with respect to said axis.

5. The compressor wheel as set forth in claim 1 , wherein said compressor shroud is disposed between said tip portion and said root portion of said plurality of impeller blades.

6. A turbocharger for receiving exhaust gas from an internal combustion engine and for delivering compressed air to the internal combustion engine, said turbocharger comprising:
a turbine housing defining a turbine housing interior;
a turbine wheel disposed within said turbine housing interior for receiving the exhaust gas from the internal combustion engine;
a shaft coupled to and rotatable by said turbine wheel;
a compressor housing defining a compressor housing interior and a flow path, with said flow path fluidly coupling said compressor housing interior with the internal combustion engine; and
a compressor wheel disposed within said compressor housing interior and coupled to said shaft, with said compressor wheel being rotatable by said shaft for delivering compressed air to the internal combustion engine through said flow path, said compressor wheel having,
a hub coupled to said shaft, with said hub having a hub length extending along an axis that extends along said compressor housing interior, with said hub presenting an outer hub surface concentric about said axis, and with said hub having a first hub end and a second hub end spaced from said first hub end along said hub length,
a plurality of impeller blades extending radially from said outer hub surface, with each of said impeller blades having a root portion coupled to said hub and a tip portion spaced radially about said axis from said root portion, with said plurality of impeller blades defining an inducer end having an inducer diameter (ID) adjacent said first hub end, and an exducer end having an exducer diameter (ED) adjacent said second hub end that is greater than said inducer diameter (ID), and with said inducer diameter (ID) and said exducer diameter (ED) establishing a compressor trim, and
a compressor wheel shroud disposed about and configured to be rotatable with said plurality of impeller blades, with said compressor wheel shroud enclosing said plurality of impeller blades to define a shroud interior;

wherein said compressor housing defines a recirculation cavity about said axis and defines a compressor housing bleed slot for allowing air to radially flow into and out of said compressor housing interior with respect said axis, and flow radially into and out of said recirculation cavity with respect to said axis.

7. The turbocharger as set forth in claim 6 , wherein said compressor wheel shroud is coupled to said tip portion of said plurality of impeller blades.

8. The turbocharger as set forth in claim 6 , wherein said compressor wheel shroud defines a first shroud diameter adjacent said first end of said hub, and a second shroud diameter adjacent said second end of said hub, with said second shroud diameter being greater than said first shroud diameter.

9. The turbocharger as set forth in claim 6 , wherein said compressor wheel shroud has a concave configuration with respect to said axis.

10. The turbocharger as set forth in claim 6 , wherein said compressor wheel shroud defines a shroud bleed slot adjacent said first hub end for allowing air to radially flow into and out of said shroud interior with respect to said axis.

11. The turbocharger as set forth in claim 10 , wherein said compressor housing bleed slot is adjacent said shroud bleed slot for allowing air to radially flow into and out of said shroud interior with respect said axis, radially flow into and out of said compressor housing interior with respect said axis, and flow radially into and out of said recirculation cavity with respect to said axis.

12. The turbocharger as set forth in claim 6 , wherein said compressor housing defines a cutout adjacent said flow path, with said cutout fluidly coupling said flow path, said compressor housing bleed slot, and said recirculation cavity for allowing air to radially flow out of said compressor housing interior and into said recirculation cavity with respect to said axis.

13. The turbocharger as set forth in claim 6 , wherein said compressor wheel shroud has an outer wheel shroud radius along said hub length and said compressor housing has an inner compressor housing radius along said hub length, with said inner compressor housing radius being greater than said outer wheel shroud radius for defining a reverse flow path therebetween.

14. The turbocharger as set forth in claim 6 , wherein said compressor housing defines a recess about said axis, with said compressor wheel shroud of said compressor wheel at least partially disposed within said recess.

15. The turbocharger as set forth in claim 6 , wherein said compressor housing has a first compressor housing radius adjacent said first hub end of said hub, with said first compressor housing radius equal to one half of said inducer diameter.

16. The turbocharger as set forth in claim 6 , wherein said compressor shroud is disposed between said tip portion and said root portion of said plurality of impeller blades.

Assignees

• Borgwarner Inc

Inventors

• Mcardle Nathan
• Murphy Paul
• Palmer-White Tristram

Classifications

• F02B33/40

  of non-positive-displacement type · CPC title

• F04D29/284 Primary

  for compressors · CPC title

• F01D5/048

  Form or construction · CPC title

• F04D29/4213

  suction ports · CPC title

• F04D29/685

  Inducing localised fluid recirculation in the stator-rotor interface · CPC title