Turbocharger Compressor and Method

Patent metadata

Field	Value
Publication number	US-2017191490-A1
Application number	US-201614987125-A
Country	US
Kind code	A1
Filing date	Jan 4, 2016
Priority date	Jan 4, 2016
Publication date	Jul 6, 2017
Grant date	—

Abstract

A compressor wheel for a turbocharger includes first, second and third pluralities of blades formed around a central hub. Each of the second plurality of blades is disposed between adjacent blades from the first plurality of blades and extend a shorter distance than the first plurality of blades along the centerline of the central hub. Each of the third plurality of blades is disposed between adjacent blades from the first and second pluralities of blades, and extends a shorter distance than the second plurality of blades along the centerline of the central hub. Together, the blades are separated in sets, each set including a blade from each of the first, second and third pluralities in order with respect to any radial location around the compressor wheel as the compressor wheel rotates.

First claim

We claim:

1 . A turbocharger for use with an internal combustion engine, comprising:
a turbine housing surrounding a rotatable turbine wheel that is connected to a shaft; a center housing that includes a bearing arrangement that rotatably supports the shaft, the shaft extending through the center housing; a compressor housing surrounding an end of the shaft; and a compressor wheel connected to the end of the shaft and being rotatably disposed within the compressor housing, the compressor wheel comprising:
a central hub having a centerline, a root portion and an end portion, the root portion being adjacent a connection between the compressor wheel and the end of the shaft;
a first plurality of blades formed around the central hub, each of the first plurality of blades extending from the root portion to a first area adjacent the end portion along the centerline;
a second plurality of blades formed around the central hub, each of the second plurality of blades disposed between adjacent blades from the first plurality of blades and extending from the root portion of the hub to a second area along the centerline that is shorter than the first area with respect to the centerline; and
a third plurality of blades formed around the central hub, each of the third plurality of blades disposed along the central hub between adjacent blades from the first plurality of blades and from the second plurality of blades, each of the third plurality of blades extending from the root portion of the hub to a third area along the centerline that is shorter than the second area with respect to the centerline;
wherein a compressor wheel includes a plurality of sets of blades, each set of blades including a blade from each of the first, second and third pluralities of blades arranged in order such that, at any radial location around the compressor wheel during operation, a blade from the first plurality of blades is followed by a blade from the second plurality of blades, and a blade from the second plurality of blades is followed by a blade from the third plurality of blades.

2 . The turbocharger of claim 1 , wherein the central hub has a generally circular cross section at a varying diameter, which diameter decreases non-linearly in a direction from the root end towards the end portion.

3 . The turbocharger of claim 1 , wherein each blade in the first, second and third pluralities of blades operates to redirect air towards a compressor outlet formed in the compressor housing.

4 . The turbocharger of claim 3 , wherein each blade in the first, second and third pluralities of blades further operates to split air streams passing over and around the compressor wheel to increase compressor efficiency.

5 . The turbocharger of claim 1 , wherein each of the first plurality of blades includes a first leading edge disposed close to the end portion.

6 . The turbocharger of claim 5 , wherein the leading edge of each of the first plurality of blades is swept back towards the root portion.

7 . The turbocharger of claim 6 , wherein the leading edge of each of the first plurality of blades extends extending at an acute angle, α, with respect to the centerline.

8 . The turbocharger of claim 7 , wherein the angle, α, is about 9.5 degrees.

9 . The turbocharger of claim 5 , wherein each of the first plurality of blades forms a first tip at a radially outer end of the respective first leading edge.

10 . The turbocharger of claim 9 , wherein the first tips of the first plurality of blades are axially aligned relative to the centerline and disposed at a first distance, X 1 , with respect to a root diameter of the central hub.

11 . The turbocharger of claim 10 , wherein each of the second plurality of blades includes a second leading edge that forms a second tip.

12 . The turbocharger of claim 11 , wherein the second tips are axially aligned relative to the centerline and disposed at a second distance, X 2 , with respect to the root diameter of the central hub.

13 . The turbocharger of claim 12 , wherein each of the third plurality of blades includes a third leading edge that forms a third tip.

14 . The turbocharger of claim 13 , wherein the third tips are axially aligned relative to the centerline and disposed at a third distance, X 3 , with respect to the root diameter of the central hub.

15 . The turbocharger of claim 14 , wherein X 2 is between 55% and 70% of X 1 .

16 . The turbocharger of claim 15 , wherein X 2 ≈0.62*X 1 .

17 . The turbocharger of claim 14 , wherein X 3 is between 40% and 55% of X 1 .

18 . The turbocharger of claim 17 , wherein X 3 ≈0.46*X 1 .

19 . The turbocharger of claim 14 , wherein X 3 is between 65% and 80% of X 2 .

20 . The turbocharger of claim 19 , wherein X 3 ≈0.73*X 2 .

Assignees

• Caterpillar Inc

Inventors

• Annati Richard E
• Reinhart Eric
• Singer Daniel

Classifications

• F01D5/146

  of blades with tandem configuration, split blades or slotted blades · CPC title

• F01D25/24

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title

• F04D29/284

  for compressors · CPC title

• F01D5/048

  Form or construction · CPC title

• F05D2220/40

  in turbochargers · CPC title