Centrifugal compressor with inclined diffuser

Patent metadata

Field	Value
Publication number	US-10935045-B2
Application number	US-201816039891-A
Country	US
Kind code	B2
Filing date	Jul 19, 2018
Priority date	Jul 19, 2018
Publication date	Mar 2, 2021
Grant date	Mar 2, 2021

Abstract

A compressor includes a compressor impeller configured to rotate about an axis of rotation as intake gases flow along the compressor impeller. The compressor impeller includes an inducer and an exducer. The compressor impeller defines a first impeller end at the inducer and a second impeller end at the exducer. The second impeller end extends along a radial axis. The compressor further includes a compressor housing encasing the compressor impeller. The compressor housing defines a compressor volute. The compressor housing partially defines a diffuser in fluid communication with the compressor volute. The diffuser is elongated along a diffuser axis. The diffuser axis is obliquely angled relative to the axis of rotation. The diffuser axis is obliquely angled relative to the radial axis to minimize a turbulence of the intake gases flowing from the diffuser to the compressor volute.

First claim

What is claimed is:

1. A centrifugal compressor, comprising:
a compressor impeller configured to rotate about an axis of rotation as intake gases flow along the compressor impeller, wherein the compressor impeller includes an inducer and an exducer, the compressor impeller defines a first impeller end at the inducer and a second impeller end at the exducer, the second impeller end extends along a radial axis, and the radial axis is perpendicular to the axis of rotation; and
a compressor housing encasing the compressor impeller, wherein the compressor housing defines a compressor volute, the compressor housing partially defines a diffuser in fluid communication with the compressor volute, the diffuser is configured to convert a kinetic energy of the intake gases into static pressure, the diffuser is elongated along a diffuser axis, the diffuser axis is obliquely angled relative to the axis of rotation, the diffuser axis is obliquely angled relative to the radial axis to minimize a turbulence of the intake gases flowing from the diffuser to the compressor volute;
wherein the diffuser defines a diffuser inlet and a diffuser outlet, the diffuser outlet is in direct fluid communication with the compressor volute, the exducer is closer to the diffuser inlet than to the diffuser outlet, the exducer is spaced apart from the inducer along a first direction, the first direction is parallel to the axis of rotation, the diffuser outlet is spaced apart from the diffuser inlet along a second direction, the second direction is perpendicular to the first direction, a first distance is defined from the first impeller end to the diffuser outlet along the first direction, a second distance is defined from the first impeller end to the diffuser inlet along the first direction, and the second distance is greater than the first distance; further comprising a center housing, wherein the compressor housing includes a first diffuser wall, the center housing includes a second diffuser wall, the first diffuser wall and the second diffuser wall collectively define the diffuser, and each of the first diffuser wall and the second diffuser wall are obliquely angled relative to the radial axis; wherein the first diffuser wall and the second diffuser wall are parallel to each other.

2. The centrifugal compressor of claim 1 , wherein each of the first diffuser wall and the second diffuser wall are entirely linear.

3. The centrifugal compressor of claim 2 , wherein an entirety of the first diffuser wall is parallel to the diffuser axis, and an entirety of the second diffuser wall is parallel to the diffuser axis.

4. The centrifugal compressor of claim 3 , wherein the diffuser includes a diffuser pinch that is closer to the exducer than to the compressor volute, the diffuser pinch defines the diffuser inlet, the diffuser pinch is partially defined by a diffuser wall portion of the second diffuser wall, and an entirety of the diffuser wall portion of the second diffuser wall is parallel to the diffuser axis to minimize the turbulence of the intake gases flowing from the compressor impeller to the diffuser.

5. The centrifugal compressor of claim 4 , wherein the diffuser pinch is partially defined by an inclined wall directly connected to the first diffuser wall, and the inclined wall is obliquely angled relative to the first diffuser wall to facilitate a flow of the intake gases from the compressor impeller to the diffuser.

6. The centrifugal compressor of claim 5 , wherein the diffuser pinch has a tapered shape such that a pinch width of the diffuser pinch decreases in the second direction, the second direction is perpendicular to the first direction, and the second direction is parallel to the radial axis, the diffuser inlet has a maximum inlet width, the diffuser outlet has a maximum outlet width, and the maximum inlet width is greater than the maximum outlet width to the facilitate the flow of the intake gases from the compressor impeller to the diffuser.

7. The centrifugal compressor of claim 6 , wherein the compressor housing defines a volute wall, and the volute wall defines the compressor volute, the volute wall includes a volute wall portion that is proximate to the second diffuser wall, the second diffuser wall includes a diffuser wall segment that is proximate to the volute wall portion, and the volute wall portion is spaced apart from the diffuser wall segment along the first direction to allow the intake gases to flow uninterrupted from the diffuser to the compressor volute.

8. A turbocharger assembly, comprising:
a compressor configured to pressurize intake gases, wherein the compressor includes:
a compressor impeller configured to rotate about an axis of rotation as the intake gases flow along the compressor impeller, wherein the compressor impeller includes an inducer and an exducer, the compressor impeller defines a first impeller end at the inducer and a second impeller end at the exducer, the second impeller end extends along a radial axis, and the radial axis is perpendicular to the axis of rotation;
a compressor housing encasing the compressor impeller, wherein the compressor housing defines a compressor volute, the compressor housing partially defines a diffuser in fluid communication with the compressor volute, the diffuser is configured to convert a kinetic energy of the intake gases into static pressure, the diffuser is elongated along a diffuser axis, the diffuser axis is obliquely angled relative to the axis of rotation, the diffuser axis is obliquely angled relative to the radial axis to minimize a turbulence of the intake gases flowing from the diffuser to the compressor volute;

a turbine coupled to the compressor such that the turbine is configured to rotate about the axis of rotation, wherein the turbine includes a turbine wheel and a turbine housing encasing the turbine wheel; and
a shaft interconnecting the compressor impeller and the turbine wheel; and
wherein the diffuser defines a diffuser inlet and a diffuser outlet, the diffuser outlet is in direct fluid communication with the compressor volute, the exducer is closer to the diffuser inlet than to the diffuser outlet, the exducer is spaced apart from the inducer along a first direction, the first direction is parallel to the axis of rotation, the diffuser outlet is spaced apart from the diffuser inlet along a second direction, the second direction is perpendicular to the first direction, a first distance is defined from the first impeller end to the diffuser outlet along the first direction, a second distance is defined from the first impeller end to the diffuser inlet along the first direction, and the second distance is greater than the first distance; further comprising a center housing, wherein the compressor housing includes a first diffuser wall, the center housing includes a second diffuser wall, the first diffuser wall and the second diffuser wall collectively define the diffuser, and each of the first diffuser wall and the second diffuser wall are obliquely angled relative to the radial axis; wherein the first diffuser wall and the second diffuser wall are parallel to each other.

9. The turbocharger assembly of claim 8 , wherein each of the first diffuser wall and the second diffuser wall are entirely linear.

10. The turbocharger assembly of claim 9 , wherein the diffuser defines a diffuser inlet and a diffuser outlet, the diffuser outlet is in direct fluid communication with the compressor volute, the exducer is closer to the diffuser inlet than to the diffuser outlet, the exducer is spaced apart from the inducer along a first direction, the first direction is parallel to the axis of rotation, an entirety of the first diffuser wall is parallel to the diffuser axis, and a

Assignees

• Gm Global Tech Operations Llc

Inventors

• Wang Chijou

Classifications

• F04D29/667

  by influencing the flow pattern, e.g. suppression of turbulence · CPC title

• F04D17/10

  for compressing or evacuating · CPC title

• F04D29/441 Primary

  especially adapted for elastic fluid pumps · CPC title

• F04D29/4233

  with volutes extending mainly in axial or radially inward direction · CPC title