Compressor housing assembly for a turbocharger

Patent metadata

Field	Value
Publication number	US-9482240-B2
Application number	US-201313956132-A
Country	US
Kind code	B2
Filing date	Jul 31, 2013
Priority date	Jul 31, 2013
Publication date	Nov 1, 2016
Grant date	Nov 1, 2016

Abstract

A compressor housing assembly for a turbocharger can include a compressor housing shell that includes an axis for alignment with a rotational axis of a compressor wheel, a wall that includes features defined in part by radii with respect to the axis, and an edge that defines in part an inlet opening of a shroud port; and an insert that includes a shroud section and a noise suppressor section that define a recirculation port where the insert is axially located by the wall of the compressor housing shell, where an internal recirculation passage is defined in part by the insert and the wall, and where an edge of the shroud section (e.g., a lowermost edge) defines in part the inlet opening of the shroud port.

First claim

What is claimed is:

1. A compressor housing assembly for a turbocharger comprising:
a compressor housing shell that comprises an axis for alignment with a rotational axis of a compressor wheel, a wall that comprises a seat defined in part by radii with respect to the axis, and an edge that defines in part an inlet opening of a shroud port; and
an insert that comprises a shroud section and a noise suppressor section that define a recirculation port wherein the insert is axially located by a shoulder of the noise suppressor section and the seat of the wall of the compressor housing shell such that the shroud section does not contact the wall of the compressor housing shell, wherein an internal recirculation passage is defined in part by the insert and the wall, wherein a lower edge of the shroud section defines in part the inlet opening of the shroud port and wherein the lower edge is axially the lowermost edge of the insert.

2. The compressor housing assembly of claim 1 wherein the insert comprises at least one bridge that bridges the noise suppressor section to the shroud section.

3. The compressor housing assembly of claim 2 wherein the at least one bridge defines an axial dimension of an inlet opening of the recirculation port between the noise suppressor section and the shroud section.

4. The compressor housing assembly of claim 1 wherein the noise suppressor section comprises an upper edge, a lower edge and an angled inner surface that extends from an upper diameter at the upper edge to a lower diameter at the lower edge wherein the upper diameter exceeds the lower diameter.

5. The compressor housing assembly of claim 1 wherein at least one bridge extends between an axial position above a lower edge of the noise suppressor section to an axial position below an upper edge of the shroud section.

6. The compressor housing assembly of claim 5 wherein a radial clearance exists between an outer surface of the at least one bridge and an inner surface of the compressor housing shell at a location within the internal recirculation passage.

7. The compressor housing assembly of claim 1 comprising at least one spacer.

8. The compressor housing assembly of claim 7 wherein at least one of the at least one spacer is disposed between the insert and the compressor housing shell to define an axial dimension of an inlet opening of the shroud port.

9. A method comprising:
providing a compressor housing shell that comprises an axis for alignment with a rotational axis of a compressor wheel, a wall that comprises a seat defined in part by radii with respect to the axis, and an edge that defines in part an inlet opening of a shroud port;
providing an insert that comprises a shroud section and a noise suppressor section that define a recirculation port; and
axially locating the insert via a shoulder of the noise suppressor section and the seat of the wall of the compressor housing shell, such that the shroud section does not contact the wall of the compressor housing shell, to define an internal recirculation passage in part by the insert and the wall, and to define an inlet opening of the shroud port in part by an edge of the shroud section.

10. The method of claim 9 further comprising assembling a turbocharger that comprises the compressor housing shell and the insert.

Assignees

• Honeywell Int Inc

Inventors

• Gerard Arnaud
• Eumont Vincent
• Van Haesebroeck Baptiste
• Abel Francis
• Roberts Quentin

Classifications

• F05D2220/40

  in turbochargers · CPC title

• Y10T29/49236

  Fluid pump or compressor making · CPC title

• F05D2230/60

  Assembly methods · CPC title

• F04D25/024 Primary

  the driving means being assisted by a power recovery turbine · CPC title

• F04D1/00

  Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps (adapted for pumping specific fluids F04D7/00; priming or boosting F04D9/00) · CPC title