Turbocharger with gas and liquid flow paths

Patent metadata

Field	Value
Publication number	US-10502263-B2
Application number	US-201715675429-A
Country	US
Kind code	B2
Filing date	Aug 11, 2017
Priority date	Aug 11, 2017
Publication date	Dec 10, 2019
Grant date	Dec 10, 2019

Abstract

A turbocharger can include a housing that includes an interior cavity in fluid communication with a lubricant inlet and a lubricant outlet where, at a compressor side, the interior cavity includes an effective opening at a first axial face that spans an azimuthal angle about an axis of a through bore of the housing; a compressor side plate disposed at least in part in a compressor side recess of the housing; and a lubricant deflector plate disposed between the compressor side plate and the first axial face of the housing where the lubricant deflector plate includes an effective opening that substantially spans the azimuthal angle about the axis and where the lubricant deflector plate defines a seal cavity with respect to a compressor side seal recess of the housing.

First claim

What is claimed is:

1. A turbocharger comprising:
a housing that comprises
a compressor side,
a turbine side,
a through bore that extends between the compressor side and the turbine side,
a compressor side recess defined in part by a first radius and a first axial face with respect to an axis of the through bore,
a compressor side seal recess defined in part by a second radius and a second axial face with respect to the axis wherein the compressor side seal recess comprises a drain passage,
a lubricant inlet,
a lubricant outlet, and
an interior cavity in fluid communication with the lubricant inlet and the lubricant outlet wherein, at the compressor side, the interior cavity comprises an interior cavity effective opening at the first axial face that spans an azimuthal angle about the axis of at least 90 degrees, wherein the housing comprises a cast housing wherein the interior cavity effective opening at the first axial face that spans the azimuthal angle about the axis comprises a cast opening;

a shaft and turbine wheel assembly that comprises a shaft free end and a turbine wheel end;
a collar that comprises a bore wherein the shaft is received in the bore of the collar;
a compressor side plate disposed at least in part in the compressor side recess wherein the compressor side plate comprises an opening and wherein the collar is disposed at least in part in the opening; and
a lubricant deflector plate disposed between the compressor side plate and the first axial face of the housing wherein the lubricant deflector plate comprises a lubricant deflector plate effective opening that spans an azimuthal angle about the axis of at least 90 degrees, wherein the interior cavity effective opening and the lubricant deflector plate effective opening at least partially overlap to form at least one gas passage, and wherein the lubricant deflector plate defines a seal cavity with respect to the compressor side seal recess.

2. The turbocharger of claim 1 wherein the lubricant deflector plate defines at least a portion of the drain passage.

3. The turbocharger of claim 1 wherein the drain passage and the lubricant outlet are located at a substantially common azimuthal angle with respect to the axis.

4. The turbocharger of claim 3 wherein the common azimuthal angle corresponds to an installed orientation of the turbocharger that aligns the drain passage and the lubricant outlet with respect to gravity.

5. The turbocharger of claim 1 wherein the interior cavity effective opening, at the first axial face that spans the azimuthal angle about the axis, enlarges a range of installed orientation angles of the turbocharger.

6. The turbocharger of claim 5 wherein the range of installed orientation angles of the turbocharger comprises a range from −45 degrees to +45 degrees.

7. The turbocharger of claim 5 wherein the interior cavity effective opening spans an azimuthal angle of at least 130 degrees and wherein the range of installed orientation angles of the turbocharger comprises a range from −65 degrees to +65 degrees.

8. The turbocharger of claim 5 wherein the interior cavity effective opening spans an azimuthal angle of at least 170 degrees and wherein the range of installed orientation angles of the turbocharger comprises a range from −85 degrees to +85 degrees.

9. The turbocharger of claim 1 wherein the lubricant deflector plate comprises a planar plate.

10. The turbocharger of claim 1 wherein the lubricant deflector plate comprises a planar portion and a rim that extends axially outwardly from the planar portion.

11. The turbocharger of claim 1 wherein the compressor side plate comprises an outer surface and an annular groove in the outer surface wherein the annular groove receives a seal element that forms a seal with respect to a surface of the housing that defines in part the compressor side recess of the housing.

12. The turbocharger of claim 1 comprising at least one seal element disposed between the collar and the compressor side plate.

13. The turbocharger of claim 12 wherein the at least one seal element comprises at least one piston ring.

14. The turbocharger of claim 1 comprising a journal bearing.

15. The turbocharger of claim 14 wherein the journal bearing comprises a unitary journal bearing that comprises a compressor side journal and a turbine side journal.

16. The turbocharger of claim 1 wherein the cast opening corresponds to and is formed by at least one casting core.

17. The turbocharger of claim 1 wherein the lubricant deflector plate comprises eyes, a nose and a smile wherein the eyes comprise bolt openings, wherein the nose comprises a shaft opening and wherein the lubricant deflector plate effective opening forms the smile.

Assignees

• Garrett Transportation I Inc

Inventors

• Wood Daniel
• Noelle Philippe
• Jin Xiao Lei

Classifications

• F05D2260/602

  Drainage · CPC title

• F02C6/12

  Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F02B39/00

  Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00 · CPC title

• F04D17/10

  for compressing or evacuating · CPC title