Turbocharger

Patent metadata

Field	Value
Publication number	US-2018371985-A1
Application number	US-201516064102-A
Country	US
Kind code	A1
Filing date	Dec 25, 2015
Priority date	Dec 25, 2015
Publication date	Dec 27, 2018
Grant date	—

Abstract

This turbocharger includes a rotating shaft extending along an axis, a turbine wheel provided at a first end portion of the rotating shaft, a compressor wheel provided at a second end portion of the rotating shaft, a housing accommodating at least a portion of the rotating shaft, bearings provided in the housing and configured to support the rotating shaft, supply flow paths supplying lubricating oil to the bearings, a discharge oil chamber formed in the housing and to which the lubricating oil is discharged from the bearings, and an oil drainage port formed below the discharge oil chamber, in which at least one of the discharge oil chamber and the oil drainage port is formed to be asymmetric between a first region and a second region defined by a vertical plane including the axis of the rotating shaft as a boundary plane.

First claim

1 - 13 . (canceled)

14 . A turbocharger comprising:
a rotating shaft extending along an axis; a turbine wheel provided at a first end portion of the rotating shaft; a compressor wheel provided at a second end portion of the rotating shaft; a housing accommodating at least a portion of the rotating shaft in a longitudinal direction along the axis; bearings provided in the housing and configured to support the rotating shaft to be rotatable around the axis; a supply flow path supplying lubricating oil to the bearing; a discharge oil chamber formed in the housing and to which the lubricating oil is discharged from the bearing; and an oil drainage port formed below the discharge oil chamber and configured to discharge the lubricating oil to the outside of the housing, wherein at least the discharge oil chamber from the discharge oil chamber and the oil drainage port is formed to be asymmetric between a first region and a second region defined by a vertical plane including the axis of the rotating shaft as a boundary plane, the discharge oil chamber is formed to be asymmetric between an upstream side and a downstream side in a rotating direction of the rotating shaft at an upper end of the rotating shaft, and a cross-sectional area of the discharge oil chamber on the downstream side in the rotating direction of the rotating shaft at the upper end of the rotating shaft is larger than that on the upstream side in the rotating direction.

15 . The turbocharger according to claim 14 , wherein the oil drainage port is formed to be asymmetric between the first region and the second region defined by the vertical plane including the axis of the rotating shaft as a boundary plane.

16 . The turbocharger according to claim 14 , wherein the oil drainage port is provided to be offset to the downstream side in the rotating direction of the rotating shaft with respect to the vertical plane.

17 . The turbocharger according to claim 14 , wherein an inclined surface inclined downward from above from the upstream side in the rotating direction of the rotating shaft to the downstream side is provided below the discharge oil chamber on the downstream side in the rotating direction of the rotating shaft.

18 . The turbocharger according to claim 17 , wherein a vertical surface having an inclination angle smaller than that of the inclined surface is formed below the discharge oil chamber at a portion facing the inclined surface on the upstream side in the rotating direction of the rotating shaft.

19 . The turbocharger according to claim 17 , wherein the oil drainage port is formed to be continuous with a lower side of the inclined surface and is provided to be offset to the upstream side in the rotating direction at an upper side of the rotating shaft with respect to the vertical plane.

20 . The turbocharger according to claim 17 , wherein the oil drainage port is inclined downward from above from the upstream side in the rotating direction of the rotating shaft to the downstream side.

21 . The turbocharger according to claim 14 , wherein a cross-sectional shape of the oil drainage port intersecting the vertical plane is an elliptical shape which is long along the vertical plane.

22 . The turbocharger according to claim 14 , wherein a cross-sectional shape of the oil drainage port intersecting the vertical plane is a rectangular shape which is long along the vertical plane.

23 . The turbocharger according to claim 14 , wherein a cross-sectional shape of the oil drainage port intersecting the vertical plane is a T shape in which a dimension in an axial direction increases in stages toward the downstream side.

24 . The turbocharger according to claim 14 , wherein a cross-sectional shape of the oil drainage port intersecting the vertical plane is a triangle shape in which a dimension in an axial direction increases gradually toward the downstream side.

25 . The turbocharger according to claim 14 , wherein an entrainment-inhibiting portion configured to inhibit entrainment of lubricating oil is provided in the discharge oil chamber.

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd
• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Nambu Takashi
• Shibata Naomichi
• Isayama Shuichi
• Futae Takaya
• Kojima Yuya

Classifications

• F01D25/162

  Bearing supports · 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

• F01D25/20

  using lubrication pumps · CPC title

• F05D2260/609

  Deoiling or demisting · CPC title

• F01D25/243

  Flange connections; Bolting arrangements (F01D25/265 takes precedence) · CPC title