Turbocharger

Patent metadata

Field	Value
Publication number	US-2020056505-A1
Application number	US-201716610152-A
Country	US
Kind code	A1
Filing date	Oct 30, 2017
Priority date	Oct 30, 2017
Publication date	Feb 20, 2020
Grant date	—

Abstract

A turbocharger includes a shaft, a bearing housing, a turbine housing, and a uniting member. The bearing housing includes a first connection section protruded in a radial direction of the shaft, the first connection section having a first face extended in the radial direction, the turbine housing includes a second connection section protruded in the radial direction of the shaft, the second connection section having a second face extended in the radial direction and being faced to the first face, the uniting member interposes the first connection section and the second connection section by being fitted to the first connection section and the second connection section from the outside, and the first face and/or the second face include a ring-shaped concave portion on an inner side in the radial direction of the shaft with a sealing member arranged at the ring-shaped concave portion.

First claim

1 . A turbocharger comprising:
a shaft; a bearing housing accommodating a bearing rotatably supporting the shaft; a turbine housing accommodating a turbine wheel arranged at one end of the shaft in an axial direction; and a uniting member uniting the bearing housing and the turbine housing, wherein the bearing housing includes a first connection section protruded in a radial direction of the shaft, the first connection section having a first face extended in the radial direction, the turbine housing includes a second connection section protruded in the radial direction of the shaft, the second connection section having a second face extended in the radial direction and being faced to the first face, the uniting member interposes the first connection section and the second connection section by being fitted to the first connection section and the second connection section from the outside, and at least one of the first face and the second face includes a ring-shaped concave portion on an inner side in the radial direction of the shaft with a sealing member arranged at the ring-shaped concave portion.

2 . The turbocharger according to claim 1 ,
wherein the uniting member includes a first end section locked on a third face of the first connection section, the third face being on an opposite side to the first face in the axial direction of the shaft, a second end section locked on a fourth face of the second connection section, the fourth face being on an opposite side to the second face in the axial direction of the shaft, and a joint section joined to the first end section and the second end section.

3 . The turbocharger according to claim 2 ,
wherein the first connection section includes a taper section formed on the third face so that thickness of the first connection section gradually becomes larger toward the inner side in the radial direction of the shaft from an outer circumferential face, the second connection section includes a taper section formed on the fourth face so that thickness of the second connection section gradually becomes larger toward the inner side in the radial direction of the shaft from an outer circumferential face, and the first end section and the second end section of the uniting member are extended in directions inclined to the radial direction of the shaft so that distal ends thereof are to be more distanced from each other.

4 . The turbocharger according to claim 1 , further comprising a back plate arranged between the turbine wheel and the bearing housing,
wherein the bearing housing includes an end face formed on a side toward the turbine wheel with respect to the first connection section in the axial direction of the shaft and extended in the radial direction of the shaft, the turbine housing includes a back plate supporting section arranged on a side toward the turbine wheel with respect to the second connection section in the axial direction of the shaft and extended radially inward in the radial direction of the shaft, and the back plate is arranged so that an outer circumferential edge section extended in the radial direction of the shaft is interposed between the back plate supporting section and the end face.

5 . The turbocharger according to claim 1 ,
wherein the ring-shaped concave portion is arranged at the second connection section.

6 . The turbocharger according to claim 1 ,
wherein the ring-shaped concave portion is arranged at the first connection section.

7 . The turbocharger according to claim 1 ,
wherein the ring-shaped concave portion is arranged at the second connection section and the first connection section.

8 . The turbocharger according to claim 1 ,
wherein the bearing housing further includes a coolant flow path through which coolant flows, the coolant flow path being arranged on a further inner side than the ring-shaped concave portion in the radial direction.

9 . The turbocharger according to claim 1 ,
wherein the sealing member is formed into a ring shape, and in section along the axial direction of the shaft, includes a first section to be in touch with the first connection section, a second section to be in touch with the second connection section, and a curved section having a predetermined curvature to join the first section and the second section.

10 . The turbocharger according to claim 9 ,
wherein the sealing member has a predetermined springback characteristic under conditions that a sectional width L satisfies L=(DO−DI)/2, a ratio between height and plate thickness H/T satisfies “8.0≤H/T≤25.0”, a ratio between the height and curvature H/R satisfies “2.0≤H/R≤6.0”, and a ratio between height and sectional width H/L satisfies “0.55≤H/L≤3.5”, while the turbine wheel has a wheel diameter of 20 mm or more and 70 mm or less, coefficients of thermal expansion of the bearing housing and the turbine housing are the same, and regarding the sealing member, DO denotes an outer diameter, DI denotes an inner diameter, H denotes the height, T denotes the plate thickness, and R denotes the curvature of the curved section.

11 . The turbocharger according to claim 8 ,
wherein the turbine housing further includes a fitting section fitted to the bearing housing with an inner side face thereof opposed to an outer side face of the bearing housing, and the fitting section is positioned on a side of the turbine wheel relative to the ring-shaped concave portion in the axial direction of the shaft.

12 . The turbocharger according to claim 11 ,
wherein the turbine housing further includes a back plate supporting section arranged on a side toward the turbine wheel with respect to the fitting section in the axial direction of the shaft and extended radially inward in the radial direction of the shaft, the bearing housing includes an end face formed on a side toward the turbine wheel with respect to the outer side face of the bearing housing in the axial direction of the shaft and extended in the radial direction of the shaft, the turbocharger further comprises a back plate arranged so that an outer circumferential edge section extended in the radial direction of the shaft is interposed between the back plate supporting section and the end face in the axial direction, and the outer circumferential edge of the back place which is interposed between the back place supporting section and the end face is on a side of the turbine wheel relative to the fitting section in the axial direction of the shaft.

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Sakamoto Keigo
• Seike Nariaki
• Irie Sosuke

Classifications

• F05D2220/40

  in turbochargers · CPC title

• F05D2240/55

  Seals · CPC title

• F01D11/005

  Sealing means between non relatively rotating elements · CPC title

• F01D25/243 Primary

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

• F01D25/162 Primary

  Bearing supports · CPC title