Turbine housing and turbocharger including the same

Patent metadata

Field	Value
Publication number	US-11221022-B2
Application number	US-201716610439-A
Country	US
Kind code	B2
Filing date	Sep 27, 2017
Priority date	Sep 27, 2017
Publication date	Jan 11, 2022
Grant date	Jan 11, 2022

Abstract

A turbine housing includes an outer housing portion which includes an inner wall internally forming a spiral space, a first heat shield core which separates the spiral space into a scroll flow passage where an exhaust gas flows and a heat shield space positioned on a side of the inner wall, the first heat shield core being disposed so as to face the inner wall in the spiral space, a variable nozzle unit for adjusting a flow of the exhaust gas from the scroll flow passage toward an impeller, the variable nozzle unit being disposed on a side opposite to the outer housing portion across the first heat shield core in an axial direction, and at least one annular seal portion disposed between the first heat shield core and the outer housing portion in the axial direction.

First claim

The invention claimed is:

1. A turbine housing comprising:
an outer housing portion which includes an inner wall internally forming a spiral space;
a first heat shield core which separates the spiral space into a scroll flow passage where an exhaust gas flows and a heat shield space positioned on a side of the inner wall, the first heat shield core being disposed so as to face the inner wall in the spiral space;
a variable nozzle unit for adjusting a flow of the exhaust gas from the scroll flow passage toward an impeller, the variable nozzle unit being disposed on a side opposite to the outer housing portion across the first heat shield core in an axial direction; and
at least one annular seal portion disposed between the first heat shield core and the outer housing portion in the axial direction,
wherein the outer housing portion includes an axial protrusion which axially protrudes toward the first heat shield core such that the at least one annular seal portion is held between the axial protrusion and the first heat shield core.

2. The turbine housing according to claim 1 ,
wherein the variable nozzle unit includes:
a nozzle mount;
a nozzle plate disposed separately from the nozzle mount on a turbine outlet side;
a nozzle support coupling and fixing the nozzle mount and the nozzle plate; and
a plurality of variable nozzles circumferentially arranged between the nozzle mount and the nozzle plate, and adjusting the flow of the exhaust gas,
wherein the nozzle plate includes:
an annular portion facing the nozzle mount; and
a cylindrical portion protruding from an inner circumferential end of the annular portion toward the outer housing portion in the axial direction,
wherein the first heat shield core includes a first inner flange portion surrounding the cylindrical portion of the nozzle plate, and
wherein the first inner flange portion is configured such that at least a radial region of the first inner flange portion is pressed against the annular portion of the nozzle plate by the annular seal portion.

3. The turbine housing according to claim 1 ,
wherein the at least the one annular seal portion includes a snap ring configured to be elastically deformable in a radial direction.

4. The turbine housing according to claim 1 ,
wherein the outer housing portion includes an outlet wall portion which forms a turbine outlet flow passage where the exhaust gas after passing through a turbine flows, and
wherein the outlet wall portion internally includes a cooling passage where a refrigerant flows.

5. The turbine housing according to claim 1 , wherein the outer housing portion includes an outlet wall portion which forms a turbine outlet flow passage where the exhaust gas after passing through a turbine flows, and wherein the outlet wall portion internally includes a cooling passage where compressed air generated by a compressor flows.

6. The turbine housing according to claim 1 ,
wherein the outer housing portion includes an outlet wall portion which forms a turbine outlet flow passage where the exhaust gas after passing through a turbine flows, and
wherein the turbine housing further comprises a third heat shield core disposed in the turbine outlet flow passage so as to face an inner wall surface of the outlet wall portion.

7. The turbine housing according to claim 6 ,
wherein the third heat shield core includes a second flange portion protruding radially outward at an axial position between the variable nozzle unit and the outlet wall portion of the outer housing portion, and a bent part formed by bending a part of the second flange portion is interposed between the variable nozzle unit and the outlet wall portion so as to be elastically deformable in the axial direction.

8. A turbocharger comprising:
a turbine which includes the turbine housing according to claim 1 and an impeller configured to be rotated by the exhaust gas guided via the scroll flow passage of the turbine housing; and
a compressor driven by the turbine.

9. A turbine housing comprising:
an outer housing portion which includes an inner wall internally forming a spiral space;
a first heat shield core which separates the spiral space into a scroll flow passage where an exhaust gas flows and a heat shield space positioned on a side of the inner wall, the first heat shield core being disposed so as to face the inner wall in the spiral space;
a variable nozzle unit for adjusting a flow of the exhaust gas from the scroll flow passage toward an impeller, the variable nozzle unit being disposed on a side opposite to the outer housing portion across the first heat shield core in an axial direction; and
at least one annular seal portion disposed between the first heat shield core and the outer housing portion in the axial direction,
wherein the variable nozzle unit includes:
a nozzle mount;
a nozzle plate disposed separately from the nozzle mount on a turbine outlet side:
a nozzle support coupling and fixing the nozzle mount and the nozzle plate; and
a plurality of variable nozzles circumferentially arranged between the nozzle mount and the nozzle plate, and adjusting the flow of the exhaust gas,
wherein the nozzle plate includes:
an annular portion facing the nozzle mount; and
a cylindrical portion protruding from an inner circumferential end of the annular portion toward the outer housing portion in the axial direction,
wherein the first heat shield core includes a first inner flange portion surrounding the cylindrical portion of the nozzle plate, and
wherein the first inner flange portion is configured such that at least a radial region of the first inner flange portion is pressed against the annular portion of the nozzle plate by the annular seal portion,
wherein the turbine housing further comprises a second heat shield core which covers a region of a gas path surface of the nozzle mount contacting the exhaust gas from an outermost peripheral part thereof to at least an inner side of the nozzle support in a radial direction.

10. The turbine housing according to claim 9 , further comprising an insulated space disposed between the nozzle mount and the second heat shield core.

11. The turbine housing according to claim 9 ,
wherein the second heat shield core is interposed and fixed between the nozzle mount and a swaging portion of the nozzle support.

12. A turbine housing comprising:
an outer housing portion which includes an inner wall internally forming a spiral space;
a first heat shield core which separates the spiral space into a scroll flow passage where an exhaust gas flows and a heat shield space positioned on a side of the inner wall, the first heat shield core being disposed so as to face the inner wall in the spiral space;
a variable nozzle unit for adjusting a flow of the exhaust gas from the scroll flow passage toward an impeller, the variable nozzle unit being disposed on a side opposite to the outer housing portion across the first heat shield core in an axial direction; and
at least one annular seal portion disposed between the first heat shield core and the outer housing portion in the axial direction,
wherein the at least the one annular seal portion includes a spring ring configured to be elastically deformable in the axial direction,
wherein the variable nozzle unit includes:
a nozzle mount;
a nozzle plate disposed separately from the nozzle mount on a turbine outlet side;
a nozzle support coupling and fixing the nozzle mount and the nozzle plate; and
a plurality of variable nozzles circumferentially arranged between the nozzle mount and the nozzle plate, and adjusting the flow of the exhaust gas, and
wherein the first heat shield c

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Sakuma Shigeyoshi
• Katou Eigo
• Sakamoto Keigo
• Watanabe Daigo
• Arai Takashi
• Ishii Yuta

Classifications

• Y02T10/12

  Improving ICE efficiencies · 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

• F01D25/08

  Cooling (of machines or engines in general F01P); Heating; Heat-insulation (of blade-carrying members, of blades F01D5/00) · CPC title

• F05D2260/231

  Preventing heat transfer · CPC title