Diffuser and turbocharger

Patent metadata

Field	Value
Publication number	US-11187144-B2
Application number	US-201716769379-A
Country	US
Kind code	B2
Filing date	Dec 7, 2017
Priority date	Dec 7, 2017
Publication date	Nov 30, 2021
Grant date	Nov 30, 2021

Abstract

A diffuser includes a connection section and a body section. The connection section extends from an outlet of turbine rotor blades. The body section is connected to an end of the connection section on a downstream side and has a larger flow passage sectional area than the connection section. The shape of the flow passage sectional surface of the connection section is formed into a circle at an outlet of the turbine rotor blades and is formed into an ellipse at an inlet of the body section. The shape of the flow passage sectional surface of the connection section is further formed to be gradually enlarged in a long-axis direction of the ellipse from the outlet of the turbine rotor blades toward the inlet of the body section.

First claim

The invention claimed is:

1. A diffuser comprising:
a connection section extending from an outlet of turbine rotor blades of a turbine wheel and in a straight line in an axial direction in which a rotation shaft of the turbine wheel extends; and
a body section connected to an end of the connection section on a downstream side and having a larger flow passage sectional area than the connection section,
wherein a shape of a flow passage sectional surface of the connection section is formed into a circle at the outlet of the turbine rotor blades and into an ellipse at an inlet of the body section, and is formed to be gradually enlarged in a long-axis direction of the ellipse from the outlet of the turbine rotor blades toward the inlet of the body section.

2. The diffuser according to claim 1 ,
wherein a connection section center that is a center of the ellipse of the connection section at the inlet of the body section is located at a position deviating from a body section center that is a center of the flow passage sectional surface of the body section, and
a long axis of the ellipse extends on a side at least closer to the body section center than to the connection section center.

3. The diffuser according to claim 1 , wherein the flow passage sectional area of the connection section is gradually enlarged from the outlet of the turbine rotor blades toward the inlet of the body section.

4. The diffuser according to claim 1 ,
wherein the connection section includes narrowing sections projecting toward the connection section center that is a center of the ellipse from an inner peripheral surface at a position that intersects a short axis of the ellipse, and
a projecting height of the narrowing sections gradually increases from the outlet of the turbine rotor blades toward the inlet of the body section.

5. A turbocharger comprising:
the diffuser according to claim 1 .

6. The diffuser according to claim 2 , wherein the flow passage sectional area of the connection section is gradually enlarged from the outlet of the turbine rotor blades toward the inlet of the body section.

7. The diffuser according to claim 2 ,
wherein the connection section includes narrowing sections projecting toward the connection section center that is a center of the ellipse from an inner peripheral surface at a position that intersects a short axis of the ellipse, and
a projecting height of the narrowing sections gradually increases from the outlet of the turbine rotor blades toward the inlet of the body section.

8. The diffuser according to claim 3 ,
wherein the connection section includes narrowing sections projecting toward the connection section center that is a center of the ellipse from an inner peripheral surface at a position that intersects a short axis of the ellipse, and
a projecting height of the narrowing sections gradually increases from the outlet of the turbine rotor blades toward the inlet of the body section.

9. A turbocharger comprising:
the diffuser according to claim 2 .

10. A turbocharger comprising:
the diffuser according to claim 3 .

11. A turbocharger comprising:
the diffuser according to claim 4 .

12. The diffuser according to claim 1 ,
wherein the connection section has a connection section center that is a central axis of the connection section and that overlaps a central axis of the rotation shaft.

13. The diffuser according to claim 1 ,
wherein the body section extends in the axial direction.

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Hoshi Toru
• Takashima Reiko
• Yokoyama Takao

Classifications

• F01D25/30

  Exhaust heads, chambers, or the like · CPC title

• F02B37/183 Primary

  Arrangements of bypass valves or actuators therefor · CPC title

• F01D17/143

  the shiftable member being a wall, or part thereof of a radial diffuser · CPC title

• F02B37/00 Primary

  Engines characterised by provision of pumps driven at least for part of the time by exhaust · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title