Turbine and turbocharger including the same

Patent metadata

Field	Value
Publication number	US-11118501-B2
Application number	US-201716610200-A
Country	US
Kind code	B2
Filing date	Oct 31, 2017
Priority date	Oct 31, 2017
Publication date	Sep 14, 2021
Grant date	Sep 14, 2021

Abstract

A turbine includes a turbine impeller, a turbine housing disposed so as to cover the turbine impeller and internally forming a scroll flow passage through which an exhaust gas flows, and a throat forming portion which is provided as a separate piece from the turbine housing. The throat forming portion is disposed to face a section of the turbine housing and forms a hub-side wall surface of a throat portion of the scroll flow passage in an axial direction, the section forming a shroud-side wall surface of the throat portion.

First claim

The invention claimed is:

1. A turbine comprising:
a turbine impeller;
a turbine housing disposed so as to cover the turbine impeller and including an outlet portion for discharging an exhaust gas having passed through the turbine impeller; and
a heat shield portion positioned on an opposite side of the outlet portion in an axial direction across at least one of the turbine impeller or a scroll flow passage communicating with the turbine impeller,
wherein the heat shield portion includes:
a first heat-shielding plate portion which is disposed while facing the scroll flow passage to face a section of the turbine housing and forms a hub-side wall surface of a throat portion of the scroll flow passage in the axial direction, the section forming a shroud-side wall surface of the throat portion; and
a second heat-shielding plate portion arranged to at least partially have a gap with the first heat-shielding plate portion; and a bearing housing disposed on an opposite side of the outlet portion of the turbine housing in the axial direction, wherein the first heat-shielding plate portion and the second heat-shielding plate portion are configured such that a first end part of the first heat-shielding plate portion and a second end part of the second heat-shielding plate portion are fixed to be interposed between the turbine housing and the bearing housing, and at least one of a first surface of the first end part or a second surface of the second end part has a recess, the first surface and the second surface facing each other.

2. The turbine according to claim 1 ,
wherein the first surface of the first heat-shielding plate portion has a first recess extending in one of a circumferential direction or a radial direction, and
wherein the second surface of the second heat-shielding plate portion has a second recess extending in the other of the circumferential direction or the radial direction.

3. The turbine according to claim 1 , further comprising a bearing housing disposed on an opposite side of the outlet portion of the turbine housing in the axial direction,
wherein the first heat-shielding plate portion has the first end part, and the second heat-shielding plate portion has the second end part, the first end part and the second end part being fixed to be interposed between the turbine housing and the bearing housing, and
wherein the gap is formed between at least a part of a section of the first heat-shielding plate portion except for the first end part and at least a part of a section of the second heat-shielding plate portion except for the second end part.

4. The turbine according to claim 3 ,
wherein each of the first heat-shielding plate portion and the second heat-shielding plate portion has an end part which is a free end on an opposite side of the first end part or the second end part interposed between the turbine housing and the bearing housing.

5. The turbine according to claim 1 ,
wherein the second heat-shielding plate portion is disposed so as to at least partially face a back surface of the turbine impeller on an inner side of the first heat-shielding plate portion in a radial direction.

6. The turbine according to claim 1 ,
wherein at least one of the first heat-shielding plate portion or the second heat-shielding plate portion has a heat-shielding coating.

7. A turbocharger comprising:
the turbine according to claim 1 ; and
a compressor including a compressor impeller and configured to be driven by the turbine.

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Yoshida Toyotaka

Classifications

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F05B2260/231

  Preventing heat transfer · CPC title

• F05D2250/51

  Inlet · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F02B39/00 Primary

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