Turbine housing, turbocharger, and gasoline engine

Patent metadata

Field	Value
Publication number	US-12055091-B2
Application number	US-202018016618-A
Country	US
Kind code	B2
Filing date	Dec 28, 2020
Priority date	Dec 28, 2020
Publication date	Aug 6, 2024
Grant date	Aug 6, 2024

Abstract

A turbine housing that includes: a body part including a scroll passage wall surface, an exhaust gas discharge path wall surface, and a wastegate passage wall surface provided inside the body part, the scroll passage wall surface forming a scroll passage having a scroll shape, the wastegate passage wall surface forming a wastegate passage connecting the scroll passage and the exhaust gas discharge path to each other while bypassing the turbine wheel; and an entrance flange part provided at an upstream end of the scroll passage in the body part, the entrance flange part including an exhaust gas inlet leading to the scroll passage. The wastegate passage has an entrance-side opening edge formed at the scroll passage wall surface and provided at a position where the entrance-side opening edge is visually recognizable at least partially from outside the turbine housing through the exhaust gas inlet.

First claim

The invention claimed is:

1. A turbine housing configured to house a turbine wheel to be driven with exhaust gas discharged from a gasoline engine, comprising:
a body part including a scroll passage wall surface, an exhaust gas discharge path wall surface, and a wastegate passage wall surface provided inside the body part,
the scroll passage wall surface forming a scroll passage having a scroll shape for guiding the exhaust gas to the turbine wheel,
the exhaust gas discharge path wall surface forming an exhaust gas discharge path for discharging the exhaust gas having passed through the turbine wheel,
the wastegate passage wall surface forming a wastegate passage connecting the scroll passage and the exhaust gas discharge path to each other while bypassing the turbine wheel; and
an entrance flange part provided at an upstream end of the scroll passage in the body part, the entrance flange part including an exhaust gas inlet leading to the scroll passage, wherein
the wastegate passage has an entrance-side opening edge formed at the scroll passage wall surface and provided at a position where the entrance-side opening edge is visually recognizable at least partially from outside the turbine housing through the exhaust gas inlet,
wherein the entrance-side opening edge includes a stress concentration part provided at a downstream end portion including a downstream end at the entrance-side opening edge and configured to cause concentration of stress resulting from thermal elongation.

2. The turbine housing according to claim 1 , wherein
the stress concentration part includes:
a first side tilting toward one side with respect to a first line connecting an upstream end and the downstream end at the entrance-side opening edge to each other as the first side extends from the downstream end portion toward an upstream side of a flow direction in the scroll passage; and
a second side tilting toward the other side with respect to the first line as the second side extends from the downstream end portion toward the upstream side of the flow direction in the scroll passage.

3. The turbine housing according to claim 1 , wherein
the stress concentration part includes a slit extending from the downstream end portion at the entrance-side opening edge toward a downstream side of a flow direction in the scroll passage.

4. The turbine housing according to claim 1 , wherein
the stress concentration part is provided in a central area in an opening width direction of an entrance opening of the wastegate passage at the scroll passage wall surface.

5. The turbine housing according to claim 1 , wherein
the exhaust gas discharge path is configured to guide the exhaust gas from one side toward the other side of a direction in which an axis of the turbine wheel extends, and
a normal passing through the center of an exit opening of the wastegate passage is configured to extend in a direction intersecting the axis of the turbine wheel.

6. The turbine housing according to claim 5 , wherein
in a plan view covering the axis of the turbine wheel and the center of the exit opening, 30°≤θ≤60° is satisfied where θ is an angle formed between the axis and the normal.

7. A turbocharger comprising the turbine housing according to claim 1 .

8. A gasoline engine comprising:
a cylinder block including a plurality of cylinders;
an exhaust manifold where exhaust gases discharged from respective ones of the plurality of cylinders join together, the exhaust manifold being provided at least partially inside the cylinder block; and
the turbocharger according to claim 7 , wherein
the entrance flange part of the turbine housing is connected to the exhaust manifold.

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Miyoshi Shunsuke
• Nitta Kenji
• Nakagawa Hiroshi
• Irie Sosuke

Classifications

• F04D29/4206

  especially adapted for elastic fluid pumps · CPC title

• F04D17/10

  for compressing or evacuating · CPC title

• F02B37/183 Primary

  Arrangements of bypass valves or actuators therefor · CPC title

• F02B37/18 Primary

  by bypassing exhaust {from the inlet to the outlet of turbine or to the atmosphere} · CPC title

• F01D25/24

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title