Manufacturing method of turbine housing

Patent metadata

Field	Value
Publication number	US-11371367-B2
Application number	US-201816955538-A
Country	US
Kind code	B2
Filing date	Dec 21, 2018
Priority date	Dec 22, 2017
Publication date	Jun 28, 2022
Grant date	Jun 28, 2022

Abstract

In a manufacturing method of a turbine housing having an exhaust gas flow path, the exhaust gas flow path in the turbine housing is formed of a sheet-metal-made divided body and a cast-metal-made divided body, the sheet-metal-made divided body is formed by press molding a sheet metal material, and the cast-metal-made divided body is molded by casting, when the cast-metal-made divided body is cast, one end of the sheet-metal-made divided body is cast into the cast-metal-made divided body by melting the one end of the sheet-metal-made divided body such that the original shape thereof is disappeared.

First claim

The invention claimed is:

1. A manufacturing method of a turbine housing having an exhaust gas flow path, the exhaust gas flow path in the turbine housing being formed of a sheet-metal-made divided body and a cast-metal-made divided body, the method comprising:
a step of forming the sheet-metal-made divided body by press molding a sheet metal material; and
a casting step of molding the cast-metal-made divided body, wherein
in the casting step, one end of the sheet-metal-made divided body is cast into the cast-metal-made divided body by melting the one end such that an original shape of the one end is disappeared.

2. The manufacturing method of the turbine housing according to claim 1 , wherein the casting step includes:
a wax molding step of molding a wax pattern into a shape of the cast-metal-made divided body into which the one end of the sheet-metal-made divided body is inserted;
a coating step of forming a coating layer on a surface of the wax pattern;
a cavity forming step of forming the cavity by allowing the wax pattern to be disappeared; and
a molten metal step of molding the cast-metal-made divided body by pouring the molten metal into an interior of the cavity in a state in which the cavity is heated to a predetermined temperature, and the predetermined temperature is equal to or high than a temperature at which the wax pattern melts and is a temperature at which a high-temperature oxidation resistance of the sheet metal material is maintained.

3. The manufacturing method of the turbine housing according to claim 2 , wherein in the cavity forming step, the wax pattern is heated at a temperature equal to or higher than a melting point of the wax pattern and at a temperature at which the high-temperature oxidation resistance of the sheet metal material is maintained.

4. The manufacturing method of the turbine housing according to claim 3 , wherein
in the step of forming the sheet-metal-made divided body, a bent portion is formed in the one end of the sheet-metal-made divided body, and
in the wax molding step, the bent portion is insert molded into the wax pattern, and the sheet-metal-made divided body is fixed to the wax pattern.

5. The manufacturing method of the turbine housing according to claim 3 , wherein the wax pattern is molded such that an inner surface of the exhaust gas flow path in the sheet-metal-made divided body is connected to an inner surface of the cast-metal-made divided body smoothly.

6. The manufacturing method of the turbine housing according to claim 1 , wherein in the casting step, an end portion of an exhaust tube is cast into the cast-metal-made divided body by melting the end portion.

7. The manufacturing method of the turbine housing according to claim 6 , wherein other end portion of the exhaust tube is fixed to an exhaust-air-outlet-side flange by being welded.

Assignees

• Marelli Corp

Inventors

• Okamoto Hiroyuki
• Yokoshima Satoru

Classifications

• B22C9/04

  Use of lost patterns · CPC title

• F01D9/06

  Fluid supply conduits to nozzles or the like · CPC title

• F05D2240/14

  Casings or housings protecting or supporting assemblies within · CPC title

• F01D9/026

  Scrolls for radial machines or engines · CPC title

• F05D2220/40

  in turbochargers · CPC title