IP Library › Granted Patent US 11,371,367
Granted Patent B2
US 11,371,367 · App. 16/955,538 · Granted Jun 28, 2022

Manufacturing method of turbine housing

Inventors: Hiroyuki Okamoto (Saitama, JP); Satoru Yokoshima (Saitama, JP)
Assignee: Marelli Corporation
F01D9/02B22C7/02B22C9/04B22D19/04F01D9/06F01N13/1872F02B39/00F01N2470/06
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Quick Facts
Patent No.
US 11,371,367
App. No.
16/955,538
Granted
Jun 28, 2022
Kind
B2
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.

Claims (16)

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.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 30, 2020
From: OKAMOTO, HIROYUKI; YOKOSHIMA, SATORU
To: MARELLI CORPORATION
Reel/Frame 054227/0600 →
Priority Claims (2)
JP JP2017-245806 · Dec 22, 2017 · national
JP JP2018-103311 · May 30, 2018 · national
Continuity (1)
Related Publication 20200318487A1 · Oct 8, 2020