Method of manufacturing supercharger

Patent metadata

Field	Value
Publication number	US-11028855-B2
Application number	US-201515551660-A
Country	US
Kind code	B2
Filing date	Feb 27, 2015
Priority date	Feb 27, 2015
Publication date	Jun 8, 2021
Grant date	Jun 8, 2021

Abstract

An object is to provide a method of manufacturing a supercharger that can promptly and easily form an abradable layer in a supercharger. A method of manufacturing a supercharger is a method of manufacturing a supercharger including a turbine configured to rotationally drive, and a compressor having an impeller configured to rotate according to rotational force of the turbine and a housing (10) configured to store the impeller, and the method includes a process of applying coating of an abradable material which is to form an abradable layer (20) when being solidified, only to a predetermined range on a surface of the housing (10) via which the impeller and the housing (10) face.

First claim

The invention claimed is:

1. A method of manufacturing a supercharger including a turbine configured to rotationally drive, and a compressor having an impeller configured to rotate according to rotational force of the turbine and a housing configured to store the impeller, the method comprising: a process of applying coating of an abradable material which is to form an abradable layer when being solidified, only to a predetermined range on either one of surfaces of the impeller and the housing via which the impeller and the housing face; and before the process of applying coating of the abradable material, a process of forming a recess portion to separate either one of the surfaces of the impeller and the housing into the predetermined range and an outer range to which coating of the abradable material is not applied, the recess portion being directly adjacent to each of the outer range and the predetermined range, wherein either one of the surfaces is a smoothly continuous surface before the recess portion is formed.

2. A method of manufacturing a supercharger including a turbine configured to rotationally drive, and a compressor having an impeller configured to rotate according to rotational force of the turbine and a housing configured to store the impeller, the method comprising: a process of applying coating of an abradable material which is to form an abradable layer when being solidified, only to a predetermined range on a surface, the surface being either one of surfaces of the impeller and the housing via which the impeller and the housing face; and before the process of applying coating of the abradable material, a process of increasing a roughness degree in an outer range to which coating of the abradable material is not applied, the outer range being directly adjacent to the predetermined range, to be rougher than a roughness degree in the predetermined range, on either one of the surfaces of the impeller and the housing, wherein a region to which coating of the abradable material is applied and a region to which coating of the abradable material is not applied are on the same continuous surface.

3. A method of manufacturing a supercharger including a turbine configured to rotationally drive, and a compressor having an impeller configured to rotate according to rotational force of the turbine and a housing configured to store the impeller, the method comprising: a process of applying coating of an abradable material which is to form an abradable layer when being solidified, only to a predetermined range on either one of surfaces of the impeller and the housing via which the impeller and the housing face, without applying masking, and before the process of applying coating of the abradable material, a process of forming a recess portion to separate either one of the surfaces of the impeller and the housing into the predetermined range and an outer range to which coating of the abradable material is not applied, the recess portion being directly adjacent to each of the outer range and the predetermined range, wherein either one of the surfaces is a smoothly continuous surface before the recess portion is formed.

4. The method of manufacturing a supercharger according to claim 3 , wherein coating of the abradable material is applied using a brush or a pad.

5. The method of manufacturing a supercharger according to claim 3 , further comprising a process of increasing a roughness degree in the outer range to which coating of the abradable material is not applied, the outer range being adjacent to the predetermined range, to be rougher than a roughness degree in predetermined range, on either one of the surfaces of the impeller and the housing, before the process of applying coating of the abradable material.

6. The method of manufacturing a supercharger according to claim 3 , wherein the abradable material contains synthetic resin and fine particles having a self-lubricating property.

7. The method of manufacturing a supercharger according to claim 3 , wherein coating of the abradable material is applied so that a density becomes lower on a surface side of the abradable layer than a density on a side of the impeller or a side of the housing, when the abradable material is solidified.

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Hatanaka Masaya
• Takeuchi Makoto
• Inoguchi Kazuhiko
• Arai Takashi
• Otsubo Hitomi

Classifications

• F05D2240/307

  related to the tip of a rotor blade · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F04D29/4206

  especially adapted for elastic fluid pumps · CPC title

• F04D29/30

  Vanes · CPC title

• F04D29/289

  having provision against erosion or for dust-separation · CPC title