Turbine housing assembly and manufacturing method of turbine housing assembly

US9835165B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9835165-B2
Application numberUS-201314387104-A
CountryUS
Kind codeB2
Filing dateMar 22, 2013
Priority dateMar 23, 2012
Publication dateDec 5, 2017
Grant dateDec 5, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A turbine housing assembly includes a plurality of constituent members connected to one another and easily manufactured. The turbine housing assembly includes a scroll part, an annular lid part, an exhaust gas outlet and a connection part connectable to a bearing housing for a turbine shaft. The scroll part and the connection part are each formed of a single piece of sheet metal and each is welded to the annular lid part that is orthogonal to a turbine axial direction so that the scroll part and the connection part are connected to each other via the annular lid part. Such a turbine housing assembly is of reduced weight, is quite easy to manufacture, of reduced cost, and can be made, at least in part, of materials having lower heat capacity as compared to conventional turbine housings made of sheet metal.

First claim

Opening claim text (preview).

The invention claimed is: 1. A turbine housing assembly including a plurality of constituent members connected to one another to constitute a turbine housing into which a turbine wheel rotated by exhaust gas introduced from an engine is inserted, the turbine housing assembly at least comprising: a scroll part made of sheet metal having a bottomed cylindrical shape, a surrounding wall part and a bottom face part, the scroll part including: an exhaust gas flow path of a spiral shape formed inside the bottomed cylindrical shape and configured such that exhaust gas that has flowed in from an exhaust gas inlet flows through the exhaust gas flow path; and an exhaust gas outlet having a through hole formed on the bottom face part, the exhaust gas outlet being configured such that the exhaust gas that has flowed through the exhaust gas flow path flows out from the exhaust gas outlet; a connection part made of sheet metal and connectable to a bearing housing that houses a bearing for supporting a rotation shaft of the turbine wheel, said connection part comprising bushing holes, an annular lid part orthogonal to a turbine axial direction, the scroll part being welded to one surface of the annular lid part and the connection part being welded to the other surface of the annular lid part, wherein the annular lid part includes a flat plate-like part of an annular shape and a positioning portion protruding outwardly from the flat plate-like part, and an end face of a threaded bushing is inserted into a bushing insertion hole formed on the connection part and connected to the positioning portion of the annular lid part. 2. The turbine housing assembly according to claim 1 , wherein the connection part is made of a material that has lower heat resistance strength than the scroll part. 3. The turbine housing assembly according to claim 2 , wherein the connection part is made of a material that contains less nickel than the scroll part. 4. The turbine housing assembly according to claim 1 , wherein the annular lid part comprises a separate body separate from the scroll part and the connection part. 5. The turbine housing assembly according to claim 4 , wherein the annular lid part is formed of a single piece of sheet metal. 6. The turbine housing assembly according to claim 4 , further comprising an exhaust part of a tubular shape comprising a separate body separate from the scroll part, wherein the exhaust part is connected to the scroll part in the turbine axial direction so that the exhaust part is in communication with the exhaust gas outlet. 7. The turbine housing assembly according to claim 1 , further comprising a variable nozzle mechanism configured to adjust flow of the exhaust gas flowing toward the turbine wheel, the variable nozzle mechanism being inserted into the scroll part and the connection part. 8. A manufacturing method for a turbine housing assembly including a plurality of constituent members connected to one another to constitute a turbine housing into which a turbine wheel rotated by exhaust gas introduced from an engine is inserted, the manufacturing method comprising: forming a scroll part of a single piece of sheet metal, the scroll part having: a bottomed cylindrical shape including a surrounding wall part and a bottom face part; an exhaust gas flow path of a spiral shape formed inside the bottomed cylindrical shape, the exhaust gas flow path being configured such that exhaust gas that has flowed in from an exhaust gas inlet flows through the exhaust gas flow path; and an exhaust gas outlet having a through hole formed on the bottom face part, the exhaust gas outlet being configured such that the exhaust gas that has flowed through the exhaust gas flow path flows out from the exhaust gas outlet; forming a connection part of a single piece of sheet metal, the connection part being connectable to a bearing housing that houses a bearing for supporting a rotation shaft of the turbine wheel, said connection part comprising bushing insertion holes; forming an annular lid part of a flat plate-like annular shape of a single piece of sheet metal, the annular lid part including a flat plate-like part of an annular shape and a positioning portion protruding outwardly from the flat plate-like part; and arranging the annular lid part to be orthogonal to a turbine axial direction, welding the scroll part to one side of the annular lid part, and welding the connection part to other side of the annular lid part, wherein said method further comprising inserting an end face of a threaded bushing into a bushing insertion hole formed on the connection part and connecting the connecting part to the positioning portion of the annular lid part. 9. The manufacturing method for a turbine housing assembly according to claim 8 , further comprising preparing an exhaust part of a tubular shape comprising a separate body separate from the scroll part, and connecting the exhaust part to the scroll part in the turbine axial direction so that the exhaust part is in communication with the exhaust gas outlet of the scroll part.

Assignees

Inventors

Classifications

  • by sheet metal manufacturing · CPC title

  • in turbochargers · CPC title

  • for compressing or evacuating · CPC title

  • by welding · CPC title

  • Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member · CPC title

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What does patent US9835165B2 cover?
A turbine housing assembly includes a plurality of constituent members connected to one another and easily manufactured. The turbine housing assembly includes a scroll part, an annular lid part, an exhaust gas outlet and a connection part connectable to a bearing housing for a turbine shaft. The scroll part and the connection part are each formed of a single piece of sheet metal and each is wel…
Who is the assignee on this patent?
Mitsubishi Heavy Ind Ltd
What technology area does this patent fall under?
Primary CPC classification F01D9/026. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Dec 05 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).