Turbine wheel

US9915152B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9915152-B2
Application numberUS-201314425660-A
CountryUS
Kind codeB2
Filing dateSep 11, 2013
Priority dateSep 19, 2012
Publication dateMar 13, 2018
Grant dateMar 13, 2018

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  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

A turbine wheel ( 4 ) having a hub ( 29 ); a multiplicity of turbine wheel blades ( 30 ) arranged around the hub ( 29 ); a turbine wheel back wall ( 31 ) which is arranged on the hub ( 29 ) adjacent to an edge region ( 32 ) of the turbine wheel blades ( 30 ); wherein the wall thickness (W) of the turbine wheel ( 4 ) back wall is reduced in regions.

First claim

Opening claim text (preview).

The invention claimed is: 1. A turbine wheel ( 4 ) having a hub ( 29 ) including a radially enlarged disc-like portion of the hub, the disc-like portion defining a floor on one side and a backwall ( 31 ) on the other side and a radially outer edge, with a wall defined between the floor and the backwall ( 31 ); and a multiplicity of turbine wheel blades ( 30 ) arranged around the hub ( 29 ); wherein the radially outer edge has regions with a first wall thickness (W) and regions with a reduced wall thickness compared to the first wall thickness (W) of the radially enlarged disc-like portion of the hub, the turbine wheel back wall ( 31 ) regions of reduced thickness are defined by pockets ( 33 ) which are open radially outwardly, and the pockets ( 33 ) do not extend through the entire wall thickness (W) of the turbine wheel backwall ( 31 ). 2. The turbine wheel as claimed in claim 1 , wherein the pockets ( 33 ) are arranged on the outer edge region of the turbine wheel backwall ( 31 ) between blades. 3. An exhaust-gas turbocharger ( 1 ) having a turbine housing ( 2 ) in which is arranged a turbine wheel ( 4 ) which has: a hub ( 29 ) including a radially enlarged disc-like portion of the hub, the disc-like portion defining a floor on one side and a backwall ( 31 ) on the other side and a radially outer edge, with a wall defined between the floor and the backwall ( 31 ); and a multiplicity of turbine wheel blades ( 30 ) arranged around the hub ( 29 ); wherein the radially outer edge has regions with a first wall thickness (W) and regions with a reduced wall thickness compared to the first wall thickness (W) of the radially enlarged disc-like portion of the hub, and the pockets ( 33 ) do not extend through the entire wall thickness (W) of the turbine wheel backwall ( 31 ). 4. The exhaust-gas turbocharger as claimed in claim 3 , wherein the turbine wheel back wall ( 31 ) has at least one pocket ( 33 ) which is open radially outwardly. 5. The exhaust-gas turbocharger as claimed in claim 3 , wherein the pockets ( 33 ) are arranged on the radially outer edge of the turbine wheel backwall ( 31 ).

Assignees

Inventors

Classifications

  • machined; miscellaneous · CPC title

  • Preventing, counteracting or reducing vibration or noise · CPC title

  • Engines characterised by provision of pumps driven at least for part of the time by exhaust · CPC title

  • in turbochargers · CPC title

  • F01D5/225Primary

    by shrouding · CPC title

Patent family

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External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US9915152B2 cover?
A turbine wheel ( 4 ) having a hub ( 29 ); a multiplicity of turbine wheel blades ( 30 ) arranged around the hub ( 29 ); a turbine wheel back wall ( 31 ) which is arranged on the hub ( 29 ) adjacent to an edge region ( 32 ) of the turbine wheel blades ( 30 ); wherein the wall thickness (W) of the turbine wheel ( 4 ) back wall is reduced in regions.
Who is the assignee on this patent?
Borgwarner Inc
What technology area does this patent fall under?
Primary CPC classification F01D5/225. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Mar 13 2018 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 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).