Turbocharger and turbine wheel

US11346226B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11346226-B2
Application numberUS-201716472558-A
CountryUS
Kind codeB2
Filing dateDec 22, 2017
Priority dateDec 23, 2016
Publication dateMay 31, 2022
Grant dateMay 31, 2022

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  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 (100) for a turbocharger includes a hub (110) and blades (120). The hub includes a primary outer surface (116), a back wall surface (115), a peripheral edge (119) extending between the primary outer surface and the back wall surface, and a central axis (111). The hub has a back wall thickness measured parallel to the central axis from the primary outer surface to the back wall surface. The blades (120) extend from the primary outer surface of the hub and are integrally formed with the hub by casting. Each blade has a blade thickness measured tangential to the central axis between opposed surfaces of the blade. A maximum diameter of the peripheral edge is 60 mm or more. Over a majority of a radially outer region (117), a thickness ratio of the blade thickness to the back wall thickness varies by 25% or less. The radially outer region extends from the peripheral edge to a 25% meridional.

First claim

Opening claim text (preview).

What is claimed is: 1. A turbine wheel ( 100 ) for a turbocharger ( 10 ) comprising: a hub ( 110 ) having a primary outer surface ( 116 ), a back wall surface ( 115 ), a peripheral edge ( 119 ) extending between the primary outer surface ( 116 ) and the back wall surface ( 115 ), and a central axis ( 111 ), wherein the hub ( 110 ) has a back wall thickness that is measured parallel to the central axis ( 111 ) from the primary outer surface ( 116 ) to the back wall surface ( 115 ); and a plurality of blades ( 120 ) extending from the primary outer surface ( 116 ) of the hub ( 110 ) and integrally formed with the hub ( 110 ) via a casting process, wherein each of the blades ( 120 ) has a blade thickness that is measured tangential to the central axis ( 111 ) between opposed surfaces ( 123 , 124 ) of the blade ( 120 ); wherein a diameter of the peripheral edge ( 119 ) is 60 mm or more; and wherein over a majority of a radially outer region ( 117 ), a thickness ratio of the blade thickness to the back wall thickness is between 0.8 and 1.2, the radially outer region ( 117 ) extending from the peripheral edge ( 119 ) to a 25% meridional distance along the primary outer surface ( 116 ), wherein the majority includes a 15% meridional range along the primary outer surface ( 116 ). 2. The turbine wheel ( 100 ) according to claim 1 , wherein over the majority of the radially outer region ( 117 ), the thickness ratio varies by 15% or less. 3. The turbine wheel ( 100 ) according to claim 1 , wherein at the 25% meridional distance, the back wall thickness is 6% or less than the maximum diameter. 4. The turbine wheel ( 100 ) according to claim 1 , further comprising fillets ( 125 ) between each of the blades ( 120 ) and the primary outer surface ( 116 ) and formed integrally therewith via the casting process, wherein the back wall thickness and the blade thickness are measured without the fillets ( 125 ). 5. The turbine wheel ( 100 ) according to claim 1 , wherein over the majority of the radially outer region ( 117 ), the thickness ratio varies by 25% or less. 6. The turbine wheel ( 100 ) according to claim 1 , wherein the thickness ratio of the blade thickness to the back wall thickness varies by 25% or less. 7. The turbine wheel ( 100 ) according to claim 1 , wherein the thickness ratio of the blade thickness to the back wall thickness is one or less.

Assignees

Inventors

Classifications

  • F01D5/048Primary

    Form or construction · CPC title

  • Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure · CPC title

  • in turbochargers · CPC title

  • of radial insertion type, e.g. in individual recesses · CPC title

  • Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

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

What does patent US11346226B2 cover?
A turbine wheel (100) for a turbocharger includes a hub (110) and blades (120). The hub includes a primary outer surface (116), a back wall surface (115), a peripheral edge (119) extending between the primary outer surface and the back wall surface, and a central axis (111). The hub has a back wall thickness measured parallel to the central axis from the primary outer surface to the back wall s…
Who is the assignee on this patent?
Borgwarner Inc
What technology area does this patent fall under?
Primary CPC classification F01D5/048. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue May 31 2022 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 12 related publications on this page (citations in our corpus or others sharing the same primary CPC).