Turbocharger combining axial flow turbine with a compressor stage utilizing active casing treatment

US2016160756A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016160756-A1
Application numberUS-201414904716-A
CountryUS
Kind codeA1
Filing dateJul 17, 2014
Priority dateJul 24, 2013
Publication dateJun 9, 2016
Grant date

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 turbocharger ( 1 ) with an axial flow turbine ( 2 ) includes a compressor stage ( 4 ) using active casing treatment ( 50 ) for choke flow improvement. With switchable slots ( 52, 54 ), one of the slots ( 52 ) may be between the compressors full and splitter blades ( 27, 23 ) and one of the slots ( 54 ) can be located downstream of the compressors splitter blades ( 23 ) to maximize choke flow capacity. In turbochargers with a wastegate assembly, an actuator ( 32 ) may control both a wastegate control valve ( 30 ) and an active casing treatment slot selection valve ( 56 ).

First claim

Opening claim text (preview).

What is claimed is: 1 . A turbocharger ( 1 ) comprising a turbine stage ( 2 ) and a compressor stage ( 4 ), the turbine stage ( 2 ) including a turbine wheel ( 16 ) selected from the group consisting of an axial flow turbine wheel and a mixed-flow turbine wheel, the compressor stage ( 4 ) including a compressor housing ( 20 ), and a compressor wheel ( 28 ) disposed in the compressor housing ( 20 ) and connected to the turbine wheel ( 16 ) via a shaft ( 18 ), wherein the compressor housing ( 20 ) includes active casing treatment ( 50 ) that is configured to control air flow to the compressor wheel ( 28 ). 2 . The turbocharger ( 1 ) of claim 1 , wherein a ratio of the size of the compressor wheel ( 28 ) to the size of the turbine wheel ( 16 ) is in a range of 0.95:1.00 to 1.05:1.00. 3 . The turbocharger ( 1 ) of claim 1 , wherein a ratio of the size of the compressor wheel ( 28 ) to the size of the turbine wheel ( 16 ) is 1.00:1.00. 4 . The turbocharger ( 1 ) of claim 1 , wherein a Blade Speed Ratio of the turbocharger ( 1 ), defined as U/Co, is in a range of 0.75 to 0.90. 5 . The turbocharger ( 1 ) of claim 1 wherein active casing treatment ( 50 ) comprises a slot ( 52 , 54 ) formed in the compressor inlet wall, the slot ( 52 , 54 ) opening facing the compressor wheel ( 28 ) and configured to selectively circulate air relative to the compressor wheel ( 28 ). 6 . The turbocharger ( 1 ) of claim 1 wherein active casing treatment ( 50 ) comprises a first slot ( 52 ) formed in the compressor inlet ( 22 ) wall, the first slot ( 52 ) opening facing the compressor wheel ( 28 ) at a first location, a second slot ( 54 ) formed in the compressor inlet ( 22 ) wall, the second slot ( 54 ) opening facing the compressor wheel ( 28 ) at a second location, a slot selection valve ( 56 ) configured to control gas flow to the first slot ( 52 ) and the second slot ( 54 ), and to permit selection between using the first slot ( 52 ) and using the second slot ( 54 ). 7 . The turbocharger ( 1 ) of claim 6 wherein the second location comprises a location downstream of a leading edge ( 21 ) of splitter blades ( 23 ) of the compressor wheel ( 28 ). 8 . The turbocharger ( 1 ) of claim 6 wherein the first location comprises a location between a leading edge ( 25 ) of full blades ( 27 ) of the compressor wheel ( 28 ) and a leading edge ( 21 ) of splitter blades ( 23 ) of the compressor wheel ( 28 ). 9 . The turbocharger ( 1 ) of claim 6 , wherein the turbine stage ( 2 ) comprises a wastegate valve ( 30 ) and the turbocharger ( 1 ) includes a single actuator ( 32 ) configured to control both the position of the wastegate valve ( 30 ) and the slot selection valve ( 56 ). 10 . The turbocharger ( 1 ) of claim 1 , wherein the turbine wheel ( 16 ) is an axial flow turbine wheel.

Assignees

Inventors

Classifications

  • Improving ICE efficiencies · CPC title

  • F02C6/12Primary

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

  • F02B37/183Primary

    Arrangements of bypass valves or actuators therefor · CPC title

  • in turbochargers · CPC title

  • by bleeding, bypassing or recycling fluids (influencing the boundary layer by an uncontrolled bleeding of the working fluid F04D29/681) · 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 US2016160756A1 cover?
A turbocharger ( 1 ) with an axial flow turbine ( 2 ) includes a compressor stage ( 4 ) using active casing treatment ( 50 ) for choke flow improvement. With switchable slots ( 52, 54 ), one of the slots ( 52 ) may be between the compressors full and splitter blades ( 27, 23 ) and one of the slots ( 54 ) can be located downstream of the compressors splitter blades ( 23 ) to maximize choke flow …
Who is the assignee on this patent?
Borgwarner Inc
What technology area does this patent fall under?
Primary CPC classification F02C6/12. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Thu Jun 09 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). 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).