Heat shield with centering features

US9988977B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9988977-B2
Application numberUS-201514870643-A
CountryUS
Kind codeB2
Filing dateSep 30, 2015
Priority dateOct 14, 2014
Publication dateJun 5, 2018
Grant dateJun 5, 2018

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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 turbocharger ( 10 ) includes a shaft ( 26 ) rotatably supported within a bearing housing ( 28 ), a turbine wheel ( 22 ) connected to the shaft ( 26 ), and a heat shield ( 150, 250 ) disposed between the turbine wheel ( 22 ) and the bearing housing ( 28 ). The heat shield ( 150, 250 ) includes surface features ( 80, 180 ) formed on at least one of a sidewall ( 57 ) portion thereof and a flange ( 63 ) portion thereof that locate the heat shield ( 150, 250 ) relative to the bearing housing ( 28 ) such that the heat shield ( 150, 250 ) is coaxial with the rotational axis of the shaft ( 26 ).

First claim

Opening claim text (preview).

What is claimed is: 1. A turbocharger ( 10 ) comprising a bearing housing ( 28 ), a shaft ( 26 ) rotatably supported within the bearing housing ( 28 ), a turbine housing ( 14 ) connected to the bearing housing ( 28 ), a turbine wheel ( 22 ) disposed in the turbine housing ( 14 ) and connected to the shaft ( 26 ), and a heat shield ( 150 ) including a radially extending base ( 51 ) having a central opening ( 52 ) that receives the shaft ( 26 ), a radially extending flange ( 63 ) that is axially offset from the radially extending base ( 51 ), and a sidewall ( 57 ) extending between the base ( 51 ) and the flange ( 63 ), the sidewall ( 57 ) having a first end ( 58 ) connected to a radially-outermost end of the base ( 51 ), and a second end ( 59 ) that is opposed to the first end ( 58 ) and connected to a radially-innermost end ( 65 ) of the flange ( 63 ), wherein the heat shield ( 150 ) includes surface features ( 80 ) formed on the flange ( 63 ) that locate the heat shield ( 150 ) relative to the bearing housing ( 28 ), the surface features ( 80 ) comprising an axially protruding ridge ( 82 ) that is formed in the flange ( 63 ), the ridge ( 82 ) being received within a circumferential groove ( 23 ) formed in the bearing housing ( 28 ) whereby the heat shield ( 150 ) is located relative to the bearing housing ( 28 ) such that the heat shield ( 150 , 250 ) is co-axial with the rotational axis of the shaft ( 26 ). 2. The turbocharger ( 10 ) of claim 1 , wherein the axially protruding ridge ( 82 ) is convex on a bearing housing-facing surface ( 66 ) of the flange ( 63 ), and concave on a turbine housing-facing surface ( 67 ) of the flange ( 63 ). 3. The turbocharger ( 10 ) of claim 1 , wherein the ridge ( 82 ) is continuous in a circumferential direction. 4. The turbocharger ( 10 ) of claim 1 , wherein the ridge ( 82 ) is formed at a location of the flange ( 63 ) that adjoins the sidewall ( 57 ). 5. The turbocharger ( 10 ) of claim 1 , wherein the bearing housing ( 28 ) includes a nose ( 29 ) on the turbine housing-facing surface ( 28 a ) of the bearing housing ( 28 ), axially protruding towards the turbine housing ( 14 ) and centered on a shaft-receiving bore ( 30 ), and wherein a radial clearance is provided between the central opening ( 52 ) of the heat shield ( 150 ) and the bearing housing nose ( 29 ). 6. A turbocharger ( 10 ) comprising a bearing housing ( 28 ), a shaft ( 26 ) rotatably supported within the bearing housing ( 28 ), a turbine housing ( 14 ) connected to the bearing housing ( 28 ), a turbine wheel ( 22 ) disposed in the turbine housing ( 14 ) and connected to the shaft ( 26 ), and a heat shield ( 250 ) including a radially extending base ( 51 ) having a central opening ( 52 ) that receives the shaft ( 26 ), a radially extending flange ( 63 ) that is axially offset from the radially extending base ( 51 ), and a sidewall ( 57 ) extending between the base ( 51 ) and the flange ( 63 ), the sidewall ( 57 ) having a first end ( 58 ) connected to a radially-outermost end of the base ( 51 ), and a second end ( 59 ) that is opposed to the first end ( 58 ) and connected to a radially-innermost end ( 65 ) of the flange ( 63 ), wherein the heat shield ( 250 ) includes surface features ( 180 ) formed on the sidewall ( 57 ) that locate the heat shield ( 250 ) relative to the bearing housing ( 28 ), the surface features ( 180 ) including radially inward-extending protrusions ( 182 , 282 ) that are spaced along a circumference of the sidewall ( 57 ), a radially inward-facing surface ( 60 a ) of the protrusions ( 182 , 282 ) abutting a radially outward-facing surface ( 28 b ) of the bearing housing ( 28 ), whereby the heat shield ( 250 ) is located relative to the bearing housing ( 28 ) such that the heat shield ( 150 , 250 ) is co-axial with the rotational axis of the shaft ( 26 ). 7. The turbocharger ( 10 ) of claim 6 , wherein a ratio (Ls/Lp) of a circumferential dimension (Ls) of the sidewall ( 57 ) to a circumferential dimension (Lp) of the protrusion ( 182 ) is in a range of 20 to 100. 8. The turbocharger ( 10 ) of claim 6 , wherein the heat shield ( 250 ) includes three protrusions ( 182 , 282 ). 9. The turbocharger ( 10 ) of claim 6 , wherein a dimension (Lp) of the protrusion ( 182 , 282 ) in a circumferential direction is less than 10% of a circumferential dimension (Ls) of the sidewall ( 57 ) without protrusion. 10. The turbocharger ( 10 ) of claim 6 , wherein the bearing housing ( 28 ) includes a nose ( 29 ) on the turbine housing-facing surface ( 28 a ) of the bearing housing ( 28 ), axially protruding towards the turbine housing ( 14 ) and centered on a shaft-receiving bore ( 30 ), and wherein a radial clearance is provided between the central opening ( 52 ) of the heat shield ( 250 ) and the bearing housing nose ( 29 ).

Assignees

Inventors

Classifications

  • Ceramic matrix composites [CMC] · CPC title

  • for sliding contact bearing · CPC title

  • Heating, heat insulation or cooling means · CPC title

  • in turbochargers · CPC title

  • F02B39/14Primary

    Lubrication of pumps; Safety measures therefor · CPC title

Patent family

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Frequently asked questions

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What does patent US9988977B2 cover?
A turbocharger ( 10 ) includes a shaft ( 26 ) rotatably supported within a bearing housing ( 28 ), a turbine wheel ( 22 ) connected to the shaft ( 26 ), and a heat shield ( 150, 250 ) disposed between the turbine wheel ( 22 ) and the bearing housing ( 28 ). The heat shield ( 150, 250 ) includes surface features ( 80, 180 ) formed on at least one of a sidewall ( 57 ) portion thereof and a flange…
Who is the assignee on this patent?
Borgwarner Inc
What technology area does this patent fall under?
Primary CPC classification F02B39/14. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jun 05 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).