Turbocharger device and method for mounting a turbocharger device

US11333040B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11333040-B2
Application numberUS-202016844456-A
CountryUS
Kind codeB2
Filing dateApr 9, 2020
Priority dateOct 10, 2017
Publication dateMay 17, 2022
Grant dateMay 17, 2022

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  1. Title

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  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

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  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A turbocharger device for an internal combustion engine and a method for mounting a turbocharger device are described. The turbocharger device has a housing with a locating hole, in which a turbocharger shaft is mounted by two rolling element bearings. A rolling element bearing sleeve is situated between the two rolling element bearings. The rolling element bearing sleeve and hence the two rolling element bearings are fixed with the turbocharger shaft in the axial direction with the aid of two pins, which are introduced through a hole in the housing and are pressed into a groove in the rolling element bearing sleeve. During this process, the beveled tips of the pins slide along the chamfered outer edges of the groove as far as an end position, which fixes the axial position of the rolling element bearing sleeve.

First claim

Opening claim text (preview).

What is claimed is: 1. A turbocharger device for an internal combustion engine, comprising: a housing having a housing axis; a turbine wheel; a compressor wheel; a common turbocharger shaft, the turbine wheel and compressor wheel arranged on the common turbocharger shaft; a plurality of rolling element bearings which are spaced apart from one another in an axial direction of the common turbocharger shaft; a rolling element bearing sleeve, which is arranged between and spaces two of the plurality of rolling element bearings apart; a locating hole formed as part of the housing, the common turbocharger shaft mounted in the locating hole in the housing of the turbocharger device by the plurality of rolling element bearings; a groove formed on the outside of the rolling element bearing sleeve, such that the groove extends in a circumferential direction; a plurality of chamfered outer edges integrally formed as part of the groove; a hole integrally formed as part of the housing of the turbocharger device, such that the hole extends perpendicularly to the housing axis; and at least two pins, wherein the at least two pins are arranged in the hole such that the at least two pins are pressed against the chamfered outer edges of the groove. 2. The turbocharger device of claim 1 , wherein the plurality of chamfered outer edges of the groove are chamfered at different angles. 3. The turbocharger device of claim 1 , wherein each of the at least two pins is of semicircular design in cross section. 4. The turbocharger device of claim 3 , wherein the at least two pins together form a full circle in cross section in the state in which the at least two pins are inserted into the hole. 5. The turbocharger device of claim 1 , wherein at least one of the tips or heads of each of the at least two pins is designed as a partial cone. 6. The turbocharger device of claim 1 , wherein the combined outside diameter of the at least two pins is greater than the width of the groove formed as part of the rolling element bearing sleeve. 7. The turbocharger device of claim 1 , wherein the contact between at least one of tips or heads of the pins and at least one of the plurality of chamfered outer edges of the groove further comprises one of a point, line, or surface contact. 8. The turbocharger device of claim 1 , wherein the at least two pins are arranged in the hole spaced apart from one another. 9. A method for mounting a turbocharger device, comprising the steps of: providing a housing having a housing axis; providing a common turbocharger shaft; providing a plurality of rolling element bearings; providing a rolling element bearing sleeve; providing a groove formed on the outside of the rolling element bearing sleeve, such that the groove extends in a circumferential direction; providing a plurality of chamfered outer edges being formed as part of the groove; providing a hole integrally formed as part of the housing of the turbocharger device, and the hole extends perpendicularly to the housing axis; and providing at least two pins; mounting the plurality of rolling element bearings and the rolling element bearing sleeve onto the common turbocharger shaft; pushing the housing over the plurality of rolling element bearings and the rolling element bearing sleeve until the groove in the rolling element bearing sleeve and the hole in the housing are substantially aligned relative to one another; arranging the at least two pins into the hole integrally formed as part of the housing; pressing at least one of tips or heads of the at least two pins against one or more of the plurality of chamfered outer edges of the groove to fix the rolling element bearing sleeve in an axial direction.

Assignees

Inventors

Classifications

  • Axial thrust bearings · CPC title

  • F01D25/162Primary

    Bearing supports · CPC title

  • in turbochargers · CPC title

  • Bearings · CPC title

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

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Frequently asked questions

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What does patent US11333040B2 cover?
A turbocharger device for an internal combustion engine and a method for mounting a turbocharger device are described. The turbocharger device has a housing with a locating hole, in which a turbocharger shaft is mounted by two rolling element bearings. A rolling element bearing sleeve is situated between the two rolling element bearings. The rolling element bearing sleeve and hence the two roll…
Who is the assignee on this patent?
Vitesco Tech Gmbh
What technology area does this patent fall under?
Primary CPC classification F01D25/162. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue May 17 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).