Linkage for exhaust bypass valve of multi-stage turbocharger

US10094272B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10094272-B2
Application numberUS-201615192615-A
CountryUS
Kind codeB2
Filing dateJun 24, 2016
Priority dateJul 17, 2015
Publication dateOct 9, 2018
Grant dateOct 9, 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.

An assembly for an exhaust bypass valve of a two-stage turbocharger can include a first turbocharger stage; a second turbocharger stage; an exhaust bypass valve that includes an open state and a closed state; and a linkage mechanism that links the exhaust bypass valve to an actuator where the linkage mechanism includes a locked state for the closed state of the exhaust bypass valve.

First claim

Opening claim text (preview).

What is claimed is: 1. An assembly for an exhaust bypass valve of a two-stage turbocharger, the assembly comprising: a first turbocharger stage; a second turbocharger stage; an exhaust bypass valve that comprises an open state and a closed state; an actuator; and a linkage mechanism that links the exhaust bypass valve to the actuator; wherein the linkage mechanism comprises a locked, closed state wherein the linkage mechanism is in a locked position for the closed state of the exhaust bypass valve; wherein the linkage mechanism comprises a movable axle and a casing; wherein the casing comprises two parallel plates and at least one fixed support, and wherein each of the two parallel plates comprises a respective seating feature that comprises a notch that seats the movable axle or a guide that seats the movable axle; and wherein the linkage mechanism comprises at least one spring being operatively coupled to at least one of the at least one fixed support to apply a force to the movable axle wherein the force biases the movable axle with respect to the respective seating features of the two parallel plates. 2. The assembly of claim 1 wherein, in the locked, closed state, the force is a locking force. 3. The assembly of claim 1 wherein the at least one spring comprises at least one coned washer. 4. The assembly of claim 1 wherein the linkage mechanism comprises at least four axles and at least four axle-to-axle links wherein the at least four axles comprise at least one fixed axle and at least three movable axles. 5. The assembly of claim 1 wherein the linkage mechanism comprises two end axles and three intermediate axles wherein the end axles are at fixed positions, wherein one of the end axles is rotatable to position the exhaust bypass valve in the open state and in the closed state, wherein one of the intermediate axles is the movable axle, and wherein another one of the intermediate axles is coupled to the actuator. 6. The assembly of claim 1 wherein the linkage mechanism comprises a zero point that corresponds to the closed state of the exhaust bypass valve, a first displacement to one side of the zero point that corresponds to the locked position of the locked, closed state and a second displacement to another side of the zero point that corresponds to the open state of the exhaust bypass valve. 7. The assembly of claim 1 wherein the exhaust bypass valve, in the open state, allows at least a portion of exhaust gas of an internal combustion engine to bypass one of the turbocharger stages. 8. The assembly of claim 1 wherein the first turbocharger stage comprises a low-pressure turbocharger and wherein the second turbocharger stage comprises a high-pressure turbocharger. 9. The assembly of claim 1 wherein in the open state of the exhaust bypass valve, a path exists for at least a portion of exhaust gas of an internal combustion engine to bypass the first turbocharger stage. 10. The assembly of claim 1 wherein the linkage mechanism comprises a first link that is fixed to a shaft of the exhaust bypass valve, a second link, a third link and a fourth link wherein a first axle links the first and second links, wherein a second axle links the second and third links and wherein a third axle links the third and fourth links. 11. The assembly of claim 10 further comprising a fifth link that is linked to the second axle for coupling the linkage mechanism to an actuator. 12. The assembly of claim 10 wherein the third axle is the movable axle. 13. An assembly for an exhaust bypass valve of a two-stage turbocharger, the assembly comprising: a first turbocharger stage; a second turbocharger stage; an exhaust bypass valve that comprises an open state and a closed state; an actuator; and a linkage mechanism that links the exhaust bypass valve to the actuator wherein the linkage mechanism that is positionable in a locked state for the closed state of the exhaust bypass valve, wherein the linkage mechanism comprises two end axles and three intermediate axles wherein the end axles are at fixed positions, wherein one of the end axles is rotatable to position the exhaust bypass valve in the open state and in the closed state, wherein one of the intermediate axles is biased by a biasing mechanism, and wherein another one of the intermediate axles is coupled to the actuator.

Assignees

Inventors

Classifications

  • F02B37/186Primary

    Arrangements of actuators or linkage for bypass valves · CPC title

  • comprising a pivoted disc or flap · CPC title

  • Cross-Sectional Technologies · mapped topic

  • for conveying or interconverting oscillating or reciprocating motions · CPC title

  • specially adapted operating means therefor (operating means per se F16K31/00) · CPC title

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Frequently asked questions

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What does patent US10094272B2 cover?
An assembly for an exhaust bypass valve of a two-stage turbocharger can include a first turbocharger stage; a second turbocharger stage; an exhaust bypass valve that includes an open state and a closed state; and a linkage mechanism that links the exhaust bypass valve to an actuator where the linkage mechanism includes a locked state for the closed state of the exhaust bypass valve.
Who is the assignee on this patent?
Honeywell Int Inc
What technology area does this patent fall under?
Primary CPC classification F02B37/186. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Oct 09 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 5 related publications on this page (citations in our corpus or others sharing the same primary CPC).