Multiple bank exhaust system comprising reductant supply system arranged upstream of a turbine

US11149622B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11149622-B2
Application numberUS-201716337246-A
CountryUS
Kind codeB2
Filing dateAug 22, 2017
Priority dateSep 30, 2016
Publication dateOct 19, 2021
Grant dateOct 19, 2021

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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.

Provided is an exhaust system for an internal combustion engine comprising: a first exhaust conduit leading from a first exhaust bank of the engine to a first turbocharger turbine inlet arranged downstream of the first exhaust bank in the direction of travel of a first exhaust stream; a second exhaust conduit leading from a second exhaust bank of the engine to a second turbocharger turbine inlet arranged downstream of the second exhaust bank in the direction of travel of a second exhaust stream; an SCR catalyst arranged downstream of the first turbocharger turbine inlet and/or second turbocharger turbine inlet; and a reductant supply system comprising a distributor pipe and a reductant injector. The distributor pipe is configured to fluidly connect the first exhaust conduit to the second exhaust conduit upstream of the first turbocharger turbine inlet and second turbocharger turbine inlet, and the reductant injector is configured to supply a reductant to the distributor pipe.

First claim

Opening claim text (preview).

The invention claimed is: 1. An exhaust system for an internal combustion engine, the exhaust system comprising: a first exhaust conduit leading from a first exhaust bank of the internal combustion engine to a first turbocharger turbine inlet arranged downstream of the first exhaust bank in the direction of travel of a first exhaust stream; a second exhaust conduit leading from a second exhaust bank of the internal combustion engine to a second turbocharger turbine inlet arranged downstream of the second exhaust bank in the direction of travel of a second exhaust stream; an SCR catalyst arranged downstream of the first turbocharger turbine inlet and/or second turbocharger turbine inlet; a reductant supply system comprising a distributor pipe and a reductant injector, wherein the distributor pipe is configured to fluidly connect the first exhaust conduit to the second exhaust conduit upstream of the first turbocharger turbine inlet and second turbocharger turbine inlet, and wherein the reductant injector is configured to supply a reductant to the distributor pipe; and thermal insulation arranged at a junction of a surface of a first end of the distributor pipe and a surface of the first exhaust conduit, said thermal insulation in contact with the surface of the first end of the distributor pipe and extending along at least a portion of the surface of the first exhaust conduit, to thereby thermally insulate the surface of the distribution pipe from the first exhaust conduit. 2. The exhaust system according to claim 1 , wherein the distributor pipe is equipped with a cooling sleeve configured to circulate a fluid through the cooling sleeve. 3. The exhaust system according to claim 2 , wherein the cooling sleeve is fluidly connected to a cooling system for the internal combustion engine. 4. The exhaust system according to claim 2 , wherein the cooling sleeve is fluidly connected to a reductant storage tank. 5. The exhaust system according to claim 1 , wherein the first turbocharger turbine inlet is associated with a first turbocharger turbine and the second turbocharger turbine inlet is associated with a second turbocharger turbine. 6. The exhaust system according to claim 1 , wherein a wastegate is arranged in association with the first turbocharger turbine inlet and/or the second turbocharger turbine inlet. 7. The exhaust system according to claim 1 , wherein the first turbocharger turbine inlet has a different geometry to the second turbocharger turbine inlet. 8. The exhaust system according to claim 1 , wherein a collective exhaust conduit configured to convey the first exhaust stream and second exhaust stream is arranged downstream of the first turbocharger turbine inlet and second turbocharger turbine inlet. 9. The exhaust system according to claim 1 further comprising thermal insulation arranged at a junction of a surface of a second end of the distributor pipe and a surface of the second exhaust conduit and, said thermal insulation in contact with the surface of the second end of the distributor pipe and extending along at least a portion of the surface of the second exhaust conduit. 10. An exhaust system for an internal combustion engine, the exhaust system comprising: a first exhaust conduit leading from a first exhaust bank of the internal combustion engine to a first turbocharger turbine inlet arranged downstream of the first exhaust bank in the direction of travel of a first exhaust stream; a second exhaust conduit leading from a second exhaust bank of the internal combustion engine to a second turbocharger turbine inlet arranged downstream of the second exhaust bank in the direction of travel of a second exhaust stream, wherein the first turbocharger turbine inlet and second turbocharger turbine inlet are associated with a single turbocharger turbine; an SCR catalyst arranged downstream of the first turbocharger turbine inlet and/or second turbocharger turbine inlet; and a reductant supply system comprising a distributor pipe and a reductant injector, wherein the distributor pipe is configured to fluidly connect the first exhaust conduit to the second exhaust conduit upstream of the first turbocharger turbine inlet and second turbocharger turbine inlet, and wherein the reductant injector is configured to supply a reductant to the distributor pipe. 11. A method of supplying a reductant to an exhaust stream of an exhaust system for an internal combustion engine, the exhaust system comprising: a first exhaust conduit leading from a first exhaust bank of the internal combustion engine to a first turbocharger turbine inlet arranged downstream of the first exhaust bank in the direction of travel of a first exhaust stream; a second exhaust conduit leading from a second exhaust bank of the internal combustion engine to second turbocharger turbine inlet arranged downstream of the second exhaust bank in the direction of travel of a second exhaust stream; an SCR catalyst arranged downstream of the first turbocharger turbine inlet and/or second turbocharger turbine inlet; and a reductant supply system comprising a distributor pipe and a reductant injector; wherein the distributor pipe is configured to fluidly connect the first exhaust conduit to the second exhaust conduit upstream of the first turbocharger turbine inlet and second turbocharger turbine inlet, and the reductant injector is configured to supply a reductant to the distributor pipe; wherein the method comprises the steps: determining a first quantity of reductant to supply to the first exhaust conduit and a second quantity of reductant to supply to the second exhaust conduit; timing an injection of the first quantity of reductant by the reductant injector in order to coincide with a first predetermined engine crank angle; and timing an injection of the second quantity of reductant by the reductant injector in order to coincide with a second predetermined engine crank angle. 12. The method of claim 11 , wherein the first predetermined crank angle coincides with the second exhaust conduit having a second transient pressure that is higher than a first transient pressure in the first exhaust conduit, and wherein the second predetermined crank angle coincides with the first exhaust conduit having a first transient pressure that is higher than a second transient pressure in the second exhaust conduit; wherein the first and second transient pressures are determined at a position upstream of the first and second turbocharger turbine inlets, respectively. 13. The method according to claim 11 , wherein the first quantity of reductant or the second quantity of reductant is zero. 14. The method according to claim 11 , wherein a final injection of reductant is made at least one half engine crank cycle prior to shutoff of the internal combustion engine. 15. A vehicle, comprising an exhaust system for an internal combustion engine, wherein said exhaust system comprises: a first exhaust conduit leading from a first exhaust bank of the internal combustion engine to a first turbocharger turbine inlet arranged downstream of the first exhaust bank in the direction of travel of a first exhaust stream; a second exhaust conduit leading from a second exhaust bank of the internal combustion engine to a second turbocharger turbine inlet arranged downstream of the second exhaust bank in the direction of travel of a second exhaust stream; an SCR catalyst arranged downstream of the first turbocharger turbine inlet and/or second turbocharger turbine inlet; a reductant supply system comprising a distributor pipe and a reductant injector, wherein the distributor pipe is configured to

Assignees

Inventors

Classifications

  • a heat exchanger · CPC title

  • the substance being ammonia or urea · CPC title

  • specially adapted for catalytic conversion (F01N3/22 takes precedence) · CPC title

  • F02B37/025Primary

    Multiple scrolls or multiple gas passages guiding the gas to the pump drive · CPC title

  • Improving ICE efficiencies · CPC title

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What does patent US11149622B2 cover?
Provided is an exhaust system for an internal combustion engine comprising: a first exhaust conduit leading from a first exhaust bank of the engine to a first turbocharger turbine inlet arranged downstream of the first exhaust bank in the direction of travel of a first exhaust stream; a second exhaust conduit leading from a second exhaust bank of the engine to a second turbocharger turbine inle…
Who is the assignee on this patent?
Scania Cv Ab
What technology area does this patent fall under?
Primary CPC classification F02B37/025. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Oct 19 2021 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 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).