Reductant nozzle with helical channel design

US11534728B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11534728-B2
Application numberUS-201816192671-A
CountryUS
Kind codeB2
Filing dateNov 15, 2018
Priority dateNov 15, 2018
Publication dateDec 27, 2022
Grant dateDec 27, 2022

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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 nozzle including a first end and a second end. The first end includes at least a first inlet and a second inlet and the second end includes a plurality of outlets. An exterior surface extends from the first end to the second end of the nozzle. A plurality of vanes are disposed on the exterior surface and extend from the first end to the second end of the nozzle. A plurality of channels form along the exterior surface of the nozzle.

First claim

Opening claim text (preview).

What is claimed is: 1. A nozzle, comprising: a nozzle body including: a first end having a first inlet and a second inlet, the first inlet being fluidly connected to a first channel and the second inlet being fluidly connected to a second channel, the first and second channels being fluidly connected at a location spaced from the first end; a second end having a plurality of outlets, the second end being disposed opposite the first end along a longitudinal direction; a central longitudinal axis extending from the first end to the second end along the longitudinal direction; and an exterior surface extending from the first end of the nozzle body to the second end of the nozzle body, and extending about the central longitudinal axis; a housing disposed about the nozzle body and the central longitudinal axis, the housing including: a first end; a second end disposed opposite the first end of the housing along the longitudinal direction, the second end of the housing being disposed abutting the second end of the nozzle body, exposing a protruding spherical sector of the nozzle body; an interior surface extending from the first end of the housing to the second end of the housing, the interior surface of the housing facing the exterior surface of the nozzle body along a radial direction, the radial direction being perpendicular to the longitudinal direction; and an exterior surface facing away from the exterior surface of the nozzle body along the radial direction; a plurality of vanes disposed between the exterior surface of the nozzle body and the interior surface of the housing; and a plurality of channels disposed between the exterior surface of the nozzle body and the interior surface of the housing, wherein individual channels of the plurality of channels are defined at least in part by: pairs of adjacent vanes of the plurality of vanes; the exterior surface of the nozzle body; and the interior surface of the housing, wherein the first end of the housing and the exterior surface of the nozzle body define a radial gap therebetween along the radial direction, the radial gap being located at the first end of the housing along the longitudinal direction, the interior surface of the housing being in fluid communication with the exterior surface of the housing via the radial gap, wherein the first end of the housing is disposed between the first inlet and the second end of the nozzle body along the longitudinal direction, and the first end of the housing is disposed between the second inlet and the second end of the nozzle body along the longitudinal direction, wherein the plurality of vanes extends from an inlet end to an outlet end along the longitudinal direction, and the plurality of outlets is disposed between the inlet end of the plurality of vanes and the outlet end of the plurality of vanes along the longitudinal direction, and wherein each vane of the plurality of vanes converges into contact with adjacent vanes of the plurality of vanes at the central longitudinal axis along the radial direction and at the outlet end of the plurality of vanes along the longitudinal direction. 2. The nozzle of claim 1 , wherein each vane of the plurality of vanes is helical about the central longitudinal axis of the nozzle. 3. The nozzle of claim 1 , wherein: each vane of the plurality of vanes has a radially outermost surface; at the first end of the nozzle body, the radially outermost surface of each vane is spaced from the exterior surface of the nozzle body by a first distance; and at the second end of the nozzle body, the radially outermost surface of each vane is spaced from the exterior surface of the nozzle body by a second distance that is less than the first distance. 4. The nozzle of claim 1 , wherein individual outlets of the plurality of outlets are disposed between adjacent sidewalls of individual vanes of the plurality of vanes. 5. The nozzle of claim 1 , wherein: the second end of the housing defines an opening; and at least a portion of the second end of the nozzle body extends beyond the opening. 6. The nozzle of claim 4 , wherein the second end of the housing is disposed between the inlet end of the plurality of vanes and the outlet end of the plurality of vanes along the longitudinal direction. 7. The nozzle of claim 1 , wherein: at the first end of the nozzle body, individual channels of the plurality of channels define a first cross-sectional area; and at the second end of the nozzle body, the individual channels define a second cross-sectional area that is less than the first cross-sectional area. 8. The nozzle of claim 1 , wherein: each vane has a first end and a second end spaced from the first end along the longitudinal direction; at the first end of each vane, the pairs of adjacent vanes of the plurality of vanes are separated by a first distance; and at the second end of each vane, the pairs of adjacent vanes are separated by a second distance that is less than the first distance. 9. An exhaust system, comprising: an exhaust pipe configured to receive exhaust from an engine; a nozzle located within the exhaust pipe, the nozzle comprising: a nozzle body including: a first end having a first inlet and a second inlet, the first inlet being fluidly connected to a first channel and the second inlet being fluidly connected to a second channel, the first and second channels being fluidly connected at a location spaced from the first end; a second end having a plurality of outlets, the second end being disposed opposite the first end along a longitudinal direction; a central longitudinal axis extending from the first end to the second end along the longitudinal direction; and an exterior surface extending from the first end of the nozzle body to the second end of the nozzle body, and extending about the central longitudinal axis; a housing disposed about the nozzle body and the central longitudinal axis, the housing including: a first end; a second end disposed opposite the first end of the housing along the longitudinal direction, the second end of the housing being disposed abutting the second end of the nozzle body, exposing a protruding spherical sector of the nozzle body; an interior surface extending from the first end of the housing to the second end of the housing, the interior surface of the housing facing the exterior surface of the nozzle body along a radial direction, the radial direction being perpendicular to the longitudinal direction; and an exterior surface facing away from the exterior surface of the nozzle body along the radial direction; a plurality of vanes disposed between the exterior surface of the nozzle body and the interior surface of the housing; and a plurality of channels disposed between the exterior surface of the nozzle body and the interior surface of the housing, wherein individual channels of the plurality of channels are defined at least in part by: pairs of adjacent vanes of the plurality of vanes; the exterior surface of the nozzle body; and the interior surface of the housing, wherein the first end of the housing and the exterior surface of the nozzle body define a radial gap therebetween along the radial direction, the radial gap being located at the first end of the housing along the longitudinal direction, the interior surface of the housing being in fluid communication with the exterior surface of the housing via the radial gap, wherein the first end of the housing is disposed between the first inlet and the second end of the nozzle body along the longitudinal direction, and the first end of the housing is disposed between the second inlet and the second end of the nozzle body along the longitudinal direction, wherein

Assignees

Inventors

Classifications

  • F01N3/2066Primary

    Selective catalytic reduction [SCR] · CPC title

  • Sprayers or atomisers; Arrangement thereof in the exhaust apparatus · CPC title

  • a flow director or deflector · CPC title

  • the substance being ammonia or urea · CPC title

  • Liquid reactants · CPC title

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What does patent US11534728B2 cover?
A nozzle including a first end and a second end. The first end includes at least a first inlet and a second inlet and the second end includes a plurality of outlets. An exterior surface extends from the first end to the second end of the nozzle. A plurality of vanes are disposed on the exterior surface and extend from the first end to the second end of the nozzle. A plurality of channels form a…
Who is the assignee on this patent?
Caterpillar Inc
What technology area does this patent fall under?
Primary CPC classification F01N3/2066. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Dec 27 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 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).