Reductant nozzle with radial air injection

Patent metadata

Field	Value
Publication number	US-10953373-B2
Application number	US-201816192616-A
Country	US
Kind code	B2
Filing date	Nov 15, 2018
Priority date	Nov 15, 2018
Publication date	Mar 23, 2021
Grant date	Mar 23, 2021

Abstract

A nozzle including a first channel, a second channel annularly disposed around the first channel, and a plurality of third channels fluidly connected to the second channel. The nozzle includes an interior cavity having a first inlet fluidly connected to the first channel and a plurality of second inlets. Individual second inlets of the plurality of second inlets fluidly connect to individual third channels of the plurality of third channels. The interior cavity includes an outlet and an impinging surface located opposite the first inlet.

First claim

What is claimed is:

1. A nozzle, comprising:
a first end including:
a first channel inlet; and
a second channel inlet radially disposed around the first channel inlet;

a second end including a spray channel outlet;
an interior cavity disposed between the first end and the second end, the interior cavity defining a chamber and including:
a first channel outlet;
a plurality of second channel outlets radially disposed around the first channel outlet; and
a spray channel inlet;
a first channel fluidly connected to the first channel inlet and the first channel outlet;
a plurality of second channels, wherein individual second channels fluidly connect between the second channel inlet and respective individual second channel outlets of the plurality of second channel outlets; and
a spray channel fluidly connected to the spray channel inlet and the spray channel outlet, wherein:
a portion of the chamber is disposed between the first channel outlet and the plurality of second channel outlets;
the plurality of second channel outlets face radially inward and the first channel outlet faces toward the second end;
the individual second channels include a proximal end fluidly connected to the second channel inlet and a distal end fluidly connected to the individual second channel outlets;
the proximal end includes a first cross-sectional area; and
the distal end includes a second cross-sectional area, the second cross-sectional area being less than the first cross-sectional area.

2. The nozzle of claim 1 , wherein the plurality of second channels taper from the second channel inlet to the individual second channel outlets.

3. The nozzle of claim 1 , wherein:
the individual second channels include at least a first portion and a second portion;
the first portion is substantially parallel to the first channel;
a second portion is substantially perpendicular to the first channel; and
the second portion is closer in a height direction of the nozzle to a corresponding individual second channel outlet than the first portion is to the corresponding individual second channel outlet.

4. The nozzle of claim 1 , wherein:
the interior cavity includes a top end, a bottom end, and a sidewall extending between the top end and the bottom end;
the nozzle further comprises:
an impinging surface located opposite the first channel inlet; and
one or more legs extending from the bottom end of the interior cavity, adjacent legs of the one or more legs being spaced apart by a gap; and
the individual second channel outlets face a respective gap between the adjacent legs of the one or more legs.

5. A nozzle, comprising:
a first channel;
a second channel annularly disposed around the first channel;
a plurality of third channels fluidly connected to the second channel, the plurality of third channels being radially disposed around the first channel; and
an interior cavity defining a chamber and including:
a first inlet fluidly connected to the first channel;
a plurality of second inlets, wherein individual second inlets of the plurality of second inlets are fluidly connected to respective individual third channels of the plurality of third channels;
an impinging surface located opposite the first inlet; and
an outlet,

wherein the third channels are disposed radially outward of the chamber such that a portion of the chamber is located between the third channels and a longitudinal axis of the nozzle,
wherein the plurality of third channels are non-circular proximal to the second channel; and
wherein the plurality of third channels are substantially circular at the individual second inlets.

6. The nozzle of claim 5 , wherein:
the plurality of third channels each comprise a first portion and a second portion, the first portion being substantially parallel to the first channel and the second portion being substantially perpendicular to the first channel; and
the second portion is closer, in a direction of the longitudinal axis of the nozzle, to a corresponding channel outlet than the first portion is to the corresponding channel outlet.

7. The nozzle of claim 5 , wherein the plurality of second inlets are substantially equally spaced around the first inlet at the interior cavity.

8. The nozzle of claim 5 , wherein:
the individual third channels include a first cross-sectional area proximal to the annular channel; and
the individual second channels include a second cross-sectional area at the individual second inlets, the second cross-sectional area being less than the first cross-sectional area.

9. The nozzle of claim 5 , wherein the individual third channels of the plurality of third channels taper from the second channel to the interior cavity.

10. The nozzle of claim 5 , wherein the plurality of third channels are substantially of a uniform shape and size.

11. The nozzle of claim 5 , further comprising one or more legs extending from the interior cavity and coupled to the impingina surface, and wherein:
a gap is interposed between adjacent legs of the one or more legs; and
the individual second inlets face the gap interposed between adjacent legs of the one or more legs.

12. The nozzle of claim 5 , wherein:
the interior cavity comprises a bottom end including the first inlet;
the plurality of second inlets are disposed at a sidewall of the interior cavity and above the bottom end.

13. 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 first end including a spray outlet;
a second end including a first channel and a second channel radially disposed around the first channel;
an interior cavity disposed between the first end and the second end, the interior cavity including:
a bottom end;
a top end;
a sidewall extending from the bottom end to the top end;
a first outlet disposed at the bottom end, the first outlet being fluidly connected to the first channel; and
a plurality of second outlets disposed at the sidewall, the plurality of second outlets being fluidly connected to the second channel via a plurality of third channels and being radially disposed around the first outlet; and

a supply line fluidly connected to the nozzle, wherein the supply line is configured to supply reductant to the first channel and air to the second channel,
wherein the plurality of second outlets face radially inward and the first outlet faces toward the first end of the nozzle,
wherein the plurality of third channels are disposed radially outward of the chamber such that a portion of the chamber is located between each third channel of the plurality of third channels and a longitudinal axis of the nozzle,
wherein the plurality of third channels are non-circular proximal to the second channel; and
wherein the plurality of third channels are substantially circular at individual second outlets of the plurality of second outlets.

14. The exhaust system of claim 13 , wherein individual second outlets of the plurality of seconds outlets are substantially diametrically opposed from one another.

15. The exhaust system of claim 13 , wherein:
the nozzle includes a longitudinal axis;
the first channel is substantially parallel to the lonaitudinal axis; and
the plurality of second outlets are substantially perpendicular to the longitudinal axis.

16. The exhaust system of claim 13 , wherein the interior cavity further includes a structure extending from the bottom end, the structure comprising an impinging surface located adjacent the first outlet.

Assignees

• Caterpillar Inc

Inventors

• MANDA VENKATA NAGA Satya Ramakrishna
• Martin Kevin L
• Zwart Paul Arthur
• Denis Andrew M

Classifications

• B01F25/45211

  the elements being cylinders or cones which obstruct the whole diameter of the tube, the flow changing from axial in radial and again in axial · CPC title

• B01F25/31331

  Perforated, multi-opening, with a plurality of holes · CPC title

• B01F25/31322

  used simultaneously · CPC title

• B01F25/313

  wherein additional components are introduced in the centre of the conduit · CPC title

• B01F23/2132 Primary

  using nozzles · CPC title