Ejector type EGR mixer

• US 9,051,900 B2
• Filed: 01/12/2010
• Issued: 06/09/2015
• Est. Priority Date: 01/13/2009
• Status: Active Grant

• Current Assignee: AVL Mobility Technologies Incorporated
• Original Assignee: AVL Powertrain Engineering, Inc.
• Inventors: Teng, Ho, Regner, Gerhard
• Primary Examiner(s): Huynh, Hai
• Assistant Examiner(s): Laguarda, Gonzalo
• Application Number:
  US13/143,561
• Publication Number:
  US 20110265772A1
• Time in Patent Office: 1,974 Days
• Field of Search: 123/568.11, 123/568.18, 123/568.17, 123/568.12, 123/590, 123/592, 606/051, 606/052
• US Class Current: 1/1
• CPC Class Codes: F02B 31/04 by means within the induction channel, e.g. deflectors
• CPC Class Codes: F02M 26/05 High pressure loops, i.e. wherein recirculated exhaust gas is taken out from the exhaust system upstream of the turbine and reintroduced into the intake system downstream of the compressor
• CPC Class Codes: F02M 26/19 Means for improving the mixing of air and recirculated exhaust gases, e.g. venturis or multiple openings to the intake system
• CPC Class Codes: F02M 29/06 generating whirling motion of mixture
• CPC Class Codes: F02M 35/10118 with variable cross-sections of intake ducts along their length; Venturis; Diffusers
• CPC Class Codes: F02M 35/10222 Exhaust gas recirculation [EGR]; Positive crankcase ventilation [PCV]; Additional air admission, lubricant or fuel vapour admission
• CPC Class Codes: F02M 35/10262 Flow guides, obstructions, deflectors or the like for generating a charge motion in the cylinder F02B31/00; for re-atomising condensed fuel or homogenising fuel-air mixture F02M29/00
• CPC Class Codes: F02M 35/112 for engines with cylinders all in one line
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A radial-mixing exhaust gas recirculation mixer is disclosed having an air supply passage having a convergent portion. An exhaust gas recirculation passage within the convergent portion includes a nozzle having a terminal end. A mixing tube is arranged downstream from the air supply passage and at least a portion of the exhaust gas recirculation passage. A mixing element is disposed in the mixing tube. In one example, a divergent portion is arranged downstream adjoining the mixing tube to increase the pressure of the mixture after the mixing tube. In one example, the exhaust gas recirculation mixer is arranged within an engine such that the air supply passage is in fluid communication with an intake manifold. The exhaust gas recirculation passage is in fluid communication with an exhaust manifold to recirculate a portion of exhaust gas to the intake manifold.

Claims

1. An exhaust gas recirculation mixer comprising:

an air supply passage having a convergent portion including a tapered portion terminating at a distal end of the convergent portion;

an exhaust gas recirculation passage within the convergent portion and including a nozzle having a terminal end substantially axially aligned with the distal end of the convergent portion;

a mixing tube downstream from the air supply passage and at least a portion of the exhaust gas recirculation passage, the mixing tube attached to the distal end of the convergent portion; and

a helical mixing element disposed in and extending axially within the mixing tube, the helical mixing element bending at least 90 degrees around a central longitudinal axis of the mixing tube.

2. The exhaust gas recirculation mixer according to claim 1, wherein the nozzle is arranged within the convergent portion, the nozzle tapering toward the mixing tube.

3. The exhaust gas recirculation mixer according to claim 2, wherein the exhaust gas recirculation passage penetrates the air supply passage upstream from the convergent portion.

4. The exhaust gas recirculation mixer according to claim 2, wherein the nozzle and the convergent portion are frustoconical and concentric with one another forming an annulus.

5. The exhaust gas recirculation mixer according to claim 1, wherein the mixing element is disposed downstream from the terminal end.

6. The exhaust gas recirculation mixer according to claim 5, wherein the mixing element is secured to the mixing tube.

7. The exhaust gas recirculation mixer according to claim 1, wherein the mixing tube includes a length and a diameter, the length less than approximately three times the diameter.

8. The exhaust gas recirculation mixer according to claim 7, further comprising a divergent portion adjoining the mixing tube opposite the air supply passage and providing a mixed gas passage.

15. The exhaust gas recirculation mixer according to claim 1, wherein the helical mixing element bends at least 180 degrees around the central longitudinal axis of the mixing tube.

9. An engine comprising:

at least one cylinder;

an intake manifold and an exhaust manifold fluidly connected to the cylinder;

an air supply passage having a convergent portion upstream from the intake manifold;

an exhaust gas recirculation passage within the convergent portion and in fluid communication with the exhaust manifold, the exhaust gas recirculation passage including a nozzle having a terminal end;

a mixing tube disposed downstream from the terminal end; and

a mixing element disposed within the mixing tube, the mixing element including a first helical element having a first leading edge and a second helical element having a second leading edge, the first and second helical elements bending around a central longitudinal axis of the mixing tube, the second helical element being located downstream from the first helical element and adjacent to the first helical element, the second leading edge of the second helical element being rotationally offset from the first leading edge of the first helical element.

10. The engine according to claim 9, wherein the air supply passage includes a compressor, the mixing element fluidly arranged between the compressor and the cylinder.

11. The engine according to claim 10, further comprising a turbine coupled to the compressor, the turbine disposed within a portion of the exhaust.

12. The engine according to claim 9, further comprising a divergent portion adjoining the mixing tube opposite the air supply passage and providing a mixed gas passage.

13. The engine according to claim 9, wherein the second leading edge of the second helical element is rotationally offset from the first leading edge of the first helical element by at least 90 degrees.

14. The engine according to claim 9, wherein the first and second helical elements bend at least 90 degrees around a central longitudinal axis of the mixing tube.