Air filter assemblies and carrier frames having vortex-generating flow guide

Patent metadata

Field	Value
Publication number	US-9504947-B2
Application number	US-201314029904-A
Country	US
Kind code	B2
Filing date	Sep 18, 2013
Priority date	Nov 13, 2012
Publication date	Nov 29, 2016
Grant date	Nov 29, 2016

Abstract

Air filter assemblies and carrier frames have a plurality of vortex-generating flow guides normalizing air flow to a uniform velocity profile downstream thereof. The airflow having the uniform velocity profile travels across a mass airflow sensor.

First claim

What is claimed is:

1. A carrier frame supporting an air filter element having a dirty air inlet and a clean air outlet, the air filter element filtering air flowing therethrough from upstream to downstream, the carrier frame comprising:
an exit side positioned downstream and adjacent the clean air outlet; and
a vortex-generating flow guide mounted on the exit side, the vortex-generating flow guide comprising:
a plurality of spaced-apart cross-ribs; and
a radially staggered array of pairs of tilted trapezoidal tabs mounted on the plurality of spaced-apart cross-ribs, each of the pairs of tilted trapezoidal tabs comprising:
a first upstream edge having a first end and a second end and a second upstream edge having a third end and a fourth end mounted on a cross-rib, the first upstream edge extending along a first length of the cross-rib and the second upstream edge extending along the first length of the cross-rib such that the first end of the first upstream edge is aligned with the third end of the second upstream edge and the second end of the first upstream edge is aligned with the fourth end of the second upstream edge, and
a first downstream edge and a second downstream edge positioned downstream from the cross-rib, the first downstream edge spaced apart from the second downstream edge,

wherein the vortex-generating flow guide promotes rapid mixing of clean air downstream of the air filter element and normalizes a uniform velocity profile downstream thereof such that mass airflow variation is minimized for flow to a mass airflow sensor positioned downstream of the vortex-generating flow guide.

2. The carrier frame according to claim 1 , wherein the first upstream edge and the second upstream edge are longer than the first downstream edge and the second downstream edge; and
wherein the pairs of tilted trapezoidal tabs have opposing elongated side edges that extend from the first upstream edge and the second upstream edge to the first downstream edge and the second downstream edge.

3. The carrier frame according to claim 1 , wherein the pairs of tilted trapezoidal tabs form a V-shape when viewed in cross section.

4. The carrier frame according to claim 1 , wherein the carrier frame is supported in a housing, the air filter element is supported in the housing by the carrier frame, the carrier frame provides a first seal between the carrier frame and the air filter element, and the carrier frame provides a second seal between the carrier frame and the housing, thereby preventing bypass of unfiltered dirty air to the mass airflow sensor in the event of a rupture of or damage to the air filter element.

5. The carrier frame according to claim 1 , wherein the air filter element comprises at least one of a primary filter element and a secondary or safety filter element.

6. The carrier frame according to claim 5 , wherein the air filter element comprises a pleated filter media.

7. The carrier frame according to claim 1 , wherein the pairs of tilted trapezoidal tabs are tilted trapezoidal tabs having the same geometry and are tilted at opposite but equal angles with respect to the axial flow path.

8. The carrier frame according to claim 7 , wherein the radially staggered array of pairs of tilted trapezoidal tabs have the same geometry.

9. The carrier frame according to claim 8 , wherein the radially staggered array of pairs of tilted trapezoidal tabs comprises first and second rows of pairs of trapezoidal tabs, the first row having less pairs of trapezoidal tabs than the second row; and wherein the pairs of trapezoidal tabs in the first row are radially offset with respect to the pairs of trapezoidal tabs in the second row.

10. The carrier frame according to claim 9 , wherein the first row of pairs of tilted trapezoidal tabs have elongated upstream edges and the second row of pairs of tilted trapezoidal tabs have elongated upstream edges; and wherein the upstream edges of the pairs of tilted trapezoidal tabs in the first row are parallel to the upstream edges of the pairs of tilted trapezoidal tabs in the second row.

11. The carrier frame according to claim 1 wherein the air flows through the clean air outlet along a generally axial flow path until the air flows along the vortex-generating flow guide, which redirects the airflow into at least one vortex flow path.

12. The carrier frame according to claim 11 , wherein the pairs of tilted trapezoidal tabs extend at a tilt angle with respect to the axial flow path.

13. The carrier frame according to claim 12 , wherein the pairs of tilted trapezoidal tabs are planar and the first and second upstream edges and first and second downstream edges extend perpendicular to the axial flow path.

14. The carrier frame according to claim 13 , wherein the pairs of tilted trapezoidal tabs are tilted at an angle of 10 to 45 degrees with respect to the axial flow path.

15. The carrier frame according to claim 11 , wherein the vortex-generating flow guide comprises a helical vane.

16. The carrier frame according to claim 15 , wherein the helical vane comprises an elongated upstream edge and an elongated downstream edge, wherein the upstream edge is transversely oriented at a twist angle with respect to the downstream edge.

17. The carrier frame according to claim 16 , wherein the helical vane comprises opposing helical side edges extending between the upstream and downstream edges.

18. The carrier frame according to claim 17 , wherein the helical vane comprises a helical surface between the upstream and downstream edges and between the opposing helical side edges, the helical surface directing the airflow into the vortex flow path.

19. The carrier frame according to claim 18 , wherein the helical vane is one of an array of helical vanes that comprises a first and a second row of helical vanes.

20. The carrier frame according to claim 19 , wherein the first row of helical vanes is radially offset from the second row of helical vanes.

21. The carrier frame according to claim 20 , wherein the helical vanes in the first row have upstream edges that are radially transversely oriented from upstream edges of the helical vanes in the second row.

22. The carrier frame according to claim 19 , comprising a plurality of spaced-apart cross-ribs that support the staggered array of the helical vanes.

Assignees

• Cummins Filtration Ip Inc

Inventors

• Herman Peter K
• Schwartz Scott W

Classifications

• B01D2279/60

  for the intake of internal combustion engines or turbines · CPC title

• B01D46/521

  using folded, pleated material · CPC title

• A47L9/1608

  Cyclonic chamber constructions · CPC title

• B01D46/0049 Primary

  containing fixed gas displacement elements or cores · CPC title

• F02M35/0205

  Details, e.g. sensors or measuring devices · CPC title