ROTATING SCREEN FOR CENTRIFUGAL FAN

• US 20140053793A1
• Filed: 08/23/2012
• Published: 02/27/2014
• Est. Priority Date: 08/23/2012
• Status: Active Grant

• Current Assignee: Briggs & Stratton LLC (Briggs & Stratton Corporation)
• Original Assignee: Briggs & Stratton Corporation
• Inventors: Johnson, Gary S., Sullivan, Ryan
• Granted Patent: US 8,746,186 B2
• Time in Patent Office: Days
• US Class Current: 123/41.65
• CPC Class Codes: F01P 11/12 Filtering, cooling, or silencing cooling-air
• CPC Class Codes: F04D 17/025 comprising axial flow and radial flow stages
• CPC Class Codes: F04D 17/16 for displacing without appreciable compression
• CPC Class Codes: F04D 29/703 specially for fans, e.g. fan guards

Abstract

A rotating screen, for use with a centrifugal fan of an engine, includes a hub having a rotational axis and a plurality of blades extending radially outwardly from the hub. Each of the blades includes a root adjacent the hub, a tip, a leading edge extending between the root and the tip, and a trailing edge extending between the root and the tip. The blades also include an airfoil shape. The rotating screen also includes a band concentric with the hub and interconnecting the tips of the respective blades.

Claims

1. A rotating screen for use with a centrifugal fan of an engine, the rotating screen comprising:

a hub including a rotational axis;

a plurality of blades extending radially outwardly from the hub, each of the blades including a root adjacent the hub, a tip, a leading edge extending between the root and the tip, and a trailing edge extending between the root and the tip, the blades also including an airfoil shape; and

a band concentric with the hub and interconnecting the tips of the respective blades, wherein the leading edge is the thinnest cross-section portion of each of the plurality of blades.

2. The rotating screen of claim 1, wherein at least the leading edge of each of the blades is sharp.

3. The rotating screen of claim 1, wherein the airfoil shape of the blades is configured to induce an airflow in a direction substantially parallel to the rotational axis in response to rotation of the screen about the rotational axis.

4. The rotating screen of claim 3, wherein the blades each include a suction surface and a pressure surface opposite the suction surface, the suction surface and the pressure surface together defining the airfoil shape of the blades.

5. The rotating screen of claim 4, wherein at least one of the suction surface and the pressure surface has an arcuate shape.

6. The rotating screen of claim 4, wherein the blades each define a blade span extending between the root and the tip, and wherein the blades each define a rake that varies along the blade span.

7. The rotating screen of claim 6, wherein the blades each define a pitch angle that is between about 25 degrees and about 45 degrees along the entire blade span.

8. The rotating screen of claim 1, wherein at least one of the plurality of blades includes a boss integrally formed with the blade.

9. The rotating screen of claim 8, wherein the boss is formed on the trailing edge of the blade.

10. The rotating screen of claim 1, wherein the plurality of blades includes between 4 blades and 16 blades.

11. An engine comprising:

a crankcase;

a cover at least partially enclosing the crankcase;

a centrifugal fan that is rotatable while the engine is in use for discharging a cooling airflow between the crankcase and the cover;

a screen coupled for co-rotation with the centrifugal fan, the screen including a hub including a rotational axis,

a plurality of blades extending radially outwardly from the hub, each of the blades including a root adjacent the hub, a tip, a sharpened leading edge extending between the root and the tip, and a trailing edge extending between the root and the tip, the blades also including an airfoil shape, and

a band concentric with the hub and interconnecting the tips of the respective blades.

12. The engine of claim 11, wherein at least the leading edge of each of the blades is sharp.

13. The engine of claim 11, wherein the airfoil shape of the blades is configured to induce an airflow toward the centrifugal fan in response to rotation of the screen about the rotational axis.

14. The engine of claim 13, wherein the blades each include a suction surface and a pressure surface opposite the suction surface, the suction surface and the pressure surface together defining the airfoil shape of the blades.

15. The engine of claim 14, wherein at least one of the suction surface and the pressure surface has an arcuate shape.

16. The engine of claim 14, wherein the blades each define a blade span extending between the root and the tip, and wherein the blades each define a rake that varies along the blade span.

17. The engine of claim 16, wherein the blades each define a pitch angle that is between about 25 degrees and about 45 degrees along at least a portion of the blade span.

18. The engine of claim 11, wherein at least one of the blades includes a boss integrally formed as a single piece with the blade.

19. The engine of claim 18, wherein the boss is formed on the trailing edge of the blade.

20. The engine of claim 18, wherein the boss on the screen is a first boss, wherein the centrifugal fan includes a plurality of fan blades configured to discharge the cooling airflow in a radially outward direction, and wherein the centrifugal fan further includes a second boss.

21. The engine of claim 20, wherein the second boss is engaged with the first boss to orient the screen relative to the centrifugal fan.

22. The engine of claim 11, wherein the plurality of blades includes between 4 blades and 16 blades.

23. The engine of claim 11, further comprising a stationary screen coupled to the cover and at least partially overlying the screen coupled for co-rotation with the centrifugal fan.

24. The engine of claim 11, wherein the cover includes an annular channel, and wherein the band is at least partially positioned within the channel.

25. The engine of claim 24, wherein the cover includes an inlet aperture in which the screen is at least partially positioned, and wherein the annular channel surrounds the inlet aperture.

26. The engine of claim 25, wherein the cover includes a flange surrounding the annular channel, and wherein the engine further includes a stationary screen fastened to the flange.