Patent Application
20110229330
This invention relates to an axial flow fan.
In particular, this invention applies to driving an air flow axially through a heat exchanger, preferably in a motor vehicle cooling and heating system.
Fans are known which comprise a central hub to which a plurality of equally spaced blades are connected. The hub is functionally associated with a motor which rotationally drives the fan in such a way as to promote the axial movement of the air flow.
Fans are known where each blade is associated with a respective aerodynamic fin located in the vicinity of the distal end of the blade relative to the hub.
The fin, which is made as single part with the blade, helps increase fan performance in terms of head and/or efficiency compared to fans without these fins.
This invention has for an aim to provide a fan with enhanced performance in terms of head supplied and/or aerodynamic efficiency.
According to the invention, this aim is achieved by an axial flow fan comprising the technical characteristics described in one or more of the appended claims.
The technical characteristics of the invention, with reference to the above aim, are clearly described in the claims below and its advantages are apparent from the detailed description which follows, with reference to the accompanying drawings which illustrate a preferred embodiment of the invention provided merely by way of example without restricting the scope of the inventive concept, and in which:
With reference to the accompanying drawings, the numeral 1 denotes in its entirety an axial flow fan according to this invention.
The fan 1 comprises a central hub 2 and a plurality of blades 3 fixed to the hub 2.
The hub 2 is cup-shaped and can be connected to a motor for rotationally driving the fan 1 about its axis of rotation “A” in order to move the air flow axially.
Each blade 3 extends betwen a first end 3a proximal to the hub 2 and a second end 3b, opposite the first, distal from the hub 2.
In other words, each blade 3 has an inner edge 4 located at the first end 3a, rigidly fixed to the hub 2 and having a concave shape.
Each blade 3 also comprises an outer edge 5 located at the second end 3b of each blade 3 and having a convex shape.
Each blade 3 also has a first lateral edge 6 which at least partly defines a leading edge 7 of each blade 3 and a second lateral edge 8 which defines a trailing edge 9. The first lateral edge 6 and/or the second lateral edge 8 are straight.
Advantageously, the blades 3 are spaced at equal angular intervals. In the embodiment described, the fan 1 comprises seven blades 3 equally spaced at angular intervals θ substantially equal to 51.4° (
In this specification, the spacing angle θ of the blades 3 is the angle measured at the axis of rotation “A” between radii passing through corresponding points of each blade 3. With reference in particular to
The blades 3 are rigidly fixed to the hub 2 in such a way that they are inclined at an angle to a rotation plane “R” of the blades 3 themselves. In other words, the blades 3 are positioned in such a way as to make a keying angle β that is not zero (in
In this specification, “keying angle β” is the angle made by the rotation plane “R” of the fan 1, that is to say, of the blades 3, with a straight line passing through the leading edge 7 and the trailing edge 9 of the aerodynamic profile of a section of the blade 3.
More in detail, each blade 3 has a spiral shape extending from the first end 3a to the second end 3b.
In other words, each blade 3 is shaped by placing side by side aerodynamic profiles of known geometry and rotating each profile with respect to the one before it in such a way that the keying angle β decreases from the first end 3a to the second end 3b of each blade 3.
In the embodiment described, the fan 1 also comprises a circular peripheral band 10 that rigidly connects the second ends 3b of the blades 3.
More specifically, the peripheral band 10 is rigidly fixed to the outer edges 5 of the blades 3.
Advantageously, the peripheral band 10 stiffens the set of blades 3 in such a way as to prevent the variation of the keying angle β of the blade 3 in a zone near the second end 3b. This variation is caused by aerodynamic loads which are higher in the zone near the second ends 3b of the blades 3.
The peripheral band 10 also reduces the vortical effect produced at the second ends 3b of the blades 3. End vortices are aerodynamic effects produced by the difference between the pressure at the back and the pressure at the front of the blades 3. They reduce the aerodynamic efficiency of the blades 3. Advantageously, therefore, the peripheral band 10 contributes to increasing the efficiency of the fan 1.
The fan 1 also comprises a plurality aerodynamic protrusions 11, each connected to a respective blade 3.
More in detail, each protrusion 11 extends from the first lateral edge 6 in the vicinity of the second end 3b of each blade 3. Further, the protrusions 11 are co-planar and lie in a plane “PP” perpendicular to the axis of rotation “A” of the fan 1.
As illustrated, the plane “PP” is parallel to the rotation plane “R”.
Each protrusion 11 is substantially triangular in shape and has a border 12 that connects it to the respective blade 3. In particular, the connecting border 12 is rigidly connected to an end portion 6a of the first lateral edge 6 of the blade 3.
Also, each protrusion 11 has an outer edge 13 that extends along a circular arc whose centre is at the axis of rotation “A”.
More in detail, the outer edge 5 of the blade 3 and the outer edge 13 of the protrusion 11 extend uninterruptedly. Further, a projection of the outer edge 5 of the blade 3 onto the perpendicular plane “PP” and the outer edge 13 of the protrusion 11 lie on the same circular arc whose centre is at the axis of rotation “A” of the fan 1.
In the embodiment described, the outer edge 13 of each protrusion 11 is also rigidly connected to the peripheral band 10.
The oblique side 14 defines at least part of the leading edge 7 of the blade 3.
More in detail, the leading edge 7 is defined by a free portion 6b of the first lateral edge 6 of the blade 3 and the oblique side 14 of the protrusion 11. More specifically, the free portion 6b of the first lateral edge 6 is the portion of the first edge 6 that extends from the inner edge 4 of the blade 3 to a point where the oblique side 14 of the protrusion 11 meets the first lateral edge 6 of the blade 3.
In the embodiment described, the ratio between a length C1 of the circular arc of the outer edge 13 of each protrusion 11 and a length C2 of the circular arc of a projection of the outer edge 5 of the blade 3 on the perpendicular plane “PP” is between 0.35 and 0.55. Preferably, this ratio is between 0.40 e 0.50. In the embodiment described, this ratio is substantially equal to 0.45 (
Further, the ratio between a length L1 of the connecting border 12 of each protrusion 11 and a length L2 of the first lateral edge 6 of each blade 3 is between 0.20 and 0.40. Preferably, this ratio is between 0.25 e 0.35. In the embodiment described, this ratio is substantially equal to 0.29 (
With reference to a projection on the perpendicular plane “PP”, the value of an advance angle α1 of the first lateral edge 6 of the blade 3 is less than 10°. Preferably, this advance angle α1 is between 5° and 9°.
More specifically, the advance angle α1 of the first lateral edge 6 of the blade 3 is defined as the angle made by the first lateral edge 6 with a radius passing through a first point “P1” where the outer edge 5 of the blade 3 meets the first lateral edge 6 of the blade 3.
Further, the value of an advance angle α2 of the second lateral edge 8 of the blade 3 is less than 20°. Preferably, this advance angle α2 is between 13° and 18°.
More specifically, the advance angle α2 of the second lateral edge 8 of the blade 3 is defined as the angle made by the second lateral edge 8 with a radius passing through a second point “P2” where the outer edge 5 of the blade 3 meets the second lateral edge 8 of the blade 3.
Each blade 3 makes an angle δ between the projection of the first lateral edge 6 on the perpendicular plane “PP” and the projection of the second lateral edge 8 on the perpendicular plane “PP”. The angle δ is between 20° and 28°. Preferably, the value of the angle 6 is between 22° and 26°.
It should be stressed that the preferred values of C1/C2, L1/L2, □1, □2 and □ selected from within the above mentioned respective ranges optimize fan performance in terms of air flow and noise compared to fans with straight blades of substantially known type, the general improvement in performance being confirmed by specific tests.
The invention achieves the proposed aim.
Fan 1 performance is appreciably enhanced by the co-planar aerodynamic protrusions 11. This enhanced performance of the fan 1 is achieved in particular in terms of guaranteed head and aerodynamic efficiency.
Another important advantage of the fan 1 according to the invention is its low noise emission.
| Number | Date | Country | Kind |
|---|---|---|---|
| BO2007A000577 | Aug 2007 | IT | national |
This application is the National Phase of International Application PCT/IB2008/002000 filed Jul. 23, 2008 which designated the U.S. and that International Application was published under PCT Article 21(2) in English. This application claims priority to Italian Patent Application No. B02007A000577 filed Aug. 7, 2007, and PCT Application No. PCT/IB2008/002000 filed Jul. 23, 2008, which applications are incorporated by reference herein.
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/IB08/02000 | 7/23/2008 | WO | 00 | 2/2/2010 |
