The field of the present invention is that of fan assemblies. More particularly, the field of the present invention is that of open blade fan assemblies, particularly useful for automotive engine cooling applications.
Engine cooling fans develop static pressure across the fan such that regions ahead of the fan are at significantly lower pressure than regions behind the fan. Practical operations of fans used in under-hood engine cooling functions dictates minimum clearances between rotating and stationary components to ensure safe, durable functioning throughout the life of the vehicle. The pressure rise developed across the fan drives leakage flow through the gaps occurring between the fan's blade tips or rotating ring, if present, and the stationary surfaces of the shroud.
In open-blade fans, this leakage flow encounters the tip gap along the entire tip region of each blade from leading edge to trailing edge and enters the gap region having a very high tangential velocity component. As the leakage flow progresses through the gap region, the vicious drag of the fan blade tips continues to strengthen this vertical flow until finally it reaches the exit of the gap region now being radially outward from the blades' leading edge tips. This strong vortex continues to propagate forward, and if not constrained will continue flowing upstream of the fan tangentially and radially outward into the shroud region (adjacent a radiator upstream of the fan assembly) until the primary flow movement recaptures it and pulls it back into the fan passage.
When the recirculation flow reenters the fan passage, it possesses a very high tangential component, which is at great odds with the velocity and direction of the primary incoming flow entering the fan passage through the fan's inlet nozzle. As the tangentially-oriented recirculation flow mixes with the mostly axial primary flow, a vortex is formed just in front of the blade's leading edge at the tip.
Since the leading edge was designed for the primary flow velocity condition, the vortex encountered by the blade is misaligned relative to the intended inlet vector. The above noted action causes the tip region to stall and resulting low relative-momentum flow tends to “hang up” in the blade tip region reducing flow-rate and static pressure and increasing drag and thereby causing efficiency losses.
It is desirable to provide a fan assembly wherein the losses from recirculating leakage flow can be reduced.
To make manifest the above noted desire, a revelation of the present invention is brought forth. In a preferred embodiment, the fan assembly of the present invention has a hub with a plurality of projecting fan blades. A recirculating flow element is provided which is generally forward adjacent an outer diameter of the fan blades. A plurality of guide vanes are positioned within the recirculating flow element. The guide vanes have an inlet angle that is nearly tangential with an outer diameter surface of the recirculating flow element. The guide vanes have an outlet angle which is nearly radial along an inner diameter surface of the recirculating flow element.
Further features of the present invention will be revealed by a review of the invention as it is provided in the accompanying drawings and detailed description.
Referring to
The recirculating flow element 18 is typically forward adjacent of a fan blade outer radial diameter leading tip 20. The fan blades 12 have a radial clearance or tip gap 11 between their leading tip 20 and the outer shroud 14. The tip gap 11 will typically be in a range of 6 mm to 10 mm. The recirculating flow element 18 will typically have an axial clearance 13 with the blade 12 in range of 6 mm to 25 mm. Thereby, in most applications, the axial clearance 13 will vary at a ratio of 5.2 to 0.6 of the tip gap 11. As mentioned previously, the recirculating flow element 18 typically has a cross-sectional shape close to that of a semi-circle with a diameter or major dimension which will typically vary from 25 mm to 50 mm. Accordingly, the diameter or major dimension of the recirculating flow element 18 will have a ratio of 8.3 to 2.5 of the tip gap 11. The recirculating flow element 18 as shown in
Positioned within the circulating flow element 18 are a plurality of guide vanes 22. The guide vanes 22 have an inlet angle 24 measured from the tangential surface of the outer diameter of the recirculating flow element of the shroud that is nearly tangential. As shown, the inlet angle 24 is typically 20° or less. The outlet angle 26 of the guide vane 22 is nearly radial and typically is plus or minus 20° from the radial at a position at recirculating flow element inner diameter surface 17. The guide vanes 22 have a curvilinear shape which is typically conic and as shown is a portion of an ellipse. However, other curvilinear shapes such as a parabolas or spirals can also be utilized. It is preferable that the shape of the guide vanes 22 be that of a continuous curve.
The guide vanes 22 have an axial clearance with the leading tip 20 that slightly decreases by an amount 29 from an inner diameter of the guide vane 22 to its outer diameter. Dimension 29 will typically be less than 50% of the diameter or major dimension of the recirculating flow element 18.
The guide vanes 22 are typically fabricated from a polymeric material and can be integrally formed with the recirculating flow element 18 of the shroud. The surfaces 28 and 30 of the guide vanes are typically linearly extruded allowing the injection molded manufacture of the guide vanes 22 in a simple two piece mold without the requirement of complex cams, sliders or other mechanisms. The total guide vane count can be specified to be that of a prime number to reduce undesirable noise or vibration. Again, to reduce noise or vibration, the spacing may be varied between given guide vanes 31, 33 and 35 as shown in an alternative embodiment shown in
The function of the recirculating flow element 18 is to collect the majority of the recirculation flow leaving the pressure side of each blade tip, allowing it to continue tangentially “centrifuging” so that when the combined leakage flow (collected over the entire blade tip region from trailing edge to leading edge) encounters the shroud guide vanes 22 it is configured to enter along the surface of the outer shroud where the inlet angles 24 of the guide vanes 22 are designed to smoothly capture it.
The function of the shroud vane 22 is to smoothly “capture” the leakage flow as it enters the gap region—this is why the vane's leading edge 23 is substantially tangential near the recirculating element 18 outer diameter surface 15—and then to gently turn the flow direction from tangential to radial and axial—hence the substantially radial trailing edge. The above noted action effectively removes the tangential component from the recirculation flow and reintroduces it back into the fan passage in correct alignment with the incoming primary flow stream.
Referring to
To improve the efficiency of the fan assembly of the present invention even further, the present invention is provided with a fan assembly 207 (
Referring to
The description of the invention is merely exemplary in nature and, thus, variations that do not depart from the gist of the invention are intended to be within the scope of the invention. Such variations are not to be regarded as a departure from the spirit and scope of the invention.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/US09/39848 | 4/8/2009 | WO | 00 | 10/5/2010 |
Number | Date | Country | |
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61124206 | Apr 2008 | US |