Large Super Low Noise commercial fans which are used in commercial air cooled apparatuses such as cooling towers, air cooled heat exchangers, including large radiator air coolers and air cooled steam condensers, have a diameter greater than four feet and have blades with forward swept concavely curved leading edges. The forward swept concave leading edges reduce the noise generated by such fan blades. A forward swept leading edge is a leading edge that in inclined at an angle in the direction of fan rotation. A typical fan 1 having blades 2 having a curved forward swept leading edge 3 is shown in
In an exemplary embodiment large diameter axial flow fans and commercial air cooled apparatuses incorporating such fans are provided. In an exemplary embodiment, a large diameter axial flow fan is mounted on an air cooled apparatus for generating an axial air flow in the air cooled apparatus for accomplishing the cooling. The fan has a diameter of at least four feet. The fan has plurality of blades. Each blade includes a leading edge opposite a trailing edge. The entire of the leading edge of each of the blades is linear and forward swept, and each blade includes a metallic outer surface. The fan is a Super Low Noise fan. In a further exemplary embodiment, the commercial air cooled apparatus is selected from the group of air cooled apparatuses consisting of air cooled heat exchangers, radiator coolers, air cooled steam condensers, and cooling towers. In one exemplary embodiment, each blade leading edge is forward swept at an angle of 25° as measured from a radius of rotation of the blade. In another exemplary embodiment, the each of the blades is made from sheet metal stressed skin. In a further exemplary embodiment, the sheet metal is aluminum. In yet another exemplary embodiment, the fan has a diameter of at least 9, 10, 11, 12, 13, or 14 feet. In yet a further exemplary embodiment, the fan has at least three blades and in another exemplary embodiment the fan has at least four blades. In a further exemplary embodiment, the fan includes a hub and the blades are resiliently mounted to the hub. In another exemplary embodiment, each blade is filled with foam. In yet another exemplary embodiment, the entire trailing edge of each blade is linear. In yet a further exemplary embodiment, each blade has a length of 42 inches. In another exemplary embodiment each blade has a length of 48 inches. In yet another exemplary embodiment, each blade has an average chord length of 48 inches. In yet a further exemplary embodiment, the fan generates a sound power level in dBA. Such power lever may be determined by the following equation:
PWL=C+30*log10(TS/1000)+10*log10(HP)+Add
Where:
PWL=Fan Sound Power Level in dBA
C=Fan baseline noise level in dBA which is a function of blade design
TS=Fan tip speed in ft/minute which is equal to π*Fan RPM*Fan Diameter
HP=Fan Shaft Horsepower
Add=Additional noise due to entry and installation effects.
In one exemplary embodiment C for the fan is not greater than 45 dBA. In another exemplary embodiment C for the fan is in the range of 43 to 45 dBA. In yet another exemplary embodiment C for the fan is in not greater than 43 dBA.
The present invention provides for axial flow Super Low Noise fans 2 for commercial (e.g., industrial) applications for use in commercial (e.g., industrial) air cooled apparatuses such as air cooled air heat exchangers 4 and cooling towers 6 (
Fan noise of large diameter fans, i.e., fans having a diameter of at least four feet, such as the fans of the present invention used in air cooled heat exchangers and in cooling towers is influenced by many factors. The noise generated by a fan may be predicted from the following equation:
PWL=C+30*log10(TS/1000)+10*log10(HP)+Add
Where:
PWL=Fan Sound Power Level in dBA
C=Fan baseline noise level in dBA which is a function of blade design
TS=Fan tip speed in ft/minute which is equal to π*Fan RPM*Fan Diameter
HP=Fan Shaft Horsepower
Add=Additional noise due to entry and installation effects (e.g., obstructions, and inlet conditions).
From this equation it can be seen that fan tip speed and horsepower are strong drivers for fan noise, so even older generation fans can be quieted to a certain extent by lowering the fan horsepower and or tip speed. However, when comparing the noise level of two operating fans, having the same dimensions and operating with the same criteria and in the same environment, the variable that determines the overall noise (i.e., the PWL) generated by such fans is “C”.
For older, narrow chord blades, “C” is typically 53-55 dB, while conventional Super Low Noise fans having a curved leading edge, such as the one shown in
In an exemplary embodiment, each forward swept blade 10 includes a rib, as for example rib 12 shown in
The resilient mounting, which is known in the art, is such that it eliminates first mode resonant frequencies.
fN=f((RM+RCG)/RCG)1/2
As can be seen from the equation above, the blade resonant frequency is always higher than the blade rotational speed. The blade resonant frequency will only coincide with the rotation frequency if the mount radius RM were equal to zero, which is not the case with the exemplary embodiment fans. The resonant frequency varies along with the rotation speed (i.e. rotation frequency) remaining a fixed percentage away. This allows the exemplary fans to operate with variable speed drives without the rotational frequency ever being equal to the resonant frequency which can lead to early structural failures.
In an exemplary embodiment, 9, 10, 11, 12, or 13 feet diameter fans are provided using the exemplary embodiment blades. With these exemplary fans, four exemplary embodiment blades are incorporated. In other exemplary embodiment, the exemplary fans have three blades. In yet other exemplary embodiments, the fans may have more than four blades. In another exemplary embodiment, 14 feet diameter fans are provided with the exemplary embodiment blades. The 14 feet diameter fans in one exemplary embodiment are provided with four blades. In another exemplary embodiment, they are provided with six blades.
The exemplary embodiment blades having a diameter in the range of 9 to 13 feet incorporate in one embodiment four blades each having a length 17 of 42 inches and an average chord length 19 of 48 inches (
The exemplary blades are formed using sheet metal stressed skin. In an exemplary embodiment, the sheet metal stressed skin is 5052 high grade marine alloy aluminum. Sheet metal stressed skin is used to form the outer surface or skin 39 of each blade, as well as the spars 16, 18 and ribs 12, as for example shown in
The exemplary embodiment fans are lighter and produce less vibration than current Super Low Noise fans of the same diameter operating under the same environment and parameters, e.g. rpm. Consequently, use of the exemplary embodiment fans reduce the stress on and transmitted through the drive mechanism and structure, thus prolonging the operating lives of such mechanisms and structures. Moreover, the exemplary embodiment fans reduce the bending loads provided to the drive mechanism and structure than the conventional Super Low Noise fans. Their installation is also easier than conventional Super Low Noise fans.
While the invention has been described with respect to a limited number of embodiments, those skilled in the art, having benefit of this disclosure, will appreciate that other embodiments can be devised which do not depart from the scope of the invention as disclosed herein. Accordingly, the scope of the invention should include not only the embodiments disclosed but also such combinations of features now known or later discovered, or equivalents within the scope of the concepts disclosed and the full scope of the claims to which applicants are entitled to patent protection.
This application is based upon and claims priority on U.S. Provisional Application Ser. No. 61/321,127 filed on Apr. 5, 2010, the contents of which are fully incorporated herein by reference.
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The International Search Report and the Written Opinion of the International Searching Authority dated Jul. 18, 2011, for International Application No. PCT/US2011/000618, filed Apr. 5, 2011. |
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Number | Date | Country | |
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20110240268 A1 | Oct 2011 | US |
Number | Date | Country | |
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61321127 | Apr 2010 | US |