LOW SOUND TUBEAXIAL FAN

Abstract

A tubeaxial fan housing has a planar support vane that is fixed at sides thereof to opposing interior sides of the tubular housing, toward an inlet of the housing. The support vane receives a shaft on an underside thereof, upon which a propeller is mounted near an outlet end of the housing. The support vane has a curved edge facing the propeller to change a pattern of eddies generated downstream of the support plate and thereby reduce the noise generated by the fan. The curve is an S-shape and may be a sine wave whose period is ⅕ the propeller diameter. The propeller is positioned a relatively large distance from the curved edge of the support vane to reduce further the generation of eddies. That is, the closest point of the curved edge to the propeller is one chord length, which chord is at a tip of a propeller blade. A rounded inlet bell on the housing includes a rounded surface to reduce further turbulence across the propeller and support vane to further reduce sound. The propeller has only five blades to further reduce the generation of eddies.

Claims

1. A fan, comprising: a housing having an inlet and an outlet; a planar support vane connected to an interior of the housing; a shaft supported by the support vane; and a propeller attached to the shaft and being positioned near the outlet of the housing, wherein the support vane includes at least one curved surface facing the propeller.

2. The fan as recited in claim 1, wherein a shortest distance from the propeller to the at least one curved surface is one chord length at an outer tip of a blade of the propeller.

3. The fan as recited in claim 2, wherein the shortest distance is about 8 inches.

4. The fan as recited in claim 1, wherein the support vane includes a straight edge closest to the propeller and two straight side portions extending perpendicularly from the straight edge away from the propeller, and wherein the at least one curved surface is a first curved surface extending from one of the two straight side portions and is a second curved surface extending from the other of the two side portions.

5. The fan as recited in claim 4, wherein each of the first and second curved surfaces is “S” shaped.

6. The fan as recited in claim 1, wherein the at least one curved surface is a sine wave and a period of the sine wave is ⅕.sup.th of a diameter of the propeller.

7. The fan as recited in claim 1, wherein the support vane includes first and second sides that are connected to opposing interior sides of the housing at about a midpoint between the inlet and the outlet of the housing.

8. The fan as recited in claim 1, wherein the propeller has only five blades.

9. The fan as recited in claim 1, further comprising an inlet bell attached to the inlet of the housing, wherein the inlet bell has a curved surface that narrows in a direction toward the inlet of the housing.

10. A tubeaxial fan, comprising: a cylindrical housing having a first length along a longitudinal axis, an inlet, an outlet and opposing first and second interior sides; a planar support vane having first and second sides connected to the interior first and second sides of the housing, respectively; a propeller shaft connected to the support vane; and a propeller attached to the shaft near the outlet of the housing, wherein the support vane includes first and second lateral curved edges facing the propeller.

11. The fan as recited in claim 10, wherein a shortest distance from the propeller to either of the curved edges is one chord length of a blade of the propeller.

12. The fan as recited in claim 10, wherein each of the curved edges is an “S” shape.

13. The fan as recited in claim 12, wherein the “S” shape is defined by a sine wave and a period of the sine wave is ⅕.sup.th of a diameter of the propeller.

14. The fan as recited in claim 10, wherein the sides of the support vane are connected to the sides of the cylindrical housing about halfway along the first length.

15. The fan as recited in claim 10, wherein the propeller has a hub from which extend only five blades.

16. The fan as recited in claim 10, further comprising an inlet bell attached to the inlet of the housing, wherein the inlet bell has a curved surface that narrows in a direction toward the inlet of the housing.

17. A tubeaxial fan, comprising: a cylindrical housing having a first length along a longitudinal axis, an inlet, an outlet and opposing first and second interior sides; a planar support vane having opposing first and second sides connected to the opposing interior first and second sides of the housing, respectively; a shaft connected to the support vane; and a propeller having a diameter, being attached to the shaft and being positioned near the outlet of the housing, wherein the support vane includes two curved edges facing the propeller, and wherein a shortest distance from the propeller to either curved edge is one chord length of a tip of a blade of the propeller.

18. The fan as recited in claim 17, wherein each of the curved edges is a sine wave and a period of the sine wave is ⅕.sup.th of the propeller's diameter.

19. The fan as recited in claim 17, wherein the sides of the vane are connected to the cylindrical housing about halfway along the first length.

20. The fan as recited in claim 17, wherein a number of blades of the propeller consists of five.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0024] The accompanying drawings, which are incorporated in and constitute a part of the specification, illustrate embodiments of the invention and, together with the description, serve to explain the principles of the invention.

[0025] FIG. 1 is a side, cross-sectional view of a conventional tubeaxial fan;

[0026] FIG. 2 is a top view of the conventional tubeaxial fan shown in FIG. 1 with the top of the housing cut away to show the propeller, support vane and streamlined enclosure;

[0027] FIG. 3 is a perspective view of the conventional tubeaxial fan shown in FIG. 1, using dashed lines to represent components interior to the tubular fan housing;

[0028] FIG. 4 is a plan view of another conventional tubeaxial fan shown and described in U.S. Pat. No. 6,702,548;

[0029] FIG. 5 is a perspective view of the tubeaxial fan of one embodiment of the present invention, using dashed lines to represent components interior to the fan housing;

[0030] FIG. 6 is a view of the fan taken along line A-A of FIG. 7A;

[0031] FIG. 7A is a rear view of the fan shown in FIG. 5;

[0032] FIG. 7B is an enlarged view of a tip of a blade of the propeller shown in FIG. 7A;

[0033] FIG. 8 is a plan view of the support vane of the fan shown in FIG. 5;

[0034] FIG. 9 is a view of the fan taken along line B-B of FIG. 7A;

[0035] FIG. 10 is a plan view of an inlet bell according to an embodiment of the present invention;

[0036] FIG. 11 is a side view of the inlet bell shown in FIG. 10; and

[0037] FIG. 12 is a perspective view of the inlet bell attached to the fan according to the present invention.

DESCRIPTION OF THE EMBODIMENTS

[0038] As shown particularly in FIG. 5-9 herein, a tubeaxial fan 100 according to the present invention includes a housing 110 with a first, open, upstream end 112, and a second, open downstream end 114.

[0039] The housing 110 is preferably made of heavy gauge steel for structural rigidity and long service life. The ends 112 and 114 of the housing 110 should include integral rolled flanges 117, 119 for structural rigidity and to connect to a mounting surface, for example duct work, without air leakage. The open ends 112 and 114 allow air to be drawn by a propeller (discussed below) to pass through the housing 110 from the upstream end 112 to the downstream end 114.

[0040] Preferably the housing 110 is cylindrically shaped. However, as would be understood by one of ordinary skill, the housing 110 can be shapes other than cylindrical and still take advantage of the benefits of the invention described herein.

[0041] A motor mount 120 located on a top exterior portion 115 of the housing 110 supports a motor 122 (see FIG. 12). Both the motor 122 and the motor mount 120 are located outside of the housing 110, and outside of an airstream “Y′” generated by the propeller described below.

[0042] A planar support plate or vane 130 is fixed at first and second sides 132 and 134 thereof to opposing interior sides 111 and 113, respectively, of the housing 110. In contrast to the location of the conventional support vane 60 discussed above, the support vane 130 of the present invention is fixed more toward the first upstream end 112 of the housing 110. That is, preferably, the sides 132, 134 of the vane 130 are attached more toward the end 112 of the housing 110, than the middle, but still preferably spaced from the inlet 112.

[0043] As with the conventional fan 10 described above, the support vane 130 of the present invention receives a shaft 140 and a bearing assembly 150 on an underside 136 thereof. The shaft 140 receives at a first end 142 a propeller 160 which is located at the second, downstream end 114 of the housing 110.

[0044] A belt enclosure 170 extends from a top interior portion 118 of the tubular housing 110 to an upper side 138 of the support vane 130. A belt 124 (FIG. 12) extends from the motor 122, through the enclosure 170, and to the shaft 140 to turn the propeller 160. The belt enclosure 170, as with the prior art, is preferably streamlined to facilitate movement of air in the housing 110.

[0045] In addition to the motor 122 and the motor mount 120, the belt 124, shaft 140, and bearing assembly 150 for the shaft 140 are located outside of the airstream “Y” which moves along a central longitudinal axis “X′” from the first, upstream end 112 of the tubular housing 110, through the tubular housing 110 (including the streamlined enclosure 170), past the propeller 160, which draws the air into the upstream end 112 of the fan 100, and out the second, downstream end 114.

[0046] The present inventor has found that re-configuring the edge of the support vane 130 across which the airstream “Y” moves downstream, reduces eddies, as described below particularly with regard to FIG. 8.

[0047] For ease of comparison, FIG. 8 includes, in broken lines, the conventional edge 66 of the support vane 60 described above, in addition to the curved edge (solid lines) 180 of the support vane 130 according to the present invention. The edge 180 of the support vane 130 that faces the propeller 160 includes at least one curve (solid lines) 186.

[0048] More particularly, the support vane 130 includes a first downstream, substantially rectangular portion 144 that has a straight edge 146 that extends the substantial width of a circular hub 164 of the propeller 160 and faces a rear 166 of the hub 164. This edge 146 is located about the same distance from the propeller as the conventional edge 66 shown, e.g., in FIG. 2.

[0049] Extending from the straight edge 146 are perpendicular sides 148 extending to the curved edge 180 of the support vane 130. In the preferred embodiment, the curved edge 180 includes two curved, separated edges 186, referred to herein as “S” or wave shapes.

[0050] The shape of the “S” or wave is sinusoidal and the period of the sine wave is set at a length of about ⅕ of the fan's propeller diameter. An exemplary propeller 160 diameter is 34 inches, so the length is about 6.8 inches. Other usual diameters are 18″, 24″, 30″, 42″, etc.

[0051] The “S-shaped” support vane 130 reduces the fan's 100 sound by changing the pattern of eddies generated downstream from the support vane 130.

[0052] From the curved edges 186 extend sides 198 of the support vane 130 that are straight and perpendicular to the straight edge 146 of the first, rectangular portion 144. These straight sides 198 are fixed to the interior sides 111, 113, respectively, of the cylindrical housing 110 by, e.g., welding. Further, straight edges 200 extend perpendicularly inward from the sides 198.

[0053] In between the straight edges 200, about midway thereof, there is a rectangular extension 202. The extension 202 includes an opening 192 near an upstream end 194 of the support vane 130 through which the belt (not shown) passes, as with the conventional tubeaxial fan 10 described above.

[0054] Otherwise, the support vane 130 includes screw holes 196 for connecting the bearing assembly 150 and the enclosure 170.

[0055] As shown particularly in FIGS. 5-7A, the fan 100 includes a propeller 160 with a plurality of blades 162 emanating from the hub 164 mounted on the shaft 140. The hub 164 preferably presents a solid surface between the bases of the blades 162 fixed to the hub 164 so as to prevent the flow of air through the hub 164. Note that the rectangular portions 144 and 202 of the vane 130 are axially aligned with the solid hub 164.

[0056] The propeller 160 is preferably aluminum with die-formed circular arc airfoil blades 162 attached to the hub 164, which is also preferably die-formed.

[0057] As noted above, the conventional tubeaxial fan 10 propeller 80 includes six blades. According to an embodiment of the present invention shown in FIG. 7, the number of blades 162 is 5. This reduced number of blades, coupled at least with the above-described S-shape of the support vane 130, further reduces the generation of eddies off of the support vane 130.

[0058] Compared to the propeller 80 of the conventional tubeaxial fan 10 described above, which is very close to the edge 66 of the support vane 60, the present invention's propeller 160 is spaced a significant amount from the curved edge 180.

[0059] In the embodiment shown particularly in FIGS. 5, 7A and 9, the curved edges 186 of the support vane 130 are moved back an amount which is based upon the propeller. That is, the closest point 188 of the “S-shaped” vane 130 to the propeller 160 is one chord length of a blade 162 of the fan's propeller 160. As shown in FIG. 7B herein, the chord length “CL” is defined as the length of the chord at the tip “T” of a blade 162 of the propeller 160.

[0060] As one example, the propeller 160 is positioned about eight inches, and more specifically 7.76 inches, from the curved edges 186 of the support vane 130. Note again the conventional distance of about 1.13 inches.

[0061] The distancing of the edge 180 of the support vane 130 from the propeller 160 further helps to reduce the generation of eddies.

[0062] According to the present invention, the support vane 130 has a primary function to keep the fan shaft 140 centered in the cylindrical housing 110. Nevertheless, the present inventor has found that the steps of moving the support vane 130 away from the propeller 160 and providing a curved edge on the support vane 130 reduces the sound generated by the fan relative to the sound generated by a conventional tubeaxial fan. Further, the inventor has found that using only one of these steps, i.e., moving the support vane edge away from the propeller or changing the shape of the support vane edge 180, as described herein, still reduces sound relative to the conventional tubeaxial fan.

[0063] As shown in FIGS. 10-12, the invention may include an inlet bell 220 that is attached to the flange 117 at the first, upstream end 112 of the housing 110. For this purpose, a plurality of holes 222 is provided that corresponds to holes 224 formed on the flange 117. Also, the inlet bell 220 may include radially outer holes 226 to connect the inlet bell 220 to an inline duct (not shown).

[0064] The inlet bell 220 is a circular member having a first, outer flange 228 in which the holes 226 are formed. Opposing the first, outer flange 228 is a second, inner flange 230 in which the holes 222 are formed and which is attached to the flange 117 of the tubeaxial fan 100. The outer and inner flanges 228 and 230 are flat and parallel to each other. Between the two flanges 228 and 230, there is a rounded wall 232 which facilitates movement of the air into the first upstream end of the tubeaxial fan 100 and reduces turbulence going across the propeller 160 and the vane 130.

[0065] The embodiment shown in FIG. 12 includes various brackets 234 for mounting the fan 100 to a floor, other equipment, etc.

[0066] The invention described above, with various combinations of the curved-edge support vane 130, the increased distance between the propeller 160 and the support vane 130, the reduced number of blades 162, and the curved inlet bell 210, results in significantly reduced fan noise. This reduced fan noise during operation of the fan results in a safer environment for those working near the fan.

[0067] More particularly, as can be seen from the following table of test results, using the same fan diameter, flow and fan speed for the conventional fan 10 and the fan 100 of the present invention, the fan 100 of the present invention exhibits lower noise as measured by sones. More particularly, the reduction in sones is about 22% using the present invention, when compared with a conventional tubeaxial fan of equal diameter. Thus, the structure of the fan 100 leads to a quieter overall fan, which reduces noise levels for workers that must work in an environment that uses a tubeaxial fan. In addition, the cost or a tubeaxial fan according to the present invention is expected to be comparable to a conventional tubeaxial fan.

TABLE-US-00001 Diameter Flow SP Speed LwA Fan (in.) (cfm) (in. w.g.) (rpm) (dB) Sones Conventional 34 13000 0.375 1003 95.4 40.9 Invention 34 13000 0.375 1004 91.1 31.7

[0068] The foregoing is considered illustrative only of the principles of the invention. Further, since numerous modifications and changes will readily occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation shown and described. For example, while the preferred embodiment described above applies mostly to tubeaxial fans, the principles of the present invention can be applied to other types of propellers and/or propeller housings requiring performance like that of tubeaxial fans, including flow properties, pressure differentials, output efficiencies, vibration and noise levels. Accordingly, all suitable modifications and equivalents may be resorted to that fall within the scope of the invention and the appended claims.