The present technology relates generally to ceiling-mounted fans, and more particularly, to fan blade mounting structures for use with such fans.
High volume, low speed (HVLS) fans are large-diameter (e.g., 20 ft. diameter), ceiling-mounted fans that can be used to provide air flow in industrial and/or commercial buildings, warehouses, loading docks, etc. HVLS fans are typically suspended from the ceiling at heights from about 10 ft. to 35 ft. above the floor, and typically include a plurality of blades extending radially outwardly from a central hub. In operation, HVLS fans rotate at relatively low speeds to produce a large downdraft of air at relatively low speed to enhance the evaporative cooling effect on the skin of personnel within the airflow.
An advantage of HLVS fans is that the costs of installation and operation are often less than those of other types of air conditioning systems, such as forced air systems that provide cooling by changing the temperature of large volumes of air. A challenge, however, with current fan designs is that fan blades can deflect or “cone” at relatively higher speeds of rotation. Coning is the deflection of the set of fan blade out of the horizontal plane due to the lift encountered along the components of the blade. Coning reduces the ability of the fan to direct airflow in a direction perpendicular to the plane of the fan blades. This, in turn, reduces lift and the overall amount of air that flows directly toward the floor. These effects become more pronounced on longer fan blades because they are more flexible than shorter fan blades.
Another challenge with certain HLVS fans is that fan blade sections can have an aerodynamic center that is not aligned with the longitudinal centerline of the fan blade section. As a result, the fan blade section can encounter a differential or twisting load that twists the blade section along the longitudinal centerline. The twist of the fan blade section is more pronounced at the distal end of the blade section and can be positive or negative relative to the air flow. A positive twist can increase angle of attack and thereby increases drag. A negative twist can reduce the angle of attack and thereby reduce lift and the resultant amount of air flow. In addition to twisting loads, the fan blade sections of HLVS fan can produce a torque load that transmits through the blade section to the attachment system.
The following disclosure describes various embodiments of HLVS fans, blade mounting structures, and related methods and systems. Certain details are set forth in the following description and in
Many of the details and features shown in the Figures are merely illustrative of particular embodiments of the technology. Accordingly, other embodiments can have other details and features without departing from the spirit and scope of the present technology. In addition, those of ordinary skill in the art will understand that further embodiments can be practiced without several of the details described below. Furthermore, various embodiments of the technology can include structures other than those illustrated in the Figures and are expressly not limited to the structures shown in the Figures. Moreover, the various elements and features illustrated in the Figures may not be drawn to scale.
In the Figures, identical reference numbers identify identical or at least generally similar elements. To facilitate the discussion of any particular element, the most significant digit or digits of any reference number refer to the Figure in which that element is first introduced. For example, element 107 is first introduced and discussed with reference to
The fan 100 includes a drive unit mount 106 coupled to the hanger 104. The drive unit mount 106 supports a drive unit 107 (e.g., an electric motor, engine, gear assembly or gearbox, etc.) that is operably coupled to a central fan hub 130 (“hub 130”) by a drive shaft (not visible in
The fan blades 140 can be formed from extruded aluminum or aluminum alloy, fabricated metal, or other suitably rigid and lightweight materials (e.g., a carbon fiber material) known in the art. In one embodiment, for example, the fan blades 140 can be made from a T6 temper aluminum alloy, such as 6061 or 6063 aluminum alloys. In the illustrated embodiment, the individual fan blades 140 have an airfoil shape with a fixed angle of attack. In some embodiments, the fan blades 140 can optionally include winglets 142 that enhance air flow at the outboard ends of the fan blades 140. In some embodiments, for example, the fan blades 140 can include winglets described in U.S. patent application Ser. No. 13/302,507, filed Nov. 22, 2011, and titled “Fan Blade Tips,” which is incorporated herein in its entirety by reference. In other embodiments, the fan blades 140 can have a different shape and/or configuration, and/or a non-constant or changeable angle of attack. For example, the fan blades 140 can have a flat profile rather than an airfoil shape. Also, although the fan 100 includes five fan blades in the illustrated embodiment, in other embodiments the fan 100 can include more or fewer fan blades (e.g., ten fan blades).
In operation, the drive unit 107 rotates the fan blades 140 via the hub 130 about a central axis 105 at a rotational speed of, e.g., 10 to 100 rpm. In some embodiments, a user can control the rotational speed and/or the direction of rotation using, for example, a wall-mounted control panel and/or a wireless controller coupled to the drive unit controller (not shown) of the drive unit 107. As the fan blades 140 revolve around the central axis 105, they can produce a moving volume of air, e.g., a column of air (not shown) in a generally downward and/or upward direction, depending on the direction of rotation of the fan blades 140.
In the illustrated embodiment, a retention member or ring 216 is attached to a top side 213a of the hub 130 by a plurality of fasteners 217a (e.g., hex-head bolts) that threadably engage corresponding locking features 217b (e.g., lock nuts;
In general, the components of the hub 130 can be formed from a variety of suitable materials known in the art, including metallic materials, using techniques such as press-forming, machining, casting, etc. For example, in some embodiments the hub plates 332, the central spacer 333, and outer spacers 336 can be made from T6 tempered aluminum alloys; and the retention ring 216 and the retention members 220 can be made from a suitable steel material (e.g., ASTM A36). Although in the illustrated embodiment the hub plates 332 have “star” shapes, in other embodiments the hub plates 332 can have different shapes, such as a round shape, pentagonal shape, etc. Also, in some embodiments the hub 130 can include integrally formed components. For example, in some embodiments the hub 130 can be a single fabricated part or unitary part (e.g. molding, casting, forging or the like), or portions of the hub 130 can be formed from a single material rather than two or more pieces fastened together.
In the illustrated embodiment, the blade mounting structure 150 further includes a third support member or strut 456 that couples the support members 452 to the inboard end portion 143 of the fan blade 140. The strut 456 can include, for example, an elongate shaft (e.g., a tube, beam etc.). A first portion 457a of the strut 456 is sandwiched between the support members 452 and attached thereto by a plurality of fasteners 458b (e.g., Huck fastener pins) that are threadably engaged with radial locking features 458a (e.g., Huck collars). A second portion 457b of the strut 456 (shown in hidden lines) is inserted into a cavity through an opening 445 at the inboard end portion 143. The second portion 457b is secured to the fan blade 140 within the cavity by a plurality of fasteners 459b (e.g., Huck fastener pins) that threadably engage corresponding locking features 459a (e.g., Huck collars). In an alternative embodiment, the second portion 457b of the strut 456 can be attached to an exterior portion of the fan blade 140, rather than being inserted into a cavity of the fan blade 140.
In the illustrated embodiment, each of the support members 452 includes an angled portion 560 (identified individually as first and second angled portions 560a and 560b, respectively) and a non-angled portion 562. The first angled portion 560a extends generally downward from the proximal end portion 453a toward the strut 456. The second angled portion 560b extends generally upward from the proximal end portion 453b toward strut 456. As discussed above, the first portion 457a of the strut 456 is positioned between the support members 452, and the second portion 457b of the strut 456 (shown in hidden lines) extends into the fan blade 140 along the longitudinal axis thereof. In some embodiments, the strut 456 can have a length of from about 4 inches to about 18 inches, such as about 15 inches. In other embodiments, the strut 456 of the fan blade 140 can have other lengths, such as a quarter of the length of the fan blade 140, half the length of the fan blade, the entire length of the fan blade, etc.
Referring next to
In the illustrated embodiment, each of the support members 452 includes a cut-out or opening 564 generally medially disposed in the angled portions 560. The opening 564 can reduce the overall weight of the blade mounting structure 150, and can be configured to augment the vertical air flow profile of the fan 100. For example, without wishing to be bound by theory, it is believed that certain shapes and/or sizes of the openings 564 can promote uptake of air toward the center of the fan 100, i.e., when the fan blades 140 are producing a generally downward draft of air away from the center of the fan 100.
The support members 452 and the strut 456 can be formed, for example, from various suitable materials and methods, such as metals, e.g., sheet metal or metal castings, plastic molds or the like. For example, in some embodiments, the support members 452 can be laser-cut from sheet metal, such as high-strength, low-alloy steel (e.g., ASTM A572), and the strut 456 can be formed from aluminum alloy, such as T6 tempered aluminum alloy. In the illustrated embodiment, the support members 452 are identical or at least have generally the same shape and are symmetric with one another in the vertical direction about the longitudinal axis of the fan blade 140. In other embodiments, however, the support members 452 can have different shapes and/or be asymmetric. For example, in some embodiments the flanges 334 of the hub 130 can carry the support members 452 such that they are asymmetric about the longitudinal axis of the blade mounting structure 150.
In the illustrated embodiment, the strut 456 has a contoured surface 571 that at least partially conforms to the shape and profile (e.g., curvature) of the leading edge cavity 549a to facility a snug or close fit between the strut 456 and the fan blade 140. The strut 456 can be hollow or partially hollow and include a stiffening web 573 extending along the longitudinal axis thereof. In other embodiments, the strut 456 can have other shapes and/or profiles. For example, the strut 456 can have an outer edge that does not conform or does not substantially conform to the leading edge cavity 549a.
Fan blades in conventional HVLS fans abut against the hub and attach to the hub with a small hub connector, such as a metal stub attached to or integrated with the hub. One shortcoming of such designs is that the long fan blades can apply relatively large loads, such as torsional loads to the hub connector, which can lead to premature wear or to damage of the hub connector. In addition, as discussed above, fan blades can apply a substantial twisting force along their longitudinal axis during operation, which can add further stress to conventional hub connectors. Further, a singular hub connector can be vulnerable to single point failure mechanisms due to the concentration of stress and other loads at this singular connection. Blade mounting structures configured in accordance with various embodiments of the present technology, such as the blade mounting structure 150, can address these and other limitations of conventional hub connectors by providing a relatively strong and stiff connection between the fan blades and the hub to reduce or eliminate the effects of coning, twisting, torsional, and/or other forces. For example, the blade mounting structures can reduce or alleviate stress at the junctions with the fasteners that attach the blade mounting structure 150 to the hub 130 and the inboard end portion 143 of the fan blade 140.
In the illustrated embodiment, the spacer insert 665 can have a longitudinal length S (
In the illustrated embodiment, a retention member or ring 1083 includes a mounting portion 1085 coupled to an underside of the mounting plate 210 via a plurality of fasteners 1090a (e.g., hex-head bolts) that threadably engage corresponding locking features 1090b (e.g., locking nuts) positioned on the opposite side of the mounting plate 210. The retention ring 1083 also includes an outward flange or outer lip 1084 that extends at least partially around the second opening 214.
From the foregoing, it will be appreciated that specific embodiments of the present technology have been described herein for purposes of illustration, but that various modifications may be made without deviating from the spirit and scope of the various embodiments of the present technology. For example, in one embodiment a remotely positioned drive unit or engine can rotate the drive shaft 208 (
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