The subject matter disclosed generally relates to a fan. More specifically, it relates to a bladeless fan for moving air in commercial and industrial applications.
There are various types of fans, which all serve the purpose of pushing air (or gas) to generate a flow of air, either for air circulation in a room or for evacuating warm air, for example.
From a general point of view, these fans consume space and energy, which can become problematic for uses such as computer systems, which require fans to evacuate warm air, or HVAC (heating, ventilation, and air conditioning) systems, which consume a lot of power in a building.
Furthermore, fans producing higher cubic feet per minute (CFM) are always in demand and, more so, fans offering better power consumption ratio (CFM per Watt or CFM/W). Such using high efficiency fans, especially in commercial and industrial applications, result in lowering power consumption and costs.
Moreover, fans are mechanical apparatuses, and as such, comprise mechanical parts which are prompt to occasional failure.
In view of this context, it is possible to propose solutions that are improvements over the existing axial fans which use blades that rotate around an axis to draw air in parallel to that axis and force air out in the same direction.
According to an embodiment, there is provided a bladeless fan comprising: a ring-shaped chamber extending longitudinally and defining a suctioned air passage having a main-flow inlet and a main-flow outlet; a compressed-gas inlet adapted to receive compressed gas and to provide the compressed gas to the ring-shaped chamber; and a proximal row of channels radially distributed about the suctioned air passage wherein the channels provide a fluid connection for the compressed gas from the ring-shaped chamber to the suctioned air passage thereby generating a pressure differential along the suctioned air passage and forcing a flow of gas from the main-flow inlet to the main-flow outlet, further wherein the proximal row of channels is closer to the main-flow inlet than to the main-flow outlet.
According to an aspect, the ring-shaped chamber comprises an inner face having an airfoil profile where a diameter of the suctioned air passage near the main-flow inlet is smaller than a diameter of the suctioned air passage near the main-flow outlet.
According to an aspect, the channels have a downstream angle greater than zero (0) degrees.
According to an aspect, the channels have a swirling angle greater than zero (0) degrees.
According to an aspect, the bladeless fan further comprises a source of compressed gas connected to the compressed-gas inlet.
According to an aspect, the source of compressed gas comprises a gas cylinder.
According to an aspect, the source of compressed gas comprises a compressor.
According to an aspect, the bladeless fan further comprises an additional row of channels, wherein the additional row is located farther from the main-flow inlet than the proximal row of channels.
According to an aspect, the compressed-gas inlet is closer to the proximal row of channels than to the additional row of channels.
According to an aspect, the channels of the additional row have a cross-section area greater than the cross-section area of the channels of the proximal row.
According to an aspect, the channels of the proximal row of channels have a first swirling angle, the channels of the additional row of channels have a second swirling angle, and the first swirling angle is greater than the second swirling angle.
According to an aspect, the proximal row of channels comprises at least three channels distant from each other and where the at least three channels are within a gas inlet plane perpendicular to a longitudinal axis.
According to an aspect, the proximal row of channels is longitudinally distant from the main-flow inlet.
According to an aspect, the compressed-gas inlet is closer to the main-flow inlet than to the main-flow outlet.
According to an aspect, the suctioned air passage has a cylindrical shape.
According to an embodiment, there is provided a bladeless fan assembly for accelerating a flow of gas in a lumen of a heating, ventilation, and air conditioning (HVAC) system, the lumen having an inner face, the bladeless fan assembly comprising: a ring-shaped chamber extending longitudinally and defining a suctioned air passage having a main-flow inlet and a main-flow outlet; a compressed-gas inlet adapted to receive compressed gas and to provide the compressed gas to the ring-shaped chamber; a proximal row of channels radially distributed about the suctioned air passage wherein the channels provide a fluid connection for the compressed gas from the ring-shaped chamber to the suctioned air passage thereby generating a pressure differential along the suctioned air passage and accelerating a first portion of the flow of gas from the main-flow inlet to the main-flow outlet; and at least one bracket adapted to mount the ring-shaped chamber to the inner face of the lumen of the HVAC system, wherein a second portion of the flow of gas travels between the inner face of the HVAC system and the ring-shaped chamber, whereby the first portion and the second portion of the flow of gas mix downstream of the ring-shaped chamber to generate an accelerated flow of gas.
According to an aspect, the at least one bracket has an airfoil shape perpendicular to the second portion of the flow of gas.
According to an aspect, the ring-shaped chamber has an inner wall delimiting the suctioned air passage and an external wall opposite the suctioned air passage, wherein the inner wall and the external wall form a cylindrically shaped airfoil.
According to an aspect, the bladeless fan assembly further comprises a source of compressed gas connected to the compressed-gas inlet, wherein the source of compressed gas is located outside the lumen.
According to an aspect, the bladeless fan assembly further comprises an upstream inlet located within the lumen, the upstream inlet being fed with compressed gas which in turn feeds the ring-shaped chamber.
According to an embodiment, there is provided a bladeless fan comprising: a ring-shaped chamber extending longitudinally and defining a suctioned air passage having a main-flow inlet and a main-flow outlet; a compressed-gas inlet adapted to receive compressed gas and to provide the compressed gas to the ring-shaped chamber; and rows of channels radially distributed about the suctioned air passage wherein the channels provide a fluid connection for the compressed gas from the ring-shaped chamber to the suctioned air passage thereby generating a pressure differential along the suctioned air passage and forcing a flow of gas from the main-flow inlet to the main-flow outlet.
According to an aspect, a proximal row of the rows of channels is closer to the main-flow inlet than to the main-flow outlet.
According to an aspect, the channels within each of the rows of channels are within a respective gas inlet plane perpendicular to the flow of gas.
According to an aspect, the ring-shaped chamber comprises an inner face having an airfoil profile where a diameter of the suctioned air passage near the main-flow inlet is smaller than a diameter of the suctioned air passage near the main-flow outlet.
According to an aspect, the channels have a swirling angle greater than zero (0) degrees.
According to an aspect, the bladeless fan further comprises a source of compressed gas connected to the compressed-gas inlet.
According to an aspect, the source of compressed gas comprises a gas cylinder.
According to an aspect, the source of compressed gas comprises a compressor.
Features and advantages of the subject matter hereof will become more apparent in light of the following detailed description of selected embodiments, as illustrated in the accompanying figures. As will be realized, the subject matter disclosed and claimed is capable of modifications in various respects, all without departing from the scope of the claims. Accordingly, the drawings and the description are to be regarded as illustrative in nature and not as restrictive and the full scope of the subject matter is set forth in the claims.
Further features and advantages of the present disclosure will become apparent from the following detailed description, taken in combination with the appended drawings, in which:
It will be noted that throughout the appended drawings, like features are identified by like reference numerals.
There is described below a bladeless fan for commercial and industrial applications.
Referring to
The bladeless fan 10 has an inner portion defining a inner face 102 which forms the lumen defined by cylinder 200. A directional flow of suctioned air thus travels through the bladeless fan 10 between a main-flow inlet 360 and a main-flow outlet 370, i.e., in the suctioned air passage 100. Preferably, the suctioned air passage 100 has a cylindrical shape.
To generate and accelerate the airflow through the suctioned air passage 100, there is provided a source of compressed air, or, more generally, a source of compressed gas 500.
The bladeless fan 10 is adapted to have compressed gas flowing from the source of compressed gas 500, via a compressed-gas inlet 350, to the suctioned air passage 100 in a manner that will generate a pressure differential along the length of the suctioned air passage 100. This arrangement forces an airflow to travel toward the main-flow outlet 370 of the suctioned air passage 100. The pressure differential is adapted to drive the airflow as a typical axial fan would, however without any mobile mechanical parts therein.
To provide the desired pressure differential along the length, and more particularly the inner face 102 of the suctioned air passage 100, the bladeless fan 10 comprises a cylinder 200, having a longitudinal axis 150, that forms the suctioned air passage 100 (which is the lumen within the cylinder 200). This cylinder 200 has a plurality of perforations, e.g., channels 210, provided along the circumference of the cylinder 200.
Channels 210 are arranged in rows of channels 210. According to different embodiments, there is one or more rows of channels 210 distributed about the suctioned air passage and providing a fluid connection for the compressed gas between the ring-shaped chamber 300 and the suctioned air passage 100.
According to an embodiment, a row of channels 210 (aka a first or proximal row of channels 210) is closer to the main-flow inlet 360 than to the main-flow outlet 370. Still according to an embodiment, the proximal row of channels 210 comprises at least three channels 210 distant from each other and within a gas inlet plane perpendicular to the longitudinal axis 150.
Surrounding the cylinder 200, a ring-shaped chamber 300 acts as an antechamber to the cylinder 200. The ring-shaped chamber 300 is fluidly connected to the suctioned air passage 100 through the channels 210. The ring-shaped chamber 300 is adapted to receive a flow of high-pressure gas, aka compressed gas, and to distribute the compressed gas into the suctioned air passage 100.
This distribution of the flow of compressed gas is made by feeding the compressed gas to the ring-shaped chamber 300 at a bottom portion, i.e., near the main-flow inlet 360, via a compressed-gas inlet 350 located about the bottom portion of the ring-shaped chamber 300. The ring-shaped chamber 300 extends upwardly therefrom.
The ring-shaped chamber 300 acts as an antechamber because the chamber is shaped as a hollow ring surrounding the cylinder 200, with channels 210 providing fluid connection therebetween providing an entrance for the compressed gas into the suctioned air passage 100.
Each one of the channels 210 individually extends substantially radially through the wall 213 forming the cylinder 200. The channels 210 traverse the width of the wall 213 and therefore provide a fluid connection between the ring-shaped chamber 300 and the suctioned air passage 100. Each channel 210 has an input opening 211 connected to the ring-shaped chamber 300, and an output opening 212 connected to the suctioned air passage 100 that is adapted to liberate compressed gas into the suctioned air passage 100.
According to various embodiments, the channels 210 may be of a circular shape, a cylindrical shape, a conical shape, an oval shape, a rectangular shape, or an irregular cross-section.
Similarly, input openings 211 and output openings 212 may take many shapes, which include for example circular, oval, rectangular, irregular or have the shape of a slot. The shape and size of the input openings 211 and output openings 212 of a channel 210 may further be identical or may differ from each other.
The pressure of the compressed gas feeding two different channels 210 depends on the longitudinal coordinates of the channels 210. As illustrated on
Referring to the orientation depicted on
The continuous feed of the channels 210 with compressed gas further ensures that the gas which makes up the pressure gradient along the inner face 102 of the cylinder 200 is continuously renewed.
According to an embodiment, the size of the channels 210 increases as the longitudinal coordinate of the channels 210 increases. In other words, the channels 210 become bigger as the channels 210 are located farther from the compressed-gas inlet 350. Accordingly, high-speed high-pressure jets exist close to the main-flow inlet 360 and lower-pressure jets of lowers speed, but of similar volumetric output, exist closer to the main-flow outlet 370.
The effect of the presence and continuous renewal of this pressure gradient is to draw air in the direction of decreasing pressure, i.e., upwardly. The upward flow of air along the inner face 102 of the cylinder 200 generated by the pressure gradient draws air upward within the suctioned air passage 100, thereby producing an acceleration of the airflow entering through the main-flow inlet 360.
According to an embodiment, the shape of the inner face 102 along which travels the airflow from the main-flow inlet 360 to the main-flow outlet 370 has an airfoil shape. According to an embodiment, the airfoil shape of the inner face 102 is designed to optimize the effect of the speed and static pressure of the airflow generated by the jets exiting the channels 210. In consequence, the airfoil shape of the inner face 102 optimizes the airflow exiting the apparatus at the main-flow outlet 370 by benefiting from the Coanda effect.
According to an embodiment, the source of compressed gas 500 is a gas cylinder. Using a bottle of pressurized gas is advantageous in some cases because it requires no mobile mechanical part anywhere in the bladeless fan 10, including the source of compressed gas 500. Therefore, it minimizes the risks of mechanical failures. The bladeless fan 10 may even keep working if there is an electrical power outage, therefore ensuring continuous ventilation of an object or of a location, which can be very useful in a context where continuous ventilation and/or heat removal is a critical aspect, for example in a room comprising heat-generating equipment, or in electronics.
According to an embodiment, a splitter splits the flow of compressed gas from a single source, i.e., using a single gas cylinder, to feed simultaneously a plurality of bladeless fan 10 that ventilate a plurality of areas using the same single source of compressed gas 500.
Alternatively, it is possible to use a compressor, or any other device adapted to such purpose, to generate the necessary compressed gas. Such a solution may be provided by using an appropriate enclosed fan to build up pressure. Such pressure is used as an input of the compressed gas-fed through tubing one or more bladeless fans 10.
The bladeless fan 10 may be used for a variety of purposes. For example, it can be used in an HVAC setting for ventilation. It can also be used, notably, in the ceiling or rooftop of rooms or buildings having heat-generating equipment, such as industrial facilities or data centers, thereby forcing airflow in or out of rooms or buildings fluidly connected thereto.
By changing the form factor of the bladeless fan 10, the same type of bladeless fan 10 as described herein may be used in smaller environments. For example, it can be installed in electronics to evacuate heat, therefore forming an active heat sink inside the electronic device having no mechanical parts.
Turning to
Step 1100: providing a source of compressed gas;
Step 1200: providing a chamber extending in a longitudinal direction, the chamber being closed, the chamber comprising a pressurized-gas inlet for receiving compressed gas, a wall defining a cylinder with a plurality of channels providing a fluid connection through the wall, the channels being located across a range of different longitudinal coordinates, and the wall being radially curved on itself to form a lumen therein adapted to receive jets of gas through the channels; and
Step 1300: injecting the compressed gas through the pressurized-gas inlet with an initial pressure which is sufficient to force a gas jet through the plurality of channels, high-pressure jets flowing through those being located close to the pressurized-gas inlet and lower pressure jets flowing through those at the farthest, thereby generating a pressure gradient along the wall in the lumen which generates the directional gas flow in the lumen.
Referring to
Exemplary bladeless fan 20 further features a variable diameter in its longitudinal direction providing a particular airfoil profile to the inner face 102 delimiting the suctioned air passage 100. More particularly, the inner face 102 has an airfoil profile where a diameter of the suctioned air passage 100 near the main-flow inlet 360 is smaller than a diameter of the suctioned air passage near the main-flow outlet 370.
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According to an embodiment, the channels 210 of at least one of the rows 220a-c have a downstream angle.
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According to an embodiment, the bladeless fan 10, and more precisely the external wall 240 of the bladeless fan 10, is mounted using a bracket 230, and preferably at least two brackets 230, and more preferably at least four brackets 230. Preferably, the brackets 230 have an airfoil or rain drop profile shape extending in the direction of the airflow, thereby minimizing their disturbance of the air flowing along the brackets 230.
The brackets 230 are adapted to have the bladeless fan 10 mounted about the inner face 610, with air upstream being able to travel in the cylinder 200 of the bladeless fan 10 and between the exterior of the bladeless fan 10 and the inner face 610.
The bladeless fan 10, as described before, is adapted to accelerate the airflow travelling in the cylinder 200, i.e., generate an accelerated airflow. The result is that the bladeless fan 10 also accelerates the surrounding airflow travelling between the exterior of the bladeless fan 10 and the inner face 610 thereby creating an entrained air flow. Since the accelerated airflow and the surrounding airflow interact, i.e., mix, downstream from the bladeless fan 10, the speed of resulting airflow is increased relative to the speed of the upstream airflow.
Referring to
According to embodiments, one previous solution may be better suited to a situation than the other based on the impact of the addition of new gas in the ducting and considering the characteristics of the new gas (e.g., nature, temperature, relative humidity, etc.).
While the embodiments above were described using terms such as upwardly, downwardly, bottom, top, etc., it should be noted that the apparatus may then be used in other directions such that the upward direction may become a lateral or downward direction, or any other intermediate direction. The apparatus was therefore described as if it was a chimney, as it appears natural to describe it in this direction, but the apparatus may be reoriented otherwise. However, orienting it to have an upward direction of the flow is advantageous as the apparatus may benefit from the ascending flow of warm air, hence accelerating an already existing upward flow of warm air. This orientation may therefore be beneficial for this reason when the apparatus is used to remove warm air from a location.
While preferred embodiments have been described above and illustrated in the accompanying drawings, it will be evident to those skilled in the art that modifications may be made without departing from this disclosure. Such modifications are considered as possible variants comprised in the scope of the disclosure.
This application claims priority from U.S. provisional patent application 63/087,973 filed Oct. 6, 2020, the specification of which is hereby incorporated herein by reference in its entirety.
Filing Document | Filing Date | Country | Kind |
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PCT/CA2021/051406 | 10/6/2021 | WO |
Number | Date | Country | |
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63087973 | Oct 2020 | US |