The present teachings relate generally to fluid nozzles or irrigators for pipes, hoses, tubes, or the like. More specifically, the present teachings relate to a nanobubble generating nozzle which mixes a gas with flowing liquid so that the liquid contains nanobubbles.
Nanobubbles are the smallest bubble size known to date. They are at least 100 times, and for example 500 times, smaller than the size of a microbubble. A typical average diameter of a nanobubble is less than 200 nm. At this size scale, much more nanobubbles can fit within the same volume of liquid (e.g., water, aqueous solution, etc.) compared to other bubbles. As a result of their extremely small size, nanobubbles have unique properties associated with neutral buoyancy, strong electric charge, high mass transfer efficiency, long-term stability, and high residence times. These properties enable nanobubbles to provide a superior aeration method for a variety of applications. Nanobubble generation and collapse is also known to create radical oxygen species, which is beneficial for water treatment without the long-lasting harmful side effects of other existing chemical water treatment methods such as chlorination for example.
A bubble nozzle or generator is a device that produces and inserts bubbles into a liquid, and may be configured according to the needs of an end user. In general, the bubble nozzle mixes the liquid with pressurized gas and ejects the liquid with bubbles under reduced pressure. However, conventional nanobubble nozzles or generators are complicated devices having complex structures. For example, some nanobubble generating devices require a high-pressure pump to pressurize the gas, dissolve and reduce the size of the gas bubbles, and/or contain the gas bubbles in the liquid. Other devices further require a rotary vane or blade to produce cavitation. This means that a separate driver or motor is necessary to impart a driving force to the rotary vane, thereby increasing the manufacturing costs and complexity of the device.
Other known nanobubble nozzles or generators utilize porous media direct injection (which involves compressors) or ultrasonic/acoustic cavitation for generating nanobubbles. However, these technologies have drawbacks. WO2011132846 discloses a nozzle which introduces gas into flowing liquid using the porous media direct injection technique. The nozzle includes a body with a passage through which a liquid flows and a nanobubble generating part corresponding to a portion of the passage, wherein a cross-section of the nanobubble generating part becomes small and then large along the flow path so that the nanobubble generating part has an internal pressure lower than an external pressure of the nozzle body. A gas inlet is formed in the nozzle body and connected to the nanobubble generating part so that gas is introduced into the nanobubble generating part due to a difference between the internal pressure and the external pressure. The nozzle of WO2011132846 also includes a dispersing member mounted to the gas inlet to disperse the gas introduced, wherein the dispersing member is formed of a porous material having a diameter smaller than 1 μm. However, porous media direct injection may be limited in the extent of how small bubbles may be generated. There is also unreliability in the way nanobubbles are generated with porous media direct injection. The size of nanobubbles is further influenced by the hydrophilicity of the porous material. The porous material may also become clogged with dust or debris from the air stream, which will change the proportion of air entering the nozzle relative to the water flow, which is an important consideration in how well the nozzle functions.
Thus, there exists a need for an improved nanobubble nozzle or generator that overcomes the above problems in conventional nanobubble nozzles.
The needs set forth herein as well as further and other needs and advantages are addressed by the present embodiments, which illustrate solutions and advantages described below.
It is an object of the present teachings to remedy the above drawbacks and shortcomings associated with known nanobubble generating devices.
In particular, it is an object of the present teachings to provide a nanobubble nozzle that requires less complexity in its structural arrangement.
It is a further object of the present teachings to provide a nanobubble nozzle that does not use porous media direct injection or ultrasonic/acoustic cavitation to generate nanobubbles.
These and other objects of the present teachings are achieved by providing a nozzle that generates nanobubbles in a flowing liquid using venturi cavitation. In particular, the present teachings provide a nanobubble nozzle comprising a body having a proximal end and a distal end; an inlet disposed at the proximal end and configured to receive a liquid; an outlet disposed at the distal end and having an aperture for discharging the liquid with nanobubbles; a forward channel extending through the body from the inlet to the discharge outlet for transmitting the liquid, the forward channel having a venturi throat, wherein a cross-sectional area of the forward channel decreases from the inlet to the venturi throat and increases from the venturi throat to the discharge outlet so that an internal pressure is provided at the venturi throat, the internal pressure being lower than an external pressure outside the body and lower than a vapor pressure of the liquid flowing through the venturi throat which causes the liquid to cavitate; a return channel extending from the discharge outlet to recirculate a portion of the liquid and mix it with a gas to form a two-phase mixture; and an inlet port connecting the return channel to the venturi throat, wherein flow of the liquid through the venturi throat creates a suction that draws the two-phase mixture into the venturi throat; wherein a section of the forward channel between the venturi throat and the outlet forms a diffusing region in which the liquid cavitates to form the nanobubbles. In some embodiments, the gas that is injected and mixed with the portion of the liquid to form the two-phase mixture is ozone O3.
These and other objects of the present teachings are achieved by providing a nozzle system comprising nanobubble nozzle and a gas supply unit in fluid communication with the nanobubble nozzle. The nanobubble nozzle is configured to generate nanobubbles in a flowing liquid using venturi cavitation. The nanobubble nozzle comprises a body having a proximal end and a distal end; an inlet disposed at the proximal end and configured to receive a liquid; an outlet disposed at the distal end and having an aperture for discharging the liquid with nanobubbles; a forward channel extending through the body from the inlet to the discharge outlet for transmitting the liquid, the forward channel having a venturi throat, wherein a cross-sectional area of the forward channel decreases from the inlet to the venturi throat and increases from the venturi throat to the discharge outlet so that an internal pressure is provided at the venturi throat, the internal pressure being lower than an external pressure outside the body and lower than a vapor pressure of the liquid flowing through the venturi throat which causes the liquid to cavitate; a return channel extending from the discharge outlet to recirculate a portion of the liquid and mix it with a gas to form a two-phase mixture; and an inlet port connecting the return channel to the venturi throat, wherein flow of the liquid through the venturi throat creates a suction that draws the two-phase mixture into the venturi throat; wherein a section of the forward channel between the venturi throat and the outlet forms a diffusing region in which the liquid cavitates to form the nanobubbles. The gas supply unit is connected to a gas inlet of the nozzle body, which is configured to feed the gas for forming the two-phase mixture. In some embodiments, the gas supply unit is connected directly to the gas inlet. In other embodiments, a tube, hose, pipe, conduit, channel, or the like, or any combination thereof, may provide the structural connection between the gas inlet of the nozzle body and the gas supply unit. The gas stored and provided by the gas supply unit may be, for example, ozone O3. In other embodiments, the gas supply unit stores and provides oxygen O2. In yet other embodiments, the gas supply unit supplies air, nitrogen, or carbon dioxide.
Other features and aspects of the present teachings will become apparent from the following detailed description, taken in conjunction with the accompanying drawings, which illustrate by way of example the features in accordance with embodiments of the present teachings. The summary is not intended to limit the scope of the present teachings.
The present teachings are described more fully hereinafter with reference to the accompanying drawings, in which the present embodiments are shown. The following description is presented for illustrative purposes only, and the present teachings should not be limited to these embodiments.
The present teachings have been described in language more or less specific as to structural and mechanical features. It is to be understood, however, that the present teachings are not limited to the specific features shown and described, since the device, apparatus, and/or system herein disclosed comprises preferred forms of putting the present teachings into effect.
For purposes of explanation and not limitation, specific details are set forth such as particular structures, architectures, interfaces, techniques, etc. in order to provide a thorough understanding. In other instances, detailed descriptions of well-known devices and/or methods are omitted so as not to obscure the description with unnecessary detail.
Generally, all terms used in the claims are to be interpreted according to their ordinary meaning in the technical field, unless explicitly defined otherwise herein. All references to a/an/the element, apparatus, component, means, step, etc. are to be interpreted openly as referring to at least one instance of the element, apparatus, component, means, step, etc., unless explicitly stated otherwise. The steps of any method disclosed herein do not have to be performed in the exact order disclosed, unless explicitly stated. The use of “first”, “second,” etc. for different features/components of the present disclosure are only intended to distinguish the features/components from other similar features/components and not to impart any order or hierarchy to the features/components.
Referring to
Downstream from the inlet 22 in a distal direction, the cross-sectional area of the forward channel 20 (cross section being perpendicular to a longitudinal axis of the forward channel) reduces towards the venturi throat 24. In a preferred embodiment, the forward channel 20 tapers and decreases gradually in size to the throat 24. The reduction in the cross-sectional area of the forward channel causes the pressure of liquid flow to drop to the extent that the static pressure of the liquid within the throat is less than or equal to 0.3 psia (absolute pressure). More specifically, the liquid vapor pressure at its incoming temperature is around 0.3 psia for water at 20° C. It is noted, however, that the throat may be configured to withstand pressures higher or lower than 0.3 psia. In the area of the throat 24, the nozzle body has a gas inlet 30, which is in fluid communication with the throat of the forward channel. The gas inlet, in some embodiments, is an air inlet which receives air from the atmosphere surrounding the nozzle or other gaseous source. In some embodiments, the gas inlet receives ozone O3, oxygen O2, nitrogen N2, carbon dioxide CO2, or some other gas, from a gas supply unit 120 (
At the downstream end of the venturi throat 24, the forward channel 20 begins to increase in size (i.e., diameter), preferably by a gradual expansion. Cavitation begins in this portion of the forward channel, known as the diffusing region 26. Within the diffusing region, the liquid (e.g., water) cavitates and/or boils, creating vapor bubbles in the liquid. The static pressure of the liquid still has a static pressure of less than or equal to the liquid vapor pressure. The diffusing region is characterized by a high and increasing void faction (air+vapor; ozone+vapor), and the velocity of the liquid flow within the diffusing region is also very high. In some embodiments, the diffusing region 26 may be longer (in the longitudinal direction of the nozzle) than the length of the inlet 22 and the length of the throat 24 individually. The diffusing region, in other embodiments, may be longer than the combination of the inlet and the throat. The extent in which cavitation occurs in the diffusing region, i.e., the length of the diffusing region where cavitation is generated, is dependent on inlet conditions. For example, higher inlet pressures result in a longer diffusing region.
As shown in
Downstream of the cavitation collapse, the nanobubble outlet 28 provides an opening or aperture 34 (
As shown in
Referring to
The nozzle 10 according to the present teachings also comprises a closed-loop feedback 50. This closed-loop feedback includes an exit port 52 positioned at and connected with (i.e., in fluid communication) the nanobubble outlet 28. The exit port 52 is preferably arranged at or substantially near the distal (downstream) end of the nanobubble outlet 28. The exit port 52 should be located downstream of the cavitation collapse 32. The closed-loop feedback 50 also includes a return channel 54 connected to the port 52. In some embodiments, the return channel is substantially parallel with the longitudinal axis of the forward channel 20. However, in other embodiments, the return channel may be arranged in a non-parallel manner, such that it either converges towards or diverges away from the longitudinal axis of the forward channel. The size (diameter) of the return channel 54 may remain constant from one end to an opposing end thereof. The closed-loop feedback 50 further includes an inlet port 56 connecting the return channel 54 to the venturi throat 24 of the forward channel 20. By way of the exit port 52, return channel 54, and the inlet port 56, liquid is recirculated from the venturi outlet back to the throat 24.
The gas inlet 30 (e.g., air inlet) is connected to the return channel 54 and/or the inlet port 56.
As shown in
A throttling valve 60 may be disposed at the exit port 52 to control the flow of liquid that is recirculated through the return channel 54. By adjusting the throttling valve 60, the flow rate and pressure of the recirculating liquid can be changed/regulated.
The liquid supply unit 126 may comprise a liquid source, storage or reservoir 128 for storing the liquid prior to being conveyed to the liquid inlet 22. In some embodiments, the liquid supply unit 126 may include a pump 130 to transmit the liquid (e.g., water) to the liquid inlet 22. The liquid supply unit 126 may be connected directly to the liquid inlet 22, or alternatively, may be connected via a tube, hose, pipe, conduit, channel, or the like 134. In some embodiments, the liquid supply unit 126 may simply be a municipal or city water system.
According to the present teachings, the two-phase liquid-gas mixture can be introduced into the low-pressure venturi throat in any one or more of the following ways: (1) single injection point as shown in
The nozzle body according to the present teachings is designed to be used in various applications, and for example, can be used on municipal water supply lines (i.e., with municipal water pressure ranging between 20-100 psi). Due to the various features and characteristics of the nozzle 10, nanobubble generation is achieved without need of a compressor, pump, or porous medium. A person of ordinary skill in the art will recognize that this to a major advantage of the present invention over conventional nanobubble generators, which require separate equipment.
While the present teachings have been described above in terms of specific embodiments, it is to be understood that they are not limited to those disclosed embodiments. Many modifications and other embodiments will come to mind to those skilled in the art to which this pertains, and which are intended to be and are covered by both this disclosure and the appended claims. For example, in some instances, one or more features disclosed in connection with one embodiment can be used alone or in combination with one or more features of one or more other embodiments. It is intended that the scope of the present teachings should be determined by proper interpretation and construction of any claims and their legal equivalents, as understood by those of skill in the art relying upon the disclosure in this specification and the attached drawings.
Number | Date | Country | |
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63234405 | Aug 2021 | US |