US20220256926A1

US20220256926A1 - Smoking substitute apparatus

Info

Publication number: US20220256926A1
Application number: US17/686,121
Authority: US
Inventors: Benjamin Illidge; Benjamin ASTBURY; Nikhil Aggarwal
Original assignee: Nerudia Ltd
Current assignee: Nerudia Ltd
Priority date: 2019-09-20
Filing date: 2022-03-03
Publication date: 2022-08-18
Also published as: WO2021053232A1; EP3930517A1; EP3794986A1

Abstract

A smoking substitute apparatus comprising: a housing; an air inlet and an air outlet formed in the housing, wherein the air inlet is in fluid communication with the air outlet through an air flow passage; and a heater located in the air flow passage configured to generate an aerosol from an aerosol precursor. There is also provided a flow modifying device which extends across the air flow passage at a position between the air inlet and the heater. The flow modifying device is configured to incite a laminar property to the air flow to the heater.

Description

CROSS REFERENCE TO RELATED APPLICATIONS

Cross-Reference to Related Applications/Incorporation by Reference Statement

This application is a non-provisional application claiming benefit to the international application no. PCT/EP2020/076309 filed on Sep. 21, 2020, which claims priority to EP 19198624.9 filed on Sep. 20, 2019. The entire contents of each of the above-referenced applications are hereby incorporated herein by reference in their entirety.

FIELD OF THE DISCLOSURE

The present disclosure relates to a smoking substitute apparatus and, in particular, a smoking substitute apparatus that is able to deliver nicotine to a user in an effective manner.

BACKGROUND

The smoking of tobacco is generally considered to expose a smoker to potentially harmful substances. It is thought that a significant amount of the potentially harmful substances is generated through the burning and/or combustion of the tobacco and the constituents of the burnt tobacco in the tobacco smoke itself.
Low temperature combustion of organic material such as tobacco is known to produce tar and other potentially harmful by-products. There have been proposed various smoking substitute systems in which the conventional smoking of tobacco is avoided.
Such smoking substitute systems can form part of nicotine replacement therapies aimed at people who wish to stop smoking and overcome a dependence on nicotine.
Known smoking substitute systems include electronic systems that permit a user to simulate the act of smoking by producing an aerosol (also referred to as a “vapor”) that is drawn into the lungs through the mouth (inhaled) and then exhaled. The inhaled aerosol typically bears nicotine and/or a flavorant without, or with fewer of, the health risks associated with conventional smoking.
In general, smoking substitute systems are intended to provide a substitute for the rituals of smoking, whilst providing the user with a similar, or improved, experience and satisfaction to those experienced with conventional smoking and with combustible tobacco products.
The popularity and use of smoking substitute systems has grown rapidly in the past few years. Although originally marketed as an aid to assist habitual smokers wishing to quit tobacco smoking, consumers are increasingly viewing smoking substitute systems as desirable lifestyle accessories. There are a number of different categories of smoking substitute systems, each utilising a different smoking substitute approach. Some smoking substitute systems are designed to resemble a conventional cigarette and are cylindrical in form with a mouthpiece at one end. Other smoking substitute devices do not generally resemble a cigarette (for example, the smoking substitute device may have a generally box-like form, in whole or in part).
One approach is the so-called “vaping” approach, in which a vaporizable liquid, or an aerosol former, sometimes typically referred to herein as “e-liquid”, is heated by a heating device (sometimes referred to herein as an electronic cigarette or “e-cigarette” device) to produce an aerosol vapor which is inhaled by a user. The e-liquid typically includes a base liquid, nicotine and may include a flavorant. The resulting vapor therefore also typically contains nicotine and/or a flavorant. The base liquid may include propylene glycol and/or vegetable glycerine.
A typical e-cigarette device includes a mouthpiece, a power source (typically a battery), a tank for containing e-liquid and a heating device. In use, electrical energy is supplied from the power source to the heating device, which heats the e-liquid to produce an aerosol (or “vapor”) which is inhaled by a user through the mouthpiece.
E-cigarettes can be configured in a variety of ways. For example, there are “closed system” vaping smoking substitute systems, which typically have a sealed tank and heating element. The tank is pre-filled with e-liquid and is not intended to be refilled by an end user. One subset of closed system vaping smoking substitute systems include a main body which includes the power source, wherein the main body is configured to be physically and electrically couplable to a consumable including the tank and the heating element. In this way, when the tank of a consumable has been emptied of e-liquid, that consumable is removed from the main body and disposed of. The main body can then be reused by connecting it to a new, replacement, consumable. Another subset of closed system vaping smoking substitute systems are completely disposable, and intended for one-use only.
There are also “open system” vaping smoking substitute systems which typically have a tank that is configured to be refilled by a user. In this way the entire device can be used multiple times.
An example vaping smoking substitute system is the myblu™ e-cigarette. The myblu™ e-cigarette is a closed system which includes a main body and a consumable. The main body and consumable are physically and electrically coupled together by pushing the consumable into the main body. The main body includes a rechargeable battery. The consumable includes a mouthpiece and a sealed tank which contains e-liquid. The consumable further includes a heater, which for this device is a heating filament coiled around a portion of a wick. The wick is partially immersed in the e-liquid, and conveys e-liquid from the tank to the heating filament. The system is controlled by a microprocessor on board the main body. The system includes a sensor for detecting when a user is inhaling through the mouthpiece, the microprocessor then activating the device in response. When the system is activated, electrical energy is supplied from the power source to the heating device, which heats e-liquid from the tank to produce a vapor which is inhaled by a user through the mouthpiece.

SUMMARY OF THE DISCLOSURE

For a smoking substitute system, it is desirable to deliver nicotine into the user's lungs, where it can be absorbed into the bloodstream. However, the present disclosure is based in part on a realization that some prior art smoking substitute systems, such delivery of nicotine is not efficient. In some prior art systems, the aerosol droplets have a size distribution that is not suitable for delivering nicotine to the lungs. Aerosol droplets of a large particle size tend to be deposited in the mouth and/or upper respiratory tract. Aerosol particles of a small (e.g., sub-micron) particle size can be inhaled into the lungs but may be exhaled without delivering nicotine to the lungs. As a result, the user would require drawing a longer puff, more puffs, or vaporizing e-liquid with a higher nicotine concentration in order to achieve the desired experience.
Accordingly, there is a need for improvement in the delivery of nicotine to a user in the context of a smoking substitute system.
The present disclosure has been devised in the light of the above considerations.
In a general aspect, the present disclosure relates to modifying air flow through a smoking substitute apparatus to reduce turbulence in the air flow presented to an aerosol generator for generating an aerosol.
According to a first preferred aspect there is provided a smoking substitute apparatus comprising: a housing; an air inlet and an air outlet formed in the housing, wherein the air inlet is in fluid communication with the air outlet through an air flow passage; an aerosol generator located in the air flow passage configured to generate an aerosol from an aerosol precursor; and a flow modifying device extending across the air flow passage at a position between the air inlet and the aerosol generator, wherein the flow modifying device is configured to incite a laminar property to the air flow to the aerosol generator.
In a second aspect, there is provided a method of operating a smoking substitute apparatus according to the first aspect, in which an air flow is drawn through the apparatus from the air inlet to the air outlet by user inhalation, and the aerosol generator operated to generate an aerosol from an aerosol precursor.
The flow modifying device may provide one or more of the following advantages. The flow modifying device may provide a lower pressure drop through the apparatus. This may allow more efficient use of the force exerted on the device for the purpose of drawing vapor, i.e., a less powerful puff. The flow modifying device may provide an increased aerosol particle size. This may increase the efficiency of nicotine deposition in the lungs and subsequent transfer to the blood stream. The flow modifying device may increase the portion of the aerosol generator (e.g., wick and/or heater, in some embodiments) which actively comes into contact with the air flow. This may increase the surface area of vaporization which leads to an increased TPM (total particulate matter). The flow modifying device may provide a reduction in liquid deposition around the internal airflow geometry, e.g., the air flow passage downstream of the wick/heater, by promotion of laminar flow. This may decrease liquid condensation and deposition in the airflow path and may lead to lower/zero build up which reduces leakage into the mouth or leakage of the pod during use or between uses (e.g., when stored in a user's pocket).
Optionally, the flow modifying device comprises a structure with an upstream face, a downstream face and a plurality of apertures through the structure between the upstream face and the downstream face.
Optionally, the plurality of apertures are of uniform size.
Optionally, the plurality of apertures are of non-uniform size.
Optionally, the plurality of apertures are arranged in a pattern and the size of the apertures varies from a center of the pattern towards an edge of the pattern.
Optionally, a largest aperture, or largest apertures, of the pattern are located at the center of the pattern.
Optionally, a largest aperture, or largest apertures, of the pattern are located at the edge of the pattern.
Optionally, the plurality of apertures are arranged in a uniform pattern.
Optionally, the plurality of apertures are arranged in a non-uniform pattern.
Optionally, the plurality of apertures have a size in a range from about 0.2 mm.
Optionally, the plurality of apertures have a size in a range up to about 0.7 mm.
Optionally, the plurality of apertures have a size in a range from about 0.2 mm to about 0.45 mm.
Optionally, the plurality of apertures have a depth in a range from about 0.1 mm to about 10 mm.
The apertures may have a uniform shape in the depth direction, i.e., in the direction from the upstream face to the downstream face. In this case, the apertures may have a substantially cylindrical shape, such as a circular cylindrical shape, hexagonal cylindrical shape, rectangular cylindrical shape, etc. A uniform shape in the depth direction may further promote the uniformity of air flow in the flow modifying device.
Alternatively, the flow modifying device may have apertures with a shape that is not necessarily uniform in the depth direction. This may still provide acceptable performance, but modifying the air flow in effect by dampening it. For example, the structure may be a woven mesh structure of strands with the apertures formed between the strands. Such a configuration is inexpensive to produce.
Optionally, the upstream face and the downstream face of the flow modifying device are substantially planar and orthogonal to the air flow passage.
Optionally, at least the downstream face of the flow modifying device has a curved or domed shape. This can help to maintain a free air flow path through the flow modifying device by encouraging liquid (that may be deposited on the flow modifying device) to move away from a center of the flow modifying device.
Optionally, the flow modifying device comprises a channel at, or adjacent to, a lateral edge of the flow modifying device. The channel may perform a function of collecting liquid. This can maintain a free air flow path through the flow modifying device.
Optionally, the channel extends continuously around a periphery of the flow modifying device.
Optionally, the flow modifying device is formed of an electrically conductive material.
Optionally, the flow modifying device is heatable. In use, the flow modifying device may be heated. This may be done, where the flow modifying device is formed of an electrically conductive material, by electrical resistive heating.
In another aspect, the present disclosure provides a smoking substitute system comprising: a main body; and a smoking substitute apparatus according to the first aspect.
The smoking substitute apparatus may be in the form of a consumable. The consumable may be configured for engagement with a main body. When the consumable is engaged with the main body, the combination of the consumable and the main body may form a smoking substitute system such as a closed smoking substitute system. For example, the consumable may comprise components of the system that are disposable, and the main body may comprise non-disposable or non-consumable components (e.g., power supply, controller, sensor, etc.) that facilitate the generation and/or delivery of aerosol by the consumable. In such an embodiment, the aerosol precursor (e.g., e-liquid) may be replenished by replacing a used consumable with an unused consumable.
Alternatively, the smoking substitute apparatus may be a non-consumable apparatus (e.g., that is in the form of an open smoking substitute system). In such embodiments an aerosol former (e.g., e-liquid) of the system may be replenished by re-filling, e.g., a reservoir of the smoking substitute apparatus, with the aerosol precursor (rather than replacing a consumable component of the apparatus).
In light of this, it should be appreciated that some of the features described herein as being part of the smoking substitute apparatus may alternatively form part of a main body for engagement with the smoking substitute apparatus. This may be the case in particular when the smoking substitute apparatus is in the form of a consumable.
Where the smoking substitute apparatus is in the form of a consumable, the main body and the consumable may be configured to be physically coupled together. For example, the consumable may be at least partially received in a recess of the main body, such that there is an interference fit between the main body and the consumable. Alternatively, the main body and the consumable may be physically coupled together by screwing one onto the other, or through a bayonet fitting, or the like.
Thus, the smoking substitute apparatus may comprise one or more engagement portions for engaging with a main body. In this way, one end of the smoking substitute apparatus may be coupled with the main body, whilst an opposing end of the smoking substitute apparatus may define a mouthpiece of the smoking substitute system.
The smoking substitute apparatus may comprise a reservoir configured to store an aerosol precursor, such as an e-liquid. The e-liquid may, for example, comprise a base liquid. The e-liquid may further comprise nicotine. The base liquid may include propylene glycol and/or vegetable glycerin. The e-liquid may be substantially flavorless. That is, the e-liquid may not contain any deliberately added additional flavorant and may consist solely of a base liquid of propylene glycol and/or vegetable glycerin and nicotine.
The reservoir may be in the form of a tank. At least a portion of the tank may be light-transmissive. For example, the tank may comprise a window to allow a user to visually assess the quantity of e-liquid in the tank. A housing of the smoking substitute apparatus may comprise a corresponding aperture (or slot) or window that may be aligned with a light-transmissive portion (e.g., window) of the tank. The reservoir may be referred to as a “clearomizer” if it includes a window, or a “cartomizer” if it does not.
The smoking substitute apparatus may comprise a passage for fluid flow therethrough. The passage may extend through (at least a portion of) the smoking substitute apparatus, between openings that may define an inlet and an outlet of the passage. The outlet may be at a mouthpiece of the smoking substitute apparatus. In this respect, a user may draw fluid (e.g., air) into and through the passage by inhaling at the outlet (i.e., using the mouthpiece). The passage may be at least partially defined by the tank. The tank may substantially (or fully) define the passage, for at least a part of the length of the passage. In this respect, the tank may surround the passage, e.g., in an annular arrangement around the passage.
The aerosol generator may comprise a wick. The aerosol generator may further comprise a heater. The wick may comprise a porous material, capable of wicking the aerosol precursor. A portion of the wick may be exposed to air flow in the passage. The wick may also comprise one or more portions in contact with liquid stored in the reservoir. For example, opposing ends of the wick may protrude into the reservoir and an intermediate portion (between the ends) may extend across the passage so as to be exposed to air flow in the passage. Thus, liquid may be drawn (e.g., by capillary action) along the wick, from the reservoir to the portion of the wick exposed to air flow.
The heater may comprise a heating element, which may be in the form of a filament wound about the wick (e.g., the filament may extend helically about the wick in a coil configuration). The heating element may be wound about the intermediate portion of the wick that is exposed to air flow in the passage. The heating element may be electrically connected (or connectable) to a power source. Thus, in operation, the power source may apply a voltage across the heating element so as to heat the heating element by resistive heating. This may cause liquid stored in the wick (i.e., drawn from the tank) to be heated so as to form a vapor and become entrained in air flowing through the passage. This vapor may subsequently cool to form an aerosol in the passage, typically downstream from the heating element.
The smoking substitute apparatus may comprise a vaporization chamber. The vaporization chamber may form part of the passage in which the heater is located. The vaporization chamber may be arranged to be in fluid communication with the inlet and outlet of the passage. The vaporization chamber may be an enlarged portion of the passage. In this respect, the air as drawn in by the user may entrain the generated vapor in a flow away from heater. The entrained vapor may form an aerosol in the vaporization chamber, or it may form the aerosol further downstream along the passage. The vaporization chamber may be at least partially defined by the tank. The tank may substantially (or fully) define the vaporization chamber. In this respect, the tank may surround the vaporization chamber, e.g., in an annular arrangement around the vaporization chamber.
In use, the user may puff on a mouthpiece of the smoking substitute apparatus, i.e., draw on the smoking substitute apparatus by inhaling, to draw in an air stream therethrough. A portion, or all, of the air stream (also referred to as a “main air flow”) may pass through the vaporization chamber so as to entrain the vapor generated at the heater. That is, such a main air flow may be heated by the heater (although typically only to a limited extent) as it passes through the vaporization chamber. Alternatively, or in addition, a portion of the air stream (also referred to as a “dilution air flow” or “bypass air flow)) may bypass the vaporization chamber and be directed to mix with the generated aerosol downstream from the vaporization chamber. That is, the dilution air flow may be an air stream at an ambient temperature and may not be directly heated at all by the heater. The dilution air flow may combine with the main air flow for diluting the aerosol contained therein. The dilution air flow may merge with the main air flow along the passage downstream from the vaporization chamber. Alternatively, the dilution air flow may be directly inhaled by the user without passing though the passage of the smoking substitute apparatus.
As a user puffs on the mouthpiece, vaporized e-liquid entrained in the passing air flow may be drawn towards the outlet of passage. The vapor may cool, and thereby nucleate and/or condense along the passage to form a plurality of aerosol droplets, e.g., nicotine-containing aerosol droplets. A portion of these aerosol droplets may be delivered to and be absorbed at a target delivery site, e.g., a user's lung, whilst a portion of the aerosol droplets may instead adhere onto other parts of the user's respiratory tract, e.g., the user's oral cavity and/or throat. Typically, in some known smoking substitute apparatuses, the aerosol droplets as measured at the outlet of the passage, e.g., at the mouthpiece, may have a droplet size, d₅₀, of less than 1 μm.
In some embodiments of the disclosure, the d₅₀particle size of the aerosol particles is preferably at least 1 μm. Typically, the d₅₀particle size is not more than 10 μm, preferably not more than 9 μm, not more than 8 μm, not more than 7 μm, not more than 6 μm, not more than 5 μm, not more than 4 μm or not more than 3 μm. It is considered that providing aerosol particle sizes in such ranges permits improved interaction between the aerosol particles and the user's lungs.
The particle droplet size, d₅₀, of an aerosol may be measured by a laser diffraction technique. For example, the stream of aerosol output from the outlet of the passage may be drawn through a Malvern Spraytec laser diffraction system, where the intensity and pattern of scattered laser light are analyzed to calculate the size and size distribution of aerosol droplets. As will be readily understood, the particle size distribution may be expressed in terms of d₁₀, d₅₀and d₉₀, for example. Considering a cumulative plot of the volume of the particles measured by the laser diffraction technique, the d₁₀particle size is the particle size below which 10% by volume of the sample lies. The d₅₀particle size is the particle size below which 50% by volume of the sample lies. The d₉₀particle size is the particle size below which 90% by volume of the sample lies. Unless otherwise indicated herein, the particle size measurements are volume-based particle size measurements, rather than number-based or mass-based particle size measurements.
The smoking substitute apparatus (or main body engaged with the smoking substitute apparatus) may comprise a power source. The power source may be electrically connected (or connectable) to a heater of the smoking substitute apparatus (e.g., when the smoking substitute apparatus is engaged with the main body). The power source may be a battery (e.g., a rechargeable battery). A connector in the form of, e.g., a USB port may be provided for recharging this battery.
When the smoking substitute apparatus is in the form of a consumable, the smoking substitute apparatus may comprise an electrical interface for interfacing with a corresponding electrical interface of the main body. One or both of the electrical interfaces may include one or more electrical contacts. Thus, when the main body is engaged with the consumable, the electrical interface of the main body may be configured to transfer electrical power from the power source to a heater of the consumable via the electrical interface of the consumable.
The electrical interface of the smoking substitute apparatus may also be used to identify the smoking substitute apparatus (in the form of a consumable) from a list of known types. For example, the consumable may have a certain concentration of nicotine and the electrical interface may be used to identify this. The electrical interface may additionally or alternatively be used to identify when a consumable is connected to the main body.
Again, where the smoking substitute apparatus is in the form of a consumable, the main body may comprise an identification means, which may, for example, be in the form of an RFID reader, a barcode or QR code reader. This identification means may be able to identify a characteristic (e.g., a type) of a consumable engaged with the main body. In this respect, the consumable may include any one or more of an RFID chip, a barcode or QR code, or memory within which is an identifier and which can be interrogated via the identification means.
The smoking substitute apparatus or main body may comprise a controller, which may include a microprocessor. The controller may be configured to control the supply of power from the power source to the heater of the smoking substitute apparatus (e.g., via the electrical contacts). A memory may be provided and may be operatively connected to the controller. The memory may include non-volatile memory. The memory may include instructions which, when implemented, cause the controller to perform certain tasks or steps of a method.
The main body or smoking substitute apparatus may comprise a wireless interface, which may be configured to communicate wirelessly with another device, for example a mobile device, e.g., via Bluetooth©. To this end, the wireless interface could include a Bluetooth© antenna. Other wireless communication interfaces, e.g., WIFI©, are also possible. The wireless interface may also be configured to communicate wirelessly with a remote server.
A puff sensor may be provided that is configured to detect a puff (i.e., inhalation from a user). The puff sensor may be operatively connected to the controller so as to be able to provide a signal to the controller that is indicative of a puff state (i.e., puffing or not puffing). The puff sensor may, for example, be in the form of a pressure sensor or an acoustic sensor. That is, the controller may control power supply to the heater of the consumable in response to a puff detection by the sensor. The control may be in the form of activation of the heater in response to a detected puff. That is, the smoking substitute apparatus may be configured to be activated when a puff is detected by the puff sensor. When the smoking substitute apparatus is in the form of a consumable, the puff sensor may be provided in the consumable or alternatively may be provided in the main body.
The term “flavorant” is used to describe a compound or combination of compounds that provide flavor and/or aroma. For example, the flavorant may be configured to interact with a sensory receptor of a user (such as an olfactory or taste receptor). The flavorant may include one or more volatile substances.
The flavorant may be provided in solid or liquid form. The flavorant may be natural or synthetic. For example, the flavorant may include menthol, licorice, chocolate, fruit flavor (including, e.g., citrus, cherry etc.), vanilla, spice (e.g., ginger, cinnamon) and tobacco flavor. The flavorant may be evenly dispersed or may be provided in isolated locations and/or varying concentrations.
The present inventors consider that a flow rate of 1.3 L min⁻¹is towards the lower end of a typical user expectation of flow rate through a conventional cigarette and therefore through a user-acceptable smoking substitute apparatus. The present inventors further consider that a flow rate of 2.0 L min⁻¹is towards the higher end of a typical user expectation of flow rate through a conventional cigarette and therefore through a user-acceptable smoking substitute apparatus. Embodiments of the present disclosure therefore provide an aerosol with advantageous particle size characteristics across a range of flow rates of air through the apparatus.
The aerosol may have a Dv50 of at least 1.1 μm, at least 1.2 μm, at least 1.3 μm, at least 1.4 μm, at least 1.5 μm, at least 1.6 μm, at least 1.7 μm, at least 1.8 μm, at least 1.9 μm or at least 2.0 μm.
The aerosol may have a Dv50 of not more than 4.9 μm, not more than 4.8 μm, not more than 4.7 μm, not more than 4.6 μm, not more than 4.5 μm, not more than 4.4 μm, not more than 4.3 μm, not more than 4.2 μm, not more than 4.1 μm, not more than 4.0 μm, not more than 3.9 am, not more than 3.8 μm, not more than 3.7 μm, not more than 3.6 μm, not more than 3.5 μm, not more than 3.4 μm, not more than 3.3 μm, not more than 3.2 μm, not more than 3.1 μm or not more than 3.0 μm.
A particularly preferred range for Dv50 of the aerosol is in the range 2-3 μm.
The air inlet, flow passage, outlet and the vaporization chamber may be configured so that, when the air flow rate inhaled by the user through the apparatus is 1.3 L min⁻¹, the average magnitude of velocity of air in the vaporization chamber is in the range 0-1.3 ms⁻¹. The average magnitude velocity of air may be calculated based on knowledge of the geometry of the vaporization chamber and the flow rate.
When the air flow rate inhaled by the user through the apparatus is 1.3 L min⁻¹, the average magnitude of velocity of air in the vaporization chamber may be at least 0.001 ms⁻¹, or at least 0.005 ms⁻¹, or at least 0.01 ms⁻¹, or at least 0.05 ms⁻¹.
When the air flow rate inhaled by the user through the apparatus is 1.3 L min⁻¹, the average magnitude of velocity of air in the vaporization chamber may be at most 1.2 ms⁻¹, at most 1.1 ms⁻¹, at most 1.0 ms⁻¹, at most 0.9 ms⁻¹, at most 0.8 ms⁻¹, at most 0.7 ms⁻¹or at most 0.6 ms⁻¹.
The air inlet, flow passage, outlet and the vaporization chamber may be configured so that, when the air flow rate inhaled by the user through the apparatus is 2.0 L min⁻¹, the average magnitude of velocity of air in the vaporization chamber is in the range 0-1.3 ms⁻¹. The average magnitude velocity of air may be calculated based on knowledge of the geometry of the vaporization chamber and the flow rate.
When the air flow rate inhaled by the user through the apparatus is 2.0 L min⁻¹, the average magnitude of velocity of air in the vaporization chamber may be at least 0.001 ms⁻¹, or at least 0.005 ms⁻¹, or at least 0.01 ms⁻¹, or at least 0.05 ms⁻¹.
When the air flow rate inhaled by the user through the apparatus is 2.0 L min⁻¹, the average magnitude of velocity of air in the vaporization chamber may be at most 1.2 ms⁻¹, at most 1.1 ms⁻¹, at most 1.0 ms⁻¹, at most 0.9 ms⁻¹, at most 0.8 ms⁻¹, at most 0.7 ms⁻¹or at most 0.6 ms⁻¹.
When the calculated average magnitude of velocity of air in the vaporization chamber is in the ranges specified, it is considered that the resultant aerosol particle size is advantageously controlled to be in a desirable range. It is further considered that the configuration of the apparatus can be selected so that the average magnitude of velocity of air in the vaporization chamber can be brought within the ranges specified, at the exemplary flow rate of 1.3 L min⁻¹and/or the exemplary flow rate of 2.0 L min⁻¹.
The aerosol generator may comprise a vaporizer element loaded with aerosol precursor, the vaporizer element being heatable by a heater and presenting a vaporizer element surface to air in the vaporization chamber. A vaporizer element region may be defined as a volume extending outwardly from the vaporizer element surface to a distance of 1 mm from the vaporizer element surface.
The air inlet, flow passage, outlet and the vaporization chamber may be configured so that, when the air flow rate inhaled by the user through the apparatus is 1.3 L min⁻¹, the average magnitude of velocity of air in the vaporizer element region is in the range 0-1.2 ms⁻¹. The average magnitude of velocity of air in the vaporizer element region may be calculated using computational fluid dynamics.
When the air flow rate inhaled by the user through the apparatus is 1.3 L min⁻¹, the average magnitude of velocity of air in the vaporizer element region may be at least 0.001 ms⁻¹, or at least 0.005 ms⁻¹, or at least 0.01 ms⁻¹, or at least 0.05 ms⁻¹.
When the air flow rate inhaled by the user through the apparatus is 1.3 L min⁻¹, the average magnitude of velocity of air in the vaporizer element region may be at most 1.1 ms⁻¹, at most 1.0 ms⁻¹, at most 0.9 ms⁻¹, at most 0.8 ms⁻¹, at most 0.7 ms⁻¹or at most 0.6 ms⁻¹.
The air inlet, flow passage, outlet and the vaporization chamber may be configured so that, when the air flow rate inhaled by the user through the apparatus is 2.0 L min⁻¹, the average magnitude of velocity of air in the vaporizer element region is in the range 0-1.2 ms⁻¹. The average magnitude of velocity of air in the vaporizer element region may be calculated using computational fluid dynamics.
When the air flow rate inhaled by the user through the apparatus is 2.0 L min⁻¹, the average magnitude of velocity of air in the vaporizer element region may be at least 0.001 ms⁻¹, or at least 0.005 ms⁻¹, or at least 0.01 ms⁻¹, or at least 0.05 ms⁻¹.
When the air flow rate inhaled by the user through the apparatus is 2.0 L min⁻¹, the average magnitude of velocity of air in the vaporizer element region may be at most 1.1 ms⁻¹, at most 1.0 ms⁻¹, at most 0.9 ms⁻¹, at most 0.8 ms⁻¹, at most 0.7 ms⁻¹or at most 0.6 ms⁻¹.
When the average magnitude of velocity of air in the vaporizer element region is in the ranges specified, it is considered that the resultant aerosol particle size is advantageously controlled to be in a desirable range. It is further considered that the velocity of air in the vaporizer element region is more relevant to the resultant particle size characteristics than consideration of the velocity in the vaporization chamber as a whole. This is in view of the significant effect of the velocity of air in the vaporizer element region on the cooling of the vapor emitted from the vaporizer element surface.
Additionally, or alternatively is it relevant to consider the maximum magnitude of velocity of air in the vaporizer element region.
Therefore, the air inlet, flow passage, outlet and the vaporization chamber may be configured so that, when the air flow rate inhaled by the user through the apparatus is 1.3 L min⁻¹, the maximum magnitude of velocity of air in the vaporizer element region is in the range 0-2.0 ms⁻¹.
When the air flow rate inhaled by the user through the apparatus is 1.3 L min⁻¹, the maximum magnitude of velocity of air in the vaporizer element region may be at least 0.001 ms⁻¹, or at least 0.005 ms⁻¹, or at least 0.01 ms⁻¹, or at least 0.05 ms⁻¹.
When the air flow rate inhaled by the user through the apparatus is 1.3 L min⁻¹, the maximum magnitude of velocity of air in the vaporizer element region may be at most 1.9 ms⁻¹, at most 1.8 ms⁻¹, at most 1.7 ms⁻¹, at most 1.6 ms⁻¹, at most 1.5 ms⁻¹, at most 1.4 ms⁻¹, at most 1.3 ms⁻¹or at most 1.2 ms⁻¹.
The air inlet, flow passage, outlet and the vaporization chamber may be configured so that, when the air flow rate inhaled by the user through the apparatus is 2.0 L min⁻¹, the maximum magnitude of velocity of air in the vaporizer element region is in the range 0-2.0 ms⁻¹.
When the air flow rate inhaled by the user through the apparatus is 2.0 L min⁻¹, the maximum magnitude of velocity of air in the vaporizer element region may be at least 0.001 ms⁻¹, or at least 0.005 ms⁻¹, or at least 0.01 ms⁻¹, or at least 0.05 ms⁻¹.
When the air flow rate inhaled by the user through the apparatus is 2.0 L min⁻¹, the maximum magnitude of velocity of air in the vaporizer element region may be at most 1.9 ms⁻¹, at most 1.8 ms⁻¹, at most 1.7 ms⁻¹, at most 1.6 ms⁻¹, at most 1.5 ms⁻¹, at most 1.4 ms⁻¹, at most 1.3 ms⁻¹or at most 1.2 ms⁻¹.
It is considered that configuring the apparatus in a manner to permit such control of velocity of the airflow at the vaporizer permits the generation of aerosols with particularly advantageous particle size characteristics, including Dv50 values.
Additionally, or alternatively is it relevant to consider the turbulence intensity in the vaporizer chamber in view of the effect of turbulence on the particle size of the generated aerosol. For example, the air inlet, flow passage, outlet and the vaporization chamber may be configured so that, when the air flow rate inhaled by the user through the apparatus is 1.3 L min⁻¹, the turbulence intensity in the vaporizer element region is not more than 1%.
When the air flow rate inhaled by the user through the apparatus is 1.3 L min⁻¹, the turbulence intensity in the vaporizer element region may be not more than 0.95%, not more than 0.9%, not more than 0.85%, not more than 0.8%, not more than 0.75%, not more than 0.7%, not more than 0.65% or not more than 0.6%.
It is considered that configuring the apparatus in a manner to permit such control of the turbulence intensity in the vaporizer element region permits the generation of aerosols with particularly advantageous particle size characteristics, including Dv50 values.
Following detailed investigations, the inventors consider, without wishing to be bound by theory, that the particle size characteristics of the generated aerosol may be determined by the cooling rate experienced by the vapor after emission from the vaporizer element (e.g., wick). In particular, it appears that imposing a relatively slow cooling rate on the vapor has the effect of generating aerosols with a relatively large particle size. The parameters discussed above (velocity and turbulence intensity) are considered to be mechanisms for implementing a particular cooling dynamic to the vapor.
More generally, it is considered that the air inlet, flow passage, outlet and the vaporization chamber may be configured so that a desired cooling rate is imposed on the vapor. The particular cooling rate to be used depends of course on the nature of the aerosol precursor and other conditions. However, for a particular aerosol precursor it is possible to define a set of testing conditions in order to define the cooling rate, and by extension this imposes limitations on the configuration of the apparatus to permit such cooling rates as are shown to result in advantageous aerosols. Accordingly, the air inlet, flow passage, outlet and the vaporization chamber may be configured so that the cooling rate of the vapor is such that the time taken to cool to 50° C. is not less than 16 ms, when tested according to the following protocol. The aerosol precursor is an e-liquid consisting of 1.6% freebase nicotine and the remainder a 65:35 propylene glycol and vegetable glycerin mixture, the e-liquid having a boiling point of 209° C. Air is drawn into the air inlet at a temperature of 25° C. The vaporizer is operated to release a vapor of total particulate mass 5 mg over a 3 second duration from the vaporizer element surface in an air flow rate between the air inlet and outlet of 1.3 L min⁻¹.
Additionally, or alternatively, the air inlet, flow passage, outlet and the vaporization chamber may be configured so that the cooling rate of the vapor is such that the time taken to cool to 50° C. is not less than 16 ms, when tested according to the following protocol. The aerosol precursor is an e-liquid consisting of 1.6% freebase nicotine and the remainder a 65:35 propylene glycol and vegetable glycerin mixture, the e-liquid having a boiling point of 209° C. Air is drawn into the air inlet at a temperature of 25° C. The vaporizer is operated to release a vapor of total particulate mass 5 mg over a 3 second duration from the vaporizer element surface in an air flow rate between the air inlet and outlet of 2.0 L min⁻¹.
Cooling of the vapor such that the time taken to cool to 50° C. is not less than 16 ms corresponds to an equivalent linear cooling rate of not more than 10° C./ms.
The equivalent linear cooling rate of the vapor to 50° C. may be not more than 9° C./ms, not more than 8° C./ms, not more than 7° C./ms, not more than 6° C./ms or not more than 5° C./ms.
Cooling of the vapor such that the time taken to cool to 50° C. is not less than 32 ms corresponds to an equivalent linear cooling rate of not more than 5° C./ms.
The testing protocol set out above considers the cooling of the vapor (and subsequent aerosol) to a temperature of 50° C. This is a temperature which can be considered to be suitable for an aerosol to exit the apparatus for inhalation by a user without causing significant discomfort. It is also possible to consider cooling of the vapor (and subsequent aerosol) to a temperature of 75° C. Although this temperature is possibly too high for comfortable inhalation, it is considered that the particle size characteristics of the aerosol are substantially settled by the time the aerosol cools to this temperature (and they may be settled at still higher temperature).
Accordingly, the air inlet, flow passage, outlet and the vaporization chamber may be configured so that the cooling rate of the vapor is such that the time taken to cool to 75° C. is not less than 4.5 ms, when tested according to the following protocol. The aerosol precursor is an e-liquid consisting of 1.6% freebase nicotine and the remainder a 65:35 propylene glycol and vegetable glycerin mixture, the e-liquid having a boiling point of 209° C. Air is drawn into the air inlet at a temperature of 25° C. The vaporizer is operated to release a vapor of total particulate mass 5 mg over a 3 second duration from the vaporizer element surface in an air flow rate between the air inlet and outlet of 1.3 L min⁻¹.
Additionally, or alternatively, the air inlet, flow passage, outlet and the vaporization chamber may be configured so that the cooling rate of the vapor is such that the time taken to cool to 75° C. is not less than 4.5 ms, when tested according to the following protocol. The aerosol precursor is an e-liquid consisting of 1.6% freebase nicotine and the remainder a 65:35 propylene glycol and vegetable glycerin mixture, the e-liquid having a boiling point of 209° C. Air is drawn into the air inlet at a temperature of 25° C. The vaporizer is operated to release a vapor of total particulate mass 5 mg over a 3 second duration from the vaporizer element surface in an air flow rate between the air inlet and outlet of 2.0 L min⁻¹.
Cooling of the vapor such that the time taken to cool to 75° C. is not less than 4.5 ms corresponds to an equivalent linear cooling rate of not more than 30° C./ms.
The equivalent linear cooling rate of the vapor to 75° C. may be not more than 29° C./ms, not more than 28° C./ms, not more than 27° C./ms, not more than 26° C./ms, not more than 25° C./ms, not more than 24° C./ms, not more than 23° C./ms, not more than 22° C./ms, not more than 21° C./ms, not more than 20° C./ms, not more than 19° C./ms, not more than 18° C./ms, not more than 17° C./ms, not more than 16° C./ms, not more than 15° C./ms, not more than 14° C./ms, not more than 13° C./ms, not more than 12° C./ms, not more than 11° C./ms or not more than 10° C./ms.
Cooling of the vapor such that the time taken to cool to 75° C. is not less than 13 ms corresponds to an equivalent linear cooling rate of not more than 10° C./ms.
It is considered that configuring the apparatus in a manner to permit such control of the cooling rate of the vapor permits the generation of aerosols with particularly advantageous particle size characteristics, including Dv50 values.
The disclosure includes the combination of the aspects and preferred features described except where such a combination is clearly impermissible or expressly avoided.

SUMMARY OF THE FIGURES

So that the disclosure may be understood, and so that further aspects and features thereof may be appreciated, embodiments illustrating the principles of the disclosure will now be discussed in further detail with reference to the accompanying figures, in which:

FIG. 1 illustrates a set of rectangular tubes for use in experiments to assess the effect of flow and cooling conditions at the wick on aerosol properties. Each tube has the same depth and length but different width.

FIG. 2 shows a schematic perspective longitudinal cross sectional view of an example rectangular tube with a wick and heater coil installed.

FIG. 3 shows a schematic transverse cross sectional view an example rectangular tube with a wick and heater coil installed. In this example, the internal width of the tube is 12 mm.

FIGS. 4A-4D show air flow streamlines in the four devices used in a turbulence study.

FIG. 5 shows the experimental set up to investigate the influence of inflow air temperature on aerosol particle size, in order to investigate the effect of vapor cooling rate on aerosol generation.

FIG. 6 shows a schematic longitudinal cross sectional view of a first smoking substitute apparatus (pod 1) used to assess influence of inflow air temperature on aerosol particle size.

FIG. 7 shows a schematic longitudinal cross sectional view of a second smoking substitute apparatus (pod 2) used to assess influence of inflow air temperature on aerosol particle size.

FIG. 8A shows a schematic longitudinal cross sectional view of a third smoking substitute apparatus (pod 3) used to assess influence of inflow air temperature on aerosol particle size.

FIG. 8B shows a schematic longitudinal cross sectional view of the same third smoking substitute apparatus (pod 3) in a direction orthogonal to the view taken in FIG. 8A.

FIG. 9 shows a plot of aerosol particle size (Dv50) experimental results against calculated air velocity.

FIG. 10 shows a plot of aerosol particle size (Dv50) experimental results against the flow rate through the apparatus for a calculated air velocity of 1 m/s.

FIG. 11 shows a plot of aerosol particle size (Dv50) experimental results against the average magnitude of the velocity in the vaporizer surface region, as obtained from CFD modelling.

FIG. 12 shows a plot of aerosol particle size (Dv50) experimental results against the maximum magnitude of the velocity in the vaporizer surface region, as obtained from CFD modelling.

FIG. 13 shows a plot of aerosol particle size (Dv50) experimental results against the turbulence intensity.

FIG. 14 shows a plot of aerosol particle size (Dv50) experimental results dependent on the temperature of the air and the heating state of the apparatus.

FIG. 15 shows a plot of aerosol particle size (Dv50) experimental results against vapor cooling rate to 50° C.

FIG. 16 shows a plot of aerosol particle size (Dv50) experimental results against vapor cooling rate to 75° C.

FIG. 17 is a schematic front view of a smoking substitute system, in an engaged position;

FIG. 18 is a schematic front view of the smoking substitute system in a disengaged position;

FIG. 19 is a schematic longitudinal cross sectional view of a smoking substitute apparatus;

FIG. 20 is an enlarged schematic cross sectional view of part of the air passage and vaporization chamber;

FIG. 21 is a cross-sectional view of a smoking substitute apparatus according to an embodiment;

FIGS. 22A-C is a plan view of example geometries of a flow modifying device in the smoking substitute apparatus of FIG. 5;

FIGS. 23A-D are another plan views of example geometries of a flow modifying device in the smoking substitute apparatus of FIG. 5; and

FIGS. 24A-D are cross-sectional views of a range of different shapes for the flow modifying device.

DETAILED DESCRIPTION OF THE DISCLOSURE

Further background to the present disclosure and further aspects and embodiments of the present disclosure will now be discussed with reference to the accompanying figures. Further aspects and embodiments will be apparent to those skilled in the art. The contents of all documents mentioned in this text are incorporated herein by reference in their entirety.
FIGS. 17 and 18 illustrate a smoking substitute system in the form of an e-cigarette system 110. The system 110 comprises a main body 120 of the system 110, and a smoking substitute apparatus in the form of an e-cigarette consumable (or “pod”) 150. In the illustrated embodiment the consumable 150 (sometimes referred to herein as a smoking substitute apparatus) is removable from the main body 120, so as to be a replaceable component of the system 110. The e-cigarette system 110 is a closed system in the sense that it is not intended that the consumable should be refillable with e-liquid by a user.
As is apparent from FIGS. 17 and 18, the consumable 150 is configured to engage the main body 120. FIG. 17 shows the main body 120 and the consumable 150 in an engaged state, whilst FIG. 18 shows the main body 120 and the consumable 150 in a disengaged state. When engaged, a portion of the consumable 150 is received in a cavity of corresponding shape in the main body 120 and is retained in the engaged position byway of a snap-engagement mechanism. In other embodiments, the main body 120 and consumable 150 may be engaged by screwing one into (or onto) the other, or through a bayonet fitting, or by way of an interference fit.
The system 110 is configured to vaporize an aerosol precursor, which in the illustrated embodiment is in the form of a nicotine-based e-liquid 160. The e-liquid 160 comprises nicotine and a base liquid including propylene glycol and/or vegetable glycerin. In the present embodiment, the e-liquid 160 is flavored by a flavorant. In other embodiments, the e-liquid 160 may be flavorless and thus may not include any added flavorant.
FIG. 19 shows a schematic longitudinal cross sectional view of the smoking substitute apparatus forming part of the smoking substitute system shown in FIGS. 17 and 18. In FIG. 17, the e-liquid 160 is stored within a reservoir in the form of a tank 152 that forms part of the consumable 150. In the illustrated embodiment, the consumable 150 is a “single-use” consumable 150. That is, upon exhausting the e-liquid 160 in the tank 152, the intention is that the user disposes of the entire consumable 150. The term “single-use” does not necessarily mean the consumable is designed to be disposed of after a single smoking session. Rather, it defines the consumable 150 is not arranged to be refilled after the e-liquid contained in the tank 152 is depleted. The tank may include a vent (not shown) to allow ingress of air to replace e-liquid that has been used from the tank. The consumable 150 preferably includes a window 158 (see FIGS. 17 and 18), so that the amount of e-liquid in the tank 152 can be visually assessed. The main body 120 includes a slot 157 so that the window 158 of the consumable 150 can be seen whilst the rest of the tank 152 is obscured from view when the consumable 150 is received in the cavity of the main body 120. The consumable 150 may be referred to as a “clearomizer” when it includes a window 158, or a “cartomizer” when it does not.
In other embodiments, the e-liquid (i.e., aerosol precursor) may be the only part of the system that is truly “single-use”. That is, the tank may be refillable with e-liquid or the e-liquid may be stored in a non-consumable component of the system. For example, in such other embodiments, the e-liquid may be stored in a tank located in the main body or stored in another component that is itself not single-use (e.g., a refillable cartomizer).
The external wall of tank 152 is provided by a casing of the consumable 150. The tank 152 annularly surrounds, and thus defines a portion of, a passage 170 that extends between a vaporizer inlet 172 and an outlet 174 at opposing ends of the consumable 150. In this respect, the passage 170 comprises an upstream end at the end 151 of the consumable 150 that engages with the main body 120, and a downstream end at an opposing end of the consumable 150 that comprises a mouthpiece 154 of the system 110.
When the consumable 150 is received in the cavity of the main body 120 as shown in FIG. 19, a plurality of device air inlets 176 are formed at the boundary between the casing of the consumable and the casing of the main body. The device air inlets 176 are in fluid communication with the vaporizer inlet 172 through an inlet flow channel 178 formed in the cavity of the main body which is of corresponding shape to receive a part of the consumable 150. Air from outside of the system 110 can therefore be drawn into the passage 170 through the device air inlets 176 and the inlet flow channels 178.
When the consumable 150 is engaged with the main body 120, a user can inhale (i.e., take a puff) via the mouthpiece 154 so as to draw air through the passage 170, and so as to form an air flow (indicated by the dashed arrows in FIG. 19) in a direction from the vaporizer inlet 172 to the outlet 174. Although not illustrated, the passage 170 may be partially defined by a tube (e.g., a metal tube) extending through the consumable 150. In FIG. 3, for simplicity, the passage 170 is shown with a substantially circular cross-sectional profile with a constant diameter along its length. In other embodiments, the passage may have other cross-sectional profiles, such as oval shaped or polygonal shaped profiles. Further, in other embodiments, the cross sectional profile and the diameter (or hydraulic diameter) of the passage may vary along its longitudinal axis.
The smoking substitute system 110 is configured to vaporize the e-liquid 160 for inhalation by a user. To provide this operability, the consumable 150 comprises a heater having a porous wick 162 and a resistive heating element in the form of a heating filament 164 that is helically wound (in the form of a coil) around a portion of the porous wick 162. The porous wick 162 extends across the passage 170 (i.e., transverse to a longitudinal axis of the passage 170 and thus also transverse to the air flow along the passage 170 during use) and opposing ends of the wick 162 extend into the tank 152 (so as to be immersed in the e-liquid 160). In this way, e-liquid 160 contained in the tank 152 is conveyed from the opposing ends of the porous wick 162 to a central portion of the porous wick 162 so as to be exposed to the air flow in the passage 170.
The helical filament 164 is wound about the exposed central portion of the porous wick 162 and is electrically connected to an electrical interface in the form of electrical contacts 156 mounted at the end of the consumable that is proximate the main body 120 (when the consumable and the main body are engaged). When the consumable 150 is engaged with the main body 120, electrical contacts 156 make contact with corresponding electrical contacts (not shown) of the main body 120. The main body electrical contacts are electrically connectable to a power source (not shown) of the main body 120, such that (in the engaged position) the filament 164 is electrically connectable to the power source. In this way, power can be supplied by the main body 120 to the filament 164 in order to heat the filament 164. This heats the porous wick 162 which causes e-liquid 160 conveyed by the porous wick 162 to vaporize and thus to be released from the porous wick 162. The vaporized e-liquid becomes entrained in the air flow and, as it cools in the air flow (between the heated wick and the outlet 174 of the passage 170), condenses to form an aerosol. This aerosol is then inhaled, via the mouthpiece 154, by a user of the system 110. As e-liquid is lost from the heated portion of the wick, further e-liquid is drawn along the wick from the tank to replace the e-liquid lost from the heated portion of the wick.
The filament 164 and the exposed central portion of the porous wick 162 are positioned across the passage 170. More specifically, the part of passage that contains the filament 164 and the exposed portion of the porous wick 162 forms a vaporization chamber. In the illustrated example, the vaporization chamber has the same cross-sectional diameter as the passage 170. However, in other embodiments the vaporization chamber may have a different cross sectional profile as the passage 170. For example, the vaporization chamber may have a larger cross sectional diameter than at least some of the downstream part of the passage 170 so as to enable a longer residence time for the air inside the vaporization chamber.
FIG. 20 illustrates in more detail the vaporization chamber and therefore the region of the consumable 150 around the wick 162 and filament 164. The helical filament 164 is wound around a central portion of the porous wick 162. The porous wick extends across passage 170. E-liquid 160 contained within the tank 152 is conveyed as illustrated schematically by arrows 401, i.e., from the tank and towards the central portion of the porous wick 162.
When the user inhales, air is drawn from through the inlets 176 shown in FIG. 19, along inlet flow channel 178 to vaporization chamber inlet 172 and into the vaporization chamber containing porous wick 162. The porous wick 162 extends substantially transverse to the air flow direction. The air flow passes around the porous wick, at least a portion of the air flow substantially following the surface of the porous wick 162. In examples where the porous wick has a cylindrical cross-sectional profile, the air flow may follow a curved path around an outer periphery of the porous wick 162.
At substantially the same time as the air flow passes around the porous wick 162, the filament 164 is heated so as to vaporize the e-liquid which has been wicked into the porous wick. The air flow passing around the porous wick 162 picks up this vaporized e-liquid, and the vapor-containing air flow is drawn in direction 403 further down passage 170.
The power source of the main body 120 may be in the form of a battery (e.g., a rechargeable battery such as a lithium-ion battery). The main body 120 may comprise a connector in the form of, e.g., a USB port for recharging this battery. The main body 120 may also comprise a controller that controls the supply of power from the power source to the main body electrical contacts (and thus to the filament 164). That is, the controller may be configured to control a voltage applied across the main body electrical contacts, and thus the voltage applied across the filament 164. In this way, the filament 164 may only be heated under certain conditions (e.g., during a puff and/or only when the system is in an active state). In this respect, the main body 120 may include a puff sensor (not shown) that is configured to detect a puff (i.e., inhalation). The puff sensor may be operatively connected to the controller so as to be able to provide a signal, to the controller, which is indicative of a puff state (i.e., puffing or not puffing). The puff sensor may, for example, be in the form of a pressure sensor or an acoustic sensor.
Although not shown, the main body 120 and consumable 150 may comprise a further interface which may, for example, be in the form of an RFID reader, a barcode or QR code reader. This interface may be able to identify a characteristic (e.g., a type) of a consumable 150 engaged with the main body 120. In this respect, the consumable 150 may include any one or more of an RFID chip, a barcode or QR code, or memory within which is an identifier and which can be interrogated via the interface.
FIG. 21 shows a cross-sectional view of a smoking substitute apparatus 250 forming part of a smoking substitute system. The smoking substitute apparatus 250 is similar to the smoking substitute apparatus 150 shown in FIGS. 1 to 4, and similar features are represented by the same reference signs. The smoking substitute apparatus 250 has a flow modifying device 500 positioned upstream of the wick 162 and the heater 164. The flow modifying device 500 may take the form of a mesh, grid or some other kind of apertured element positioned across the air flow passage 200 through the apparatus 250. A function of the flow modifying device 500 is to straighten air flow leading to the wick 162 and the heater 164. This can reduce turbulence in a vaporization chamber. The flow modifying device 500 comprises a structure with an upstream side 501 and a downstream side 502. The device 500 has a plurality of apertures 505 extending through it. Each of the apertures 505 extends from the upstream side 501 to the downstream side 502. Each of the apertures 505 is parallel to the longitudinal axis 101 of the air flow passage 200. In this embodiment the flow modifying device 500 is a planar structure, but other shaped devices are possible, such as a curved or domed profile.
With current e-cigarette devices, the airflow path can be quite tortuous and prone to turbulent flows. By designing the airflow more carefully, the path can be modified to allow the airflow path to become more laminar in nature. The path being more laminar in nature, decreases the amount of turbulence which is most prevalent in the appearance of eddy currents. A laminar airflow results in the reduction in the average local velocity magnitude. This can be understood as being due to the airflow mass moving in a more consistent direction, typically axially along the flow passage and therefore with a smaller component of velocity perpendicular to the axis of the flow passage. This also reduces pressure loss and particles/droplet collisions. With a more laminar airflow, it is found that the dilution air from the inlet has a larger active contact area with the coil and wick assembly. Having an increased contact, more laminar airflow and, overall, a lowervelocity magnitude around the wick 162 and heater 164 causes an increased and more consistent aerosol particle size. It also reduces the deposition of aerosol particles on the internal surfaces facing the airflow path. This may lead to less overall perceived leakage during use, such leakage typically being due to the deposited liquid migrating out of the device along the surfaces on which it has deposited. Having a more laminar airflow overall tends to lead to a lower pressure drop across the device. By suitable design of the geometry of the air flow passage in the device the laminar airflow can be tailored to give a consistent particle size increase for tailored lung disposition and absorption.
The flow modifying device 500 may also help to reduce leakage of liquid from the vaporization chamber and the bottom (inlet 172 end) of the apparatus 250.
FIG. 22 shows some example geometries of the flow modifying device 500. The flow modifying device can be manufactured in different ways and the following is not considered to be an exhaustive list. Each of the Figures (A) to (C) shows a pattern of apertures viewed as a plan view from one side of the device (e.g., viewed from the upstream side). FIGS. 22(A) to 6(C) show a flow modifying device 500 comprising a plurality of apertures 505 arranged in a grid pattern. The aperture diameters may range from, for example, 0.7 mm to 0.2 mm. The center-to-center distances of the nearest neighbor apertures in the pattern may range from 1.5 mm to 0.3 mm. The depth/length of the apertures may, for example, have a range from 0.1 mm to an upper value of 10 mm or 20 mm. A deeper/longer flow modifying device 500 can improve the straightening effect of the air flow, but there is limited space in which to accommodate the flow modifying device 500 within the physical constraint of the consumable 150.
FIGS. 22(A) and 22(B) each show a rectangular grid pattern. FIG. 22(C) shows a rectangular grid pattern with alternate rows of the grid offset. Other, non-uniform or lower symmetry, patterns are possible.
FIG. 23 shows some more example geometries of the flow modifying device 500. Each of Figures (A) to (D) shows a pattern of apertures 505 viewed as a plan view from one side of the device (e.g., viewed from the upstream side). FIG. 23(A) shows a regular pattern of circular apertures 505. FIG. 23(B) shows a pattern of apertures 505 with non-uniform diameters. In this pattern, the aperture diameter varies from the center of the pattern (largest diameter) to the periphery of the pattern (smallest diameter). FIG. 23(C) shows an example with apertures 505 of a different shape. The apertures 505 are rounded rectangles. The apertures 505 are arranged in a grid-shaped pattern. FIG. 23(D) shows an example with linear slot-shaped apertures 505.
In any of the examples, the pattern of apertures may comprise uniform, or non-uniform, center-to-center distances.
The thickness of the flow modifying device 500 can have an effect on shaping the air flow to a laminar flow. It has been found that a thicker flow modifying device may provide more desirable performance. An example range of depths of the flow modifying device is from 0.1 mm to 20 mm, more preferably 0.1 mm to 10 mm.
The apertures may be formed from a monolithic material for example by molding, machining (e.g., drilling), etc. However, other manufacturing techniques can be used. For example, the apertures may be formed by weaving wire (such as metal wire) or strands of any suitable material to form a woven mesh structure. Apertures are formed between the strands. A range of possible aperture shapes is possible, such as circular, oval, elliptical, triangular, or other polygonal shapes.
The woven mesh structure may have apertures of uniform aperture diameter, or apertures of non-uniform aperture diameter. A woven mesh structure with apertures of non-uniform aperture diameter has a varying porosity across the woven mesh structure. Apertures of non-uniform aperture diameter may be achieved by varying the pitch of the strands of the woven mesh structure, where “pitch” is the spacing of a longitudinal axis of respective adjacent strands.
The strands or wires used to form the woven mesh structure may have a uniform strand diameter, or a non-uniform strand diameter. The use of strands of non-uniform strand diameter may provide a mesh in which the center-to-center distance between nearest neighbor apertures varies across the woven mesh structure. The use of strands of non-uniform strand diameter may provide a mesh with apertures of non-uniform aperture diameter.
The woven mesh structure may have a single woven layer, or a plurality of woven layers. For a woven mesh structure with a plurality of woven layers, the layers may have the same properties (e.g., one or more of aperture diameter, center-to-center distance between nearest neighbor apertures, strand diameter) in each layer. Alternatively, one or more of the layers may have a property, or properties (e.g., one or more of aperture diameter, center-to-center distance between nearest neighbor apertures, strand diameter) which is different to another layer. The layers of the woven mesh structure may be overlaid upon one another to provide an overall structure with increased depth, or the layers may be spaced apart to allow flow through a free space region between adjacent layers. The apertures in adjacent layers may be aligned in an axial direction.
It has been found that a more laminar flow can be achieved with small apertures and a small center-to-center distance. It has been found that a laminar flow can be achieved directly downstream of the flow modifying device 500 with an aperture diameter of around 0.2 mm. It has been found that a laminar flow can be achieved a small distance downstream of the flow modifying device 500 with an aperture diameter of around 0.45 mm. The larger diameter apertures are easier to manufacture by molding. It has been shown that the optimal range lies between 0.45 mm-0.2 mm holes for the purposes of inciting laminar flow at typical flow rates used in smoking substitute systems.
FIGS. 24A-D show a range of different shapes for the flow modifying device 500. FIGS. 24A-D show cross-sections through the flow modifying devices 500, taken along a direction which is orthogonal to the longitudinal axis 101. FIG. 24A shows a flow modifying device 500 with a generally planar shape. The device has an upstream face 501 and a downstream face 502 which are parallel to one another. A possible disadvantage with the planar shape is that liquid 511 may collect across all, or part of, the downstream face 502 of the device. This may block the apertures and reduce effectiveness of the device 500.
FIG. 24B shows another flow modifying device 510 with a planar shape. Device 510 may have any of the features described above for device 500. Device 510 has a liquid trap or “moat” 512 on the downstream side 502. The liquid trap 512 is located adjacent the outer wall 508 of the air flow passage. The liquid trap 512 is a continuous channel or trough around the perimeter of the device 510. The liquid trap 511 provides a region to collect any liquid from the downstream face 502 of the device. By moving and collecting the liquid in a defined area out of the active region of the device, the device will remain as efficient as possible.
FIG. 24C shows a flow modifying device 520 with a curved or domed shape. The device 520 is concave on the upstream face 501 and convex on the downstream face 502. The domed shape of the flow modifying device 520 is symmetrical about the longitudinal axis 101. Each of the apertures 505 in the flow modifying device 520 is parallel to the longitudinal axis 101 of the air flow passage 200. Device 520 may have any of the features described above for device 500. The domed shape can help to divert any liquid on the downstream face 502 of the device to the sides, such that air flow through the device is not blocked by excess liquid. A domed shape flow modifying device will have a curved shape when viewed in any 2D cross-section taken about the longitudinal axis 101. A flow modifying device 520 with a curved shape may be considered as a planar mesh which is curved to the shape shown in FIG. 24C.
FIG. 24D shows another flow modifying device 530 with a curved or domed shape. The device 520 is similar to the device 520. Similar to device 510, device 530 has a liquid trap or “moat” 512 on the downstream side 502. The liquid trap 512 is located adjacent the outer wall 508 of the air flow passage. The liquid trap 512 is a continuous channel or trough around the perimeter of the device 530. The liquid trap 512 provides a region to collect any liquid from the downstream face 502 of the device.
Referring again to FIGS. 24A-D, the flow modifying device 500 is positioned in the air flow passage, part-way between the inlet 172 and the wick 162/heater 164. The position of the flow modifying device 500 can have an impact on how well the laminar flow is incited and how laminar the flow is by the time it reaches the wick 162/heater 164. The distance 541 of the device 500 relative to the inlet 172 can, for example, lie in a range between 0 mm (i.e., device 500 is located at the inlet) and 5 mm. The distance 542 of the device 500 relative to the wick 162/heater 164 can, for example, lie in a range between 1 mm and 10 mm.
Advantageous effects may be achieved by controlling a temperature of the flow modifying device 500. The flow modifying device 500 may be heated, such as by supplying an electric current to an electrically conductive flow modifying device 500 to cause the generation of heat by resistive heating. In this way, the flow modifying device 500 may be operated in a similar manner as the main heater 164. In this arrangement, the flow modifying device 500 may be formed of an electrically conductive material, such as metal. Alternatively, the flow modifying device 500 may be formed of an exothermic material. In such an arrangement, the flow modifying device may be configured to undergo an exothermic reaction, e.g., on contact with an airflow, or on contact with an activating agent, and thereby generate heat to be passed on to the airflow.
As will be understood, in such an arrangement, the flow modifying device may be consumed during the use of the system.
Alternatively, the flow modifying device 500 may be cooled or formed of an endothermic material.
The flow modifying device may provide one or more of the following advantages. The flow modifying device may provide a lower pressure drop through the apparatus. For the consumer, this allows more efficient use of the force exerted on the device for the purpose of drawing vapor, i.e., a less powerful puff. The flow modifying device may provide an increased particle size. For the consumer this would increase the efficiency of nicotine deposition in the lungs and subsequent transfer to the blood stream. The flow modifying device may increase the portion of the wick 162/heater 164 which actively comes into contact with the air flow. For the user this increases the surface area of vaporization which leads to an increased TPM (total particulate matter). The flow modifying device may provide a reduction in liquid deposition around the internal airflow geometry, e.g., the air flow passage leading to the wick/heater or downstream of the wick/heater, by promotion of laminar flow. For the user this decreases liquid condensation and deposition in the airflow path. This leads to lower/zero build up which reduces leakage into the mouth or leakage of the pod during use or in the pocket. Furthermore, by management of liquid deposited along the internal surfaces facing the airflow (e.g., by capture in the “moat” at the periphery of the flow modifying device), it is possible to reduce leakage through the bottom of the apparatus.

EXAMPLES

There now follows a disclosure of certain examples of experimental work undertaken to determine the effects of certain conditions in the smoking substitute apparatus on the particle size of the generated aerosol. However, the present disclosure is to be understood to not be limited in its application to the specific experimentation, results, and laboratory procedures disclosed herein after. Rather, the Examples are simply provided as one of various embodiments and are meant to be exemplary, not exhaustive.
The experiments described in these examples are relevant to the embodiments disclosed above in particular in view of the control provided by those embodiments to the flow conditions at the wick, being shown in these experimental results to affect the particle size of the generated aerosol.

Introduction

Aerosol droplet size is a considered to be an important characteristic for smoking substitution devices. Droplets in the range of 2-5 μm are preferred in order to achieve improved nicotine delivery efficiency and to minimize the hazard of second-hand smoking. However, at the time of writing (September 2019), commercial EVP devices typically deliver aerosols with droplet size averaged around 0.5 μm, and to the knowledge of the inventors not a single commercially available device can deliver an aerosol with an average particle size exceeding 1 μm.
The present inventors speculate, without themselves wishing to be bound by theory, that there has to date been a lack of understanding in the mechanisms of e-liquid evaporation, nucleation and droplet growth in the context of aerosol generation in smoking substitute devices.
The present inventors have therefore studied these issues in order to provide insight into mechanisms for the generation of aerosols with larger particles. The present inventors have carried out experimental and modelling work alongside theoretical investigations, leading to significant achievements as now reported.
This disclosure considers the roles of air velocity, air turbulence and vapor cooling rate in affecting aerosol particle size.

2. Experiments

In the following examples, a Malvern PANalytical Spraytec laser diffraction system was employed for the particle size measurement. In order to limit the number of variables, the same coil and wick (1.5 ohms Ni—Cr coil, 1.8 mm Y07 cotton wick), the same e-liquid (1.6% freebase nicotine, 65:35 propylene glycol (PG)/vegetable glycerin (VG) ratio, no added flavor) and the same input power (10 W) were used in all experiments. Y07 represents the grade of cotton wick, meaning that the cotton has a linear density of 0.7 grams per meter.
Particle sizes were measured in accordance with ISO 13320:2009(E), which is an international standard on laser diffraction methods for particle size analysis. This is particularly well suited to aerosols, because there is an assumption in this standard that the particles are spherical (which is a good assumption for liquid-based aerosols). The standard is stated to be suitable for particle sizes in the range 0.1 micron to 3 mm.
The results presented here concentrate on the volume-based median particle size Dv50. This is to be taken to be the same as the parameter d₅₀used above.

First Example: Rectangular Tube Testing

The work of a first example reported here based on the inventors' insight that aerosol particle size might be related to: 1) air velocity; 2) flow rate; and 3) Reynolds number. In a given EVP device, these three parameters are inter-linked to each other, making it difficult to draw conclusions on the roles of each individual factor. In order to decouple these factors, experiments of the first example were carried out using a set of rectangular tubes having different dimensions. These were manufactured by 3D printing. The rectangular tubes were 3D printed in an MJP 2500 3D printer. FIG. 1 illustrates the set of rectangular tubes. Each tube has the same depth and length but different width. Each tube has an integral end plate in order to provide a seal against air flow outside the tube. Each tube also has holes formed in opposing side walls in order to accommodate a wick.
FIG. 2 shows a schematic perspective longitudinal cross sectional view of an example rectangular tube 1170 with a wick 1162 and heater coil 1164 installed. The location of the wick is about half way along the length of the tube. This is intended to allow the flow of air along the tube to settle before reaching the wick.
FIG. 3 shows a schematic transverse cross sectional view an example rectangular tube 1170 with a wick 1162 and heater coil 1164 installed. In this example, the internal width of the tube is 12 mm
The rectangular tubes were manufactured to have same internal depth of 6 mm in order to accommodate the standardized coil and wick, however the tube internal width varied from 4.5 mm to 50 mm. In this disclosure, the “tube size” is referred to as the internal width of rectangular tubes.
The rectangular tubes with different dimensions were used to generate aerosols that were tested for particle size in a Malvern PANalytical Spraytec laser diffraction system. An external digital power supply was dialed to 2.6 A constant current to supply 10 W power to the heater coil in all experiments. Between two runs, the wick was saturated manually by applying one drop of e-liquid on each side of the wick.
Three groups of experiments were carried out in this study:

- 1. 1.3 lpm (liters per minute, L min⁻¹or LPM) constant flow rate on different size tubes
- 2. 2.0 lpm constant flow rate on different size tubes
- 3. 1 m/s constant air velocity on 3 tubes: i) 5 mm tube at 1.4 lpm flow rate; ii) 8 mm tube at 2.8 lpm flow rate; and iii) 20 mm tube at 8.6 lpm flow rate.

Table 1 shows a list of experiments of the first example. The values in “calculated air velocity” column were obtained by simply dividing the flow rate by the intersection area at the center plane of wick. Reynolds numbers (Re) were calculated through the following equation:
$Re = \frac{ρ v L}{μ}$
where: ρ is the density of air (1.225 kg/m³); v is the calculated air velocity in Table 1; μ is the viscosity of air (1.48×10⁻⁵m²/s); L is the characteristic length calculated by:
$L = \frac{4 P}{A}$
where: P is the perimeter of the flow path's intersection, and A is the area of the flow path's intersection.

TABLE 1

List of experiments in the rectangular
tube study of the first example

			Calculated
Tube size	Flow rate	Reynolds	air velocity
[mm]	[lpm]	number	[m/s]

1.3 lpm	4.5	1.3	153	1.17
constant	6	1.3	142	0.71
flow rate	7	1.3	136	0.56
	8	1.3	130	0.47
	10	1.3	120	0.35
	12	1.3	111	0.28
	20	1.3	86	0.15
	50	1.3	47	0.06
2.0 lpm	4.5	2.0	236	1.81
constant	5	2.0	230	1.48
flow rate	6	2.0	219	1.09
	8	2.0	200	0.72
	12	2.0	171	0.42
	20	2.0	132	0.23
	50	2.0	72	0.09
1.0 m/s	5.0	1.4	155	1.00
constant air	8	2.8	279	1.00
velocity	20	8.6	566	1.00

Five repetition runs were carried out for each tube size and flow rate combination. Between adjacent runs there were at least 5 minutes wait time for the Spraytec system to be purged. In each run, real time particle size distributions were measured in the Spraytec laser diffraction system at a sampling rate of 2500 per second, the volume distribution median (Dv50) was averaged over a puff duration of 4 seconds. Measurement results were averaged and the standard deviations were calculated to indicate errors as shown in section 4 below.

Second Example: Turbulence Tube Testing

The Reynolds numbers in Table 1 are all well below 1000, therefore, it is considered fair to assume all the experiments of the first example would be under conditions of laminar flow. Further experiments were carried out and reported in a second example to investigate the role of turbulence.
Turbulence intensity was introduced as a quantitative parameter to assess the level of turbulence. The definition and simulation of turbulence intensity is discussed below.
Different device designs were considered in order to introduce turbulence. In the experiments of the second example reported here, jetting panels were added in the existing 12 mm rectangular tubes upstream of the wick. This approach enables direct comparison between different devices as they all have highly similar geometry, with turbulence intensity being the only variable.
FIGS. 4A-4D show air flow streamlines in the four devices used in this turbulence study of the second example. FIG. 4A is a standard 12 mm rectangular tube with wick and coil installed as explained in the previous section, with no jetting panel. FIG. 4B has a jetting panel located 10 mm below (upstream from) the wick. FIG. 4C has the same jetting panel 5 mm below the wick. FIG. 4D has the samejetting panel 2.5 mm below the wick. As can be seen from FIGS. 4B-4D, the jetting panel has an arrangement of apertures shaped and directed in order to promotejetting from the downstream face of the panel and therefore to promote turbulent flow. Accordingly, the jetting panel can introduce turbulence downstream, and the panel causes higher level of turbulence near the wick when it is positioned closer to the wick. As shown in FIGS. 4A-4D, the four geometries gave turbulence intensities of 0.55%, 0.77%, 1.06% and 1.34%, respectively, with FIG. 4A being the least turbulent, and FIG. 4D being the most turbulent.
For each of FIGS. 4A-4D, there are shown three modelling images. The image on the left shows the original image (color in the original), the central image shows a greyscale version of the image and the right image shows a black and white version of the image. As will be appreciated, each version of the image highlights slightly different features of the flow. Together, they give a reasonable picture of the flow conditions at the wick.
These four devices were operated to generate aerosols following the procedure explained above (in the first example) using a flow rate of 1.3 lpm and the generated aerosols were tested for particle size in the Spraytec laser diffraction system.

Third Example: High Temperature Testing

This experiment of a third example aimed to investigate the influence of inflow air temperature on aerosol particle size, in order to investigate the effect of vapor cooling rate on aerosol generation.
The experimental set up of the third example is shown in FIG. 5. The testing used a Carbolite Gero EHA 12300B tube furnace 3210 with a quartz tube 3220 to heat up the air. Hot air in the tube furnace was then led into a transparent housing 3158 that contains the EVP device 3150 to be tested. A thermocouple meter 3410 was used to assess the temperature of the air pulled into the EVP device. Once the EVP device was activated, the aerosol was pulled into the Spraytec laser diffraction system 3310 via a silicone connector 3320 for particle size measurement.
Three smoking substitute apparatuses (referred to as “pods”) were tested in the study: pod 1 is the commercially available “myblu optimised” pod (FIG. 6); pod 2 is a pod featuring an extended inflow path upstream of the wick (FIG. 7); and pod 3 is pod with the wick located in a stagnant vaporization chamber and the inlet air bypassing the vaporization chamber but entraining the vapor from an outlet of the vaporization chamber (FIGS. 8A and 8B).
Pod 1, shown in longitudinal cross sectional view (in the width plane) in FIG. 6, has a main housing that defines a tank 160 x holding an e-liquid aerosol precursor. Mouthpiece 154 x is formed at the upper part of the pod. Electrical contacts 156 x are formed at the lower end of the pod. Wick 162 x is held in a vaporization chamber. The air flow direction is shown using arrows.
Pod 2, shown in longitudinal cross sectional view (in the width plane) in FIG. 7, has a main housing that defines a tank 160 y holding an e-liquid aerosol precursor. Mouthpiece 154 y is formed at the upper part of the pod. Electrical contacts 156 y are formed at the lower end of the pod. Wick 162 y is held in a vaporization chamber. The air flow direction is shown using arrows. Pod 2 has an extended inflow path (plenum chamber 157 y) with a flow conditioning element 159 y, configured to promote reduced turbulence at the wick 162 y.
FIG. 8A shows a schematic longitudinal cross sectional view of pod 3. FIG. 8B shows a schematic longitudinal cross sectional view of the same pod 3 in a direction orthogonal to the view taken in FIG. 8A. Pod 3 has a main housing that defines a tank 160 z holding an e-liquid aerosol precursor. Mouthpiece 154 z is formed at the upper part of the pod. Electrical contacts 156 z are formed at the lower end of the pod. Wick 162 z is held in a vaporization chamber. The air flow direction is shown using arrows. Pod 3 uses a stagnant vaporizer chamber, with the air inlets bypassing the wick and picking up the vapor/aerosol downstream of the wick.
All three pods were filled with the same e-liquid (1.6% freebase nicotine, 65:35 PG/VG ratio, no added flavor). Three experiments were carried out for each pod: 1) standard measurement in ambient temperature; 2) only the inlet air was heated to 50° C.; and 3) both the inlet air and the pods were heated to 50° C. Five repetition runs were carried out for each experiment and the Dv50 results were taken and averaged.
Modelling Work
In the following examples, modelling work was performed using COMSOL Multiphysics 5.4, engaged physics include: 1) laminar single-phase flow; 2) turbulent single-phase flow; 3) laminar two-phase flow; 4) heat transfer in fluids; and (5) particle tracing. Data analysis and data visualization were mostly completed in MATLAB R2019a.

Fourth Example: Velocity Modelling

Air velocity in the vicinity of the wick is believed to play an important role in affecting particle size. In the first example, the air velocity was calculated by dividing the flow rate by the intersection area, which is referred to as “calculated velocity”. This involves a very crude simplification that assumes velocity distribution to be homogeneous across the intersection area.
In order to increase reliability of the work, computational fluid dynamics (CFD) modelling was performed to obtain more accurate velocity values:

- 1) The average velocity in the vicinity of the wick (defined as a volume from the wick surface to 1 mm away from the wick surface)
- 2) The maximum velocity in the vicinity of the wick (defined as a volume from the wick surface to 1 mm away from the wick surface)

TABLE 2

Average and maximum velocity in the vicinity
of wick surface obtained from CFD modelling

Tube	Flow	Calculated	Average	Maximum
size	rate	velocity*	velocity**	Velocity**
[mm]	[lpm]	[m/s]	[m/s]	[m/s]

1.3 lpm	4.5	1.3	1.17	0.99	1.80
constant	6	1.3	0.71	0.66	1.22
flow rate	7	1.3	0.56	0.54	1.01
	8	1.3	0.47	0.46	0.86
	10	1.3	0.35	0.35	0.66
	12	1.3	0.28	0.27	0.54
	20	1.3	0.15	0.15	0.32
	50	1.3	0.06	0.05	0.12
2.0 lpm	4.5	2.0	1.81	1.52	2.73
constant	5	2.0	1.48	1.31	2.39
flow rate	6	2.0	1.09	1.02	1.87
	8	2.0	0.72	0.71	1.31
	12	2.0	0.42	0.44	0.83
	20	2.0	0.23	0.24	0.49
	50	2.0	0.09	0.08	0.19

*Calculated by dividing flow rate with intersection area
**Obtained from CFD modelling

The CFD model uses a laminar single-phase flow setup. For each experiment, the outlet was configured to a corresponding flowrate, the inlet was configured to be pressure-controlled, the wall conditions were set as “no slip”. A 1 mm wide ring-shaped domain (wick vicinity) was created around the wick surface, and domain probes were implemented to assess the average and maximum magnitudes of velocity in this ring-shaped wick vicinity domain.
The CFD model outputs the average velocity and maximum velocity in the vicinity of the wick for each set of experiments carried out in section 2.1. The outcomes are reported in Table 2.

Fifth Example: Turbulence Modelling

Turbulence intensity (I) is a quantitative value that represents the level of turbulence in a fluid flow system. It is defined as the ratio between the root-mean-square of velocity fluctuations, u′, and the Reynolds-averaged mean flow velocity, U:
$I = \frac{u^{'}}{U} = \frac{\sqrt{\frac{1}{3} (u_{x}^{′2} + u_{y}^{′2} + u_{z}^{′2})}}{\sqrt{{\overline{u_{x}}}^{2} + {\overline{u_{y}}}^{2} + {\overline{u_{z}}}^{2}}} = \frac{\sqrt{\frac{1}{3} [{(u_{x} - \overline{u_{x}})}^{2} + {(u_{y} - \overline{u_{y}})}^{2} + + {(u_{z} - \overline{u_{z}})}^{2}]}}{\sqrt{{\overline{u_{x}}}^{2} + {\overline{u_{y}}}^{2} + {\overline{u_{z}}}^{2}}}$
where u_x, u_yand u_zare the x-, y- and z-components of the velocity vector, u_x , u_y , and u_z represent the average velocities along three directions.
Higher turbulence intensity values represent higher levels of turbulence. As a rule of thumb, turbulence intensity below 1% represents a low-turbulence case, turbulence intensity between 1% and 5% represents a medium-turbulence case, and turbulence intensity above 5% represents a high-turbulence case.
In a fifth example, turbulence intensity was obtained from CFD simulation using turbulent single-phase setup in COMSOL Multiphysics. For each of the four experiments explained in the second example, the outlet was set to 1.3 lpm, the inlet was set to be pressure-controlled, and all wall conditions were set to be “no slip”.
Turbulence intensity was assessed within the volume up to 1 mm away from the wick surface (defined as the wick vicinity domain). For the four experiments of the second example, the turbulence intensities are 0.55%, 0.77%, 1.06% and 1.34%, respectively, as also shown in FIGS. 4A-4D.

Sixth Example: Cooling Rate Modelling

The cooling rate modelling of the sixth example involves three coupling models in COMSOL Multiphysics: 1) laminar two-phase flow; 2) heat transfer in fluids, and 3) particle tracing. The model is setup in three steps:
(1) Set Up Two Phase Flow Model
Laminar mixture flow physics was selected in this study of the sixth example. The outlet was configured in the same way as the fourth example. However, this model of the sixth example includes two fluid phases released from two separate inlets: the first one is the vapor released from wick surface, at an initial velocity of 2.84 cm/s (calculated based on 5 mg total particulate mass over 3 seconds puff duration) with initial velocity direction normal to the wick surface; the second inlet is air influx from the base of tube, the rate of which is pressure-controlled.
(2) Set Up Two-Way Coupling with Heat Transfer Physics
The inflow and outflow settings in heat transfer physics was configured in the same way as in the two-phase flow model. The air inflow was set to 25° C., and the vapor inflow was set to 209° C. (boiling temperature of the e-liquid formulation). In the end, the heat transfer physics is configured to be two-way coupled with the laminar mixture flow physics. The above model reaches steady state after approximately 0.2 second with a step size of 0.001 second.
(3) Set Up Particle Tracing
A wave of 2000 particles were release from wick surface at t=0.3 second after the two-phase flow and heat transfer model has stabilized. The particle tracing physics has one-way coupling with the previous model, which means the fluid flow exerts dragging force on the particles, whereas the particles do not exert counterforce on the fluid flow. Therefore, the particles function as moving probes to output vapor temperature at each timestep.
The model of the sixth example outputs average vapor temperature at each time steps. A MATLAB script was then created to find the time step when the vapor cools to a target temperature (50° C. or 75° C.), based on which the vapor cooling rates were obtained (Table 3).

TABLE 3

Average vapor cooling rate obtained from Multiphysics
modelling of the sixth example

		Cooling rate	Cooling rate
Tube size	Flow rate	to 50° C.	to 75° C.
[mm]	[lpm]	[° C./ms]	[° C./ms]

1.3 lpm	4.5	1.3	11.4	44.7
constant	6	1.3	5.48	14.9
flow rate	7	1.3	3.46	7.88
	8	1.3	2.24	5.15
	10	1.3	1.31	2.85
	12	1.3	0.841	1.81
	20	1.3	0*	0.536
	50	1.3	0	0
2.0 lpm	4.5	2.0	19.9	670
constant	5	2.0	13.3	67
flow rate	6	2.0	8.83	26.8
	8	2.0	3.61	8.93
	12	2.0	1.45	3.19
	20	2.0	0.395	0.761
	50	2.0	0	0

*Zero cooling rate when the average vapor temperature is still above target temperature after 0.5 second

Results and Discussions
Particle size measurement results for the rectangular tube testing of the above examples are shown in Table 4. For every tube size and flow rate combination, five repetition runs were carried out in the Spraytec laser diffraction system. The Dv50 values from five repetition runs were averaged, and the standard deviations were calculated to indicate errors, as shown in Table 4.
For the examples, the roles of different factors affecting aerosol particle size will be discussed based on experimental and modelling results.

TABLE 4

Particle size measurement results for the rectangular tube testing

Tube	Flow	Dv50	Dv50 standard
size	rate	average	deviation
[mm]	[lpm]	[μm]	[μm]

1.3 lpm	4.5	1.3	0.971	0.125
constant	6	1.3	1.697	0.341
flow rate	7	1.3	2.570	0.237
	8	1.3	2.705	0.207
	10	1.3	2.783	0.184
	12	1.3	3.051	0.325
	20	1.3	3.116	0.354
	50	1.3	3.161	0.157
2.0 lpm	4.5	2.0	0.568	0.039
constant	5	2.0	0.967	0.315
flow rate	6	2.0	1.541	0.272
	8	2.0	1.646	0.363
	12	2.0	3.062	0.153
	20	2.0	3.566	0.260
	50	2.0	3.082	0.440
1.0 m/s	5.0	1.4	1.302	0.187
constant air	8	2.8	1.303	0.468
velocity	20	8.6	1.463	0.413

Seventh Example: Decouple the Factors Affecting Particle Size

The particle size (Dv50) experimental results of a seventh example the above example are plotted against calculated air velocity in FIG. 9. The graph shows a strong correlation between particle size and air velocity.
Different size tubes were tested at two flow rates: 1.3 lpm and 2.0 lpm. Both groups of data show the same trend that slower air velocity leads to larger particle size. The conclusion was made more convincing by the fact that these two groups of data overlap well in FIG. 9: for example, the 6 mm tube delivered an average Dv50 of 1.697 μm when tested at 1.3 lpm flow rate, and the 8 mm tube delivered a highly similar average Dv50 of 1.646 μm when tested at 2.0 lpm flow rate, as they have similar air velocity of 0.71 and 0.72 m/s, respectively.
In addition, FIG. 10 shows the results of three experiments of the seventh example with highly different setup arrangements: 1) 5 mm tube measured at 1.4 lpm flow rate with Reynolds number of 155; 2) 8 mm tube measured at 2.8 lpm flow rate with Reynolds number of 279; and 3) 20 mm tube measured at 8.6 lpm flow rate with Reynolds number of 566. It is relevant that these setup arrangements have one similarity: the air velocities are all calculated to be 1 m/s. FIG. 10 shows that, although these three sets of experiments of the seventh example have different tube sizes, flow rates and Reynolds numbers, they all delivered similar particle sizes, as the air velocity was kept constant. These three data points were also plotted out in FIG. 9 (1 m/s data with star marks) and they tie in nicely into particle size-air velocity trendline.
The above results of the seventh example lead to a strong conclusion that air velocity is an important factor affecting the particle size of EVP devices. Relatively large particles are generated when the air travels with slower velocity around the wick. It can also be concluded that flow rate, tube size and Reynolds number are not necessarily independently relevant to particle size, providing the air velocity is controlled in the vicinity of the wick.

Eighth Example: Further Consideration of Velocity

In FIG. 9 the “calculated velocity” was obtained by dividing the flow rate by the intersection area, which is a crude simplification that assumes a uniform velocity field. In order to increase reliability of the work, CFD modelling has been performed to assess the average and maximum velocities in the vicinity of the wick in an eighth example. In this example, the “vicinity” was defined as a volume from the wick surface up to 1 mm away from the wick surface.
The particle size measurement data were plotted against the average velocity (FIG. 11) and maximum velocity (FIG. 12) in the vicinity of the wick, as obtained from CFD modelling.
The data in these two graphs indicates that in order to obtain an aerosol with Dv50 larger than 1 μm, the average velocity should be less than or equal to 1.2 m/s in the vicinity of the wick and the maximum velocity should be less than or equal to 2.0 m/s in the vicinity of the wick.
Furthermore, in order to obtain an aerosol with Dv50 of 2 μm or larger, the average velocity should be less than or equal to 0.6 m/s in the vicinity of the wick and the maximum velocity should be less than or equal to 1.2 m/s in the vicinity of the wick.
It is considered that typical commercial EVP devices deliver aerosols with Dv50 around 0.5 μm, and there is no commercially available device that can deliver aerosol with Dv50 exceeding 1 μm. It is considered that typical commercial EVP devices have average velocity of 1.5-2.0 m/s in the vicinity of the wick.

Ninth Example: The Role of Turbulence

The role of turbulence has been investigated in a ninth example in terms of turbulence intensity, which is a quantitative characteristic that indicates the level of turbulence. In this work, four tubes of different turbulence intensities were used to general aerosols which were measured in the Spraytec laser diffraction system. The particle size (Dv50) experimental results are plotted against turbulence intensity in FIG. 13.
The graph suggests a correlation between particle size and turbulence intensity, that lower turbulence intensity is beneficial for obtaining larger particle size. It is noted that when turbulence intensity is above 1% (medium-turbulence case), there are relatively large measurement fluctuations. In FIG. 13, the tube with a jetting panel 10 mm below the wick has the largest error bar, because airjets become unpredictable near the wick after traveling through a long distance.
The results of the ninth example clearly indicate that laminar air flow is favorable for the generation of aerosols with larger particles, and that the generation of large particle sizes is jeopardized by introducing turbulence. In FIG. 13, the 12 mm standard rectangular tube (without jetting panel) delivers above 3 μm particle size (Dv50). The particle size values reduced by at least a half when jetting panels were added to introduce turbulence.

Tenth Example: Vapor Cooling Rate

FIG. 14 shows the high temperature testing results. Larger particle sizes were observed from all 3 pods when the temperature of inlet air increased from room temperature (23° C.) to 50° C. When the pods were heated as well, two of the three pods saw even larger particle size measurement results, while pod 2 was unable to be measured due to significant amount of leakage.
Without wishing to be bound by theory, the results are in line with the inventors' insight that control over the vapor cooling rate in a tenth example provides an important degree of control over the particle size of the aerosol. As reported above, the use of a slow air velocity can have the result of the formation of an aerosol with large Dv50. It is considered that this is due to slower air velocity allowing a slower cooling rate of the vapor.
Another conclusion related to laminar flow can also be explained by a cooling rate theory: laminar flow allows slow and gradual mixing between cold air and hot vapor, which means the vapor can cool down in slower rate when the airflow is laminar, resulting in larger particle size.
The results in FIG. 14 further validate this cooling rate theory of the tenth example: when the inlet air has higher temperature, the temperature difference between hot vapor and cold air becomes smaller, which allows the vapor to cool down at a slower rate, resulting in larger particle size; when the pods were heated as well, this mechanism was exaggerated even more, leading to an even slower cooling rate and an even larger particle size.

Eleventh Example: Further Consideration of Vapor Cooling Rate

In the sixth example, the vapor cooling rates for each tube size and flow rate combination were obtained via multiphysics simulation. In FIG. 15 and FIG. 16, the particle size measurement results were plotted against vapor cooling rate to 50° C. and 75° C., respectively.
The data in these graphs indicates that in order to obtain an aerosol with Dv50 larger than 1 μm, the apparatus should be operable to require more than 16 ms for the vapor to cool to 50° C., or an equivalent (simplified to an assumed linear) cooling rate being slower than 10° C./ms. From an alternative viewpoint, in order to obtain an aerosol with Dv50 larger than 1 μm, the apparatus should be operable to require more than 4.5 ms for the vapor to cool to 75° C., or an equivalent (simplified to an assumed linear) cooling rate slower than 30° C./ms.
Furthermore, in order to obtain an aerosol with Dv50 of 2 μm or larger, the apparatus should be operable to require more than 32 ms for the vapor to cool to 50° C., or an equivalent (simplified to an assumed linear) cooling rate being slower than 5° C./ms. From an alternative viewpoint, in order to obtain an aerosol with Dv50 of 2 μm or larger, the apparatus should be operable to require more than 13 ms for the vapor to cool to 75° C., or an equivalent (simplified to an assumed linear) cooling rate slower than 10° C./ms.

Conclusions of Particle Size Experimental Work

In the above examples, particle size (Dv50) of aerosols generated in a set of rectangular tubes was studied in order to decouple different factors (flow rate, air velocity, Reynolds number, tube size) affecting aerosol particle size. It is considered that air velocity is an important factor affecting particle size—slower air velocity leads to larger particle size. When air velocity was kept constant, the other factors (flow rate, Reynolds number, tube size) has low influence on particle size.
The role of turbulence was also investigated. It is considered that laminar air flow favors generation of large particles, and introducing turbulence deteriorates (reduces) the particle size.
Modelling methods were used to simulate the average air velocity, the maximum air velocity, and the turbulence intensity in the vicinity of the wick. A COMSOL model with three coupled physics has also been developed to obtain the vapor cooling rate.
All experimental and modelling results of the above examples support a cooling rate theory that slower vapor cooling rate is a significant factor in ensuring larger particle size. Slower air velocity, laminar air flow and higher inlet air temperature lead to larger particle size, because they all allow vapor to cool down at slower rates.
The features disclosed in the foregoing description, or in the following claims, or in the accompanying drawings, of in the above examples, expressed in their specific forms or in terms of a means for performing the disclosed function, or a method or process for obtaining the disclosed results, as appropriate, may, separately, or in any combination of such features, be utilized for realizing the disclosure in diverse forms thereof.
While the disclosure has been described in conjunction with the exemplary embodiments and examples described above, many equivalent modifications and variations will be apparent to those skilled in the art when given this disclosure. Accordingly, the exemplary embodiments of the disclosure and various examples set forth above are considered to be illustrative and not limiting. Various changes to the described embodiments may be made without departing from the spirit and scope of the disclosure.
For the avoidance of any doubt, any theoretical explanations provided herein are provided for the purposes of improving the understanding of a reader. The inventors do not wish to be bound by any of these theoretical explanations.
Any section headings used herein are for organizational purposes only and are not to be construed as limiting the subject matter described.
Throughout this specification, including the claims which follow, unless the context requires otherwise, the words “have”, “comprise”, and “include”, and variations such as “having”, “comprises”, “comprising”, and “including” will be understood to imply the inclusion of a stated integer or step or group of integers or steps but not the exclusion of any other integer or step or group of integers or steps.
It must be noted that, as used in the specification and the appended claims, the singular forms “a,” “an,” and “the” include plural referents unless the context clearly dictates otherwise. Ranges may be expressed herein as from “about” one particular value, and/or to “about” another particular value. When such a range is expressed, another embodiment includes from the one particular value and/or to the other particular value. Similarly, when values are expressed as approximations, by the use of the antecedent “about,” it will be understood that the particular value forms another embodiment. The term “about” in relation to a numerical value is optional and means, for example, +/−10%.
The words “preferred” and “preferably” are used herein refer to embodiments of the disclosure that may provide certain benefits under some circumstances. It is to be appreciated, however, that other embodiments may also be preferred under the same or different circumstances. The recitation of one or more preferred embodiments therefore does not mean or imply that other embodiments are not useful, and is not intended to exclude other embodiments from the scope of the disclosure, or from the scope of the claims.

Claims

1. A smoking substitute apparatus comprising:

a housing;

an air inlet and an air outlet formed in the housing, wherein the air inlet is in fluid communication with the air outlet through an air flow passage;

an aerosol generator located in the air flow passage configured to generate an aerosol from an aerosol precursor; and

a flow modifying device extending across the air flow passage at a position between the air inlet and the aerosol generator, wherein the flow modifying device is configured to incite a laminar property to the air flow to the aerosol generator.

2. A smoking substitute apparatus according to claim 1, wherein the flow modifying device comprises a structure with an upstream face, a downstream face and a plurality of apertures through the structure between the upstream face and the downstream face.

3. A smoking substitute apparatus according to claim 2, wherein the plurality of apertures are of uniform size.

4. A smoking substitute apparatus according to claim 2, wherein the plurality of apertures are of non-uniform size.

5. A smoking substitute apparatus according to claim 4, wherein the plurality of apertures are arranged in a pattern and the size of the apertures varies from a center of the pattern towards an edge of the pattern.

6. A smoking substitute apparatus according to claim 5, wherein a largest aperture, or largest apertures, of the pattern are located at the center of the pattern.

7. A smoking substitute apparatus according to claim 5, wherein a largest aperture, or largest apertures, of the pattern are located at the edge of the pattern.

8. A smoking substitute apparatus according to claim 2, wherein the plurality of apertures are arranged in a uniform pattern.

9. A smoking substitute apparatus according to claim 2, wherein the plurality of apertures are arranged in a non-uniform pattern.

10. A smoking substitute apparatus according to claim 2, wherein the plurality of apertures have a size in a range from about 0.2 mm to about 0.7 mm.

11. A smoking substitute apparatus according to claim 2, wherein the plurality of apertures have a depth in a range from about 0.1 mm to about 10 mm.

12. A smoking substitute apparatus according to claim 2, wherein the structure is a woven mesh structure of strands with the apertures formed between the strands.

13. A smoking substitute apparatus according to claim 1, wherein the upstream face and the downstream face of the flow modifying device are substantially planar and orthogonal to the air flow passage.

14. A smoking substitute apparatus according to claim 1, wherein at least the downstream face of the flow modifying device has a curved or domed shape.

15. A smoking substitute apparatus according to claim 1, wherein the flow modifying device comprises a channel at, or adjacent to, a lateral edge of the flow modifying device.

16. A smoking substitute apparatus according to claim 14, wherein the channel extends continuously around a periphery of the flow modifying device.

17. A smoking substitute apparatus according to claim 1, wherein the flow modifying device is formed of an electrically conductive material.

18. A smoking substitute apparatus according to claim 17, wherein the flow modifying device is heated.

19. A smoking substitute apparatus according to claim 1 wherein the aerosol generator includes a heater operable to vaporize the aerosol precursor.

20. A smoking substitute system comprising:

a main body; and

a smoking substitute apparatus comprising:

a housing;