Multi-liquid nozzle

Abstract

The present invention relates to the field of nozzles for inhalation devices for liquids. In particular, the present invention relates to a spray nozzle for an inhalation device suitable for generating an aerosol of a medically active liquid, and to an inhalation device including such a nozzle. Such a nozzle (1) for an inhalation device for generating an aerosol of a medically active liquid (F, F1, F2) comprises a main axis (Z) and at least three ejection channels (1A, 1B, 1C, 1D) adapted to eject the liquids (F, F1, F2) along respective ejection trajectories, wherein at least two of the ejection trajectories intersect with each other at at least two impingement points (X1, X2), and / or wherein all ejection angles (A, A1, A2) at which the individual trajectories leave the nozzle (1) are the same or at least one of the ejection angles (A, A1, A2) is different from the other ejection angles (A, A1, A2). [Selection diagram] Figure 4

Description

[Technical field]

[0001] The present invention relates to the field of nozzles for inhalation devices for liquids, in particular to an atomizing nozzle for an inhalation device suitable for generating an aerosol of a medically active liquid. [Background technology]

[0002] Nebulizers or other aerosol generators for liquids have been known in the art for a long time. Among other things, such devices are used in medicine and therapy. In medicine and therapy, nebulizers or other aerosol generators serve as inhalation devices for the application of active ingredients in the form of aerosols, i.e. small droplets embedded in a gas. Such inhalation devices are known, for example, from EP 0627230. The essential components of this inhalation device are a reservoir in which the liquid to be aerosolized is contained, a pump unit for generating a pressure high enough to atomize, and an atomizing device in the form of a nozzle. A pump unit is defined as a unit or device component capable of moving or compressing a fluid material, comprising at least one pumping chamber, and optionally further comprising auxiliary components such as a body, an interface, etc. By means of the pump unit, the liquid is drawn from the reservoir in discrete amounts, i.e. not continuously, and is supplied to the nozzle. The pump unit operates without a propellant and generates pressure mechanically.

[0003] However, the inhalation devices disclosed in the above documents can only be used to nebulize a single type of liquid. In certain circumstances, it is advantageous to be able to nebulize multiple liquids simultaneously.

[0004] US Patent No. 7,819,342 discloses an inhalation device configuration capable of dispensing two liquids simultaneously. The inhalation device housing holds two reservoirs that feed one or two pump mechanisms. The pressurized liquid is either dispensed by two separate nozzle bodies, thus providing two separate doses of atomized liquid. An alternative embodiment discloses an inhalation device with a single nozzle, the nozzle having two ejection channels. The trajectories of the channels intersect, thus providing a common impingement point at which a single dose containing droplets of both liquids is generated. [Prior art documents] [Patent documents]

[0005] [Patent Document 1] European Patent No. 0627230 [Patent Document 2] U.S. Pat. No. 7,819,342 Summary of the Invention [Problem to be solved by the invention]

[0006] However, the nozzles described above cannot atomize more than two liquids at a time. Also, it is not possible to use known nozzles using one impingement point to deliver medically active liquids containing active ingredients that, due to their high dose or low (e.g. aqueous) solubility, require a relatively large amount of liquid to be aerosolized per dose. Also, the nozzle structure requires a significant amount of space, which is not always available.

[0007] The present invention aims to provide a nozzle that avoids the drawbacks of the known technology, or to provide a medical aerosol generator that includes such a nozzle, in particular a nozzle that is capable of atomizing three or more liquids at once and that consumes less space than known solutions. [Means for solving the problem]

[0008] This object is solved by a medical aerosol generator or inhalation device which comprises a nozzle according to claim 1. Advantageous embodiments are set out in the dependent claims, the subsequent description and the accompanying drawings.

[0009] In particular, the present invention provides an aerosol generator for medically active liquids configured and adapted for the generation of an inhalable mist, vapor or spray, comprising: a) a housing; b) a reservoir within the housing for holding a medically active liquid; c) a pump unit; d) a nozzle (1); Equipped with The nozzle (1) has a main axis (Z) and at least three ejection channels (1A, 1B, 1C, 1D) adapted to eject liquids (F, F1, F2) along respective ejection trajectories, and is provided with at least two impingement points (X1, X2) at which at least two of said ejection trajectories intersect each other, and further All the exit angles (A, A1, A2) at which the individual trajectories exit the nozzle (1) are the same, or At least one of the ejection angles (A, A1, A2) is different from the other ejection angles (A, A1, A2); The present invention relates to an aerosol generator.

[0010] In a preferred embodiment of the invention, the aerosol generator further comprises an applicator piece, preferably for oral use, hi another preferred embodiment, said applicator piece is a mouthpiece.

[0011] In a further preferred embodiment of the invention, the aerosol generator or inhalation device is a handheld device.

[0012] We begin with some definitions of terms used throughout the description and claims. The definitions should be used to determine the meaning of each expression, unless the context requires otherwise.

[0013] A "medical aerosol generator", "inhaler" or "inhalation device" is a device configured and adapted to generate an inhalable mist, vapor, or spray. In the context of the present invention, the terms "medical aerosol generator", "aerosol generator", "inhaler" and "inhalation device" are used interchangeably. In this context, "inhalable" refers to the characteristics, including particle size, of the aerosol, mist, vapor, or spray being such that it is suitable for administration by inhalation to a subject, such as a human subject. Inhalable is sometimes also referred to as respirable.

[0014] "Atomization" and "nebulization" in the context of inhalers refer to the production of fine, inhalable droplets of a liquid. Typical sizes of atomized droplets are in the range of a few microns.

[0015] An "aerosol" is a dispersion of a solid or liquid phase in a gas phase. The dispersed phase, also called the discontinuous phase, is composed of a plurality of solid or liquid particles. The aerosol produced by the inhalation device of the present invention is a dispersion of a liquid phase in the form of inhalable droplets in a gas phase, typically air. The dispersed liquid phase may optionally contain solid particles dispersed in the liquid.

[0016] A "liquid" is a fluid material that can change its shape to that of the container holding the liquid, but maintains a nearly constant volume regardless of pressure. A liquid may refer to a single-phase solution or a dispersion of a continuous liquid phase and a dispersed phase that may or may not be liquid.

[0017] A liquid is "medically active" if it represents or contains a biologically active or medically active compound or material that is useful for a medical purpose in its application.

[0018] "Plurality" means two or more.

[0019] A "nozzle" is a unit that serves to atomize / atomize a liquid. Generally, the term refers to the whole unit. However, a nozzle may contain one or more sets of separate, identical, or different subunits. A nozzle may be equipped with multiple ejection channels for ejecting liquid.

[0020] The "major axis" of a nozzle is the central axis of the nozzle that is parallel to or collinear with the direction along which the majority of the emitted aerosol travels after exiting the nozzle.

[0021] A "horizontal" plane is a plane perpendicular to the major axis.

[0022] The "ejection trajectory" is an imaginary relatively straight line starting from the end of the ejection channel. The ejection trajectory resembles the initial travel path of the liquid ejected from the ejection channel when the suction device is activated. It is clear that the nozzle (and the entire suction device) must be adapted and configured with a suitable channel shape and a sufficiently high pressure, for example, so that the ejected liquid can be provided in a sharp stream in the above-mentioned straight line.

[0023] When two or more ejection trajectories intersect, a "collision point" is formed.

[0024] The "impact angle" is the angle between the ejection trajectory at the impact point and the main axis. The "ejection angle" is defined as 90 degrees minus the angle between the ejection trajectory and a line that is parallel to the main axis and intersects the ejection trajectory (the "middle angle I"). If the impact point is on the main axis, the parallel line is the main axis itself, and the middle angle is the impact angle. If the impact point is not on the main axis, the parallel line is offset from the main axis. This "ejection offset" is the distance between the main axis and the impact point measured in a plane perpendicular to the main axis. The ejection angle can also be understood as the angle between the ejection trajectory and a line perpendicular to the main axis that connects the outlet opening of the ejection channel to the main axis when the respective impact point is on the main axis, and can also be understood as the angle between the ejection trajectory and a line perpendicular to the main axis that connects the outlet opening of the ejection channel to a line parallel to the main axis that intersects the ejection trajectory when the respective impact point is not on the main axis.

[0025] The terms "upstream" and "downstream" refer to the side of a first component on which a second component is (fluidically) disposed, with respect to a normal flow direction starting at the reservoir, through the pump unit, and continuing through the inlet opening, the ejection channel, and the outlet opening of the nozzle. "Upstream" of a first component means that the second component is fluidically disposed before or in front of this first component, and "downstream" of a first component means that the second component is fluidically disposed after or behind the first component.

[0026] Further definitions will be provided in the ensuing discussion.

[0027] The present invention particularly relates to an inhalation device with a nozzle. In some embodiments of the present invention, the inhalation device is a handheld device. In a particular embodiment, the present invention relates to a nozzle for a handheld medical aerosol generator.

[0028] The nozzle according to the invention is useful in an inhalation device for producing aerosols, in particular inhalable aerosols, of medically active liquids.

[0029] The nozzle has a main axis and at least three, preferably four, ejection channels adapted to eject liquid along respective ejection trajectories, and at least two impingement points are provided where at least two of the ejection trajectories intersect each other.

[0030] The main axis is parallel or collinear with the direction in which the aerosol generated from the liquid leaves the inhalation device towards the user. The main axis may also be the axis of rotation of the nozzle body.

[0031] Each ejection channel has its own ejection trajectory, i.e. the direction in which the respective ejected liquid stream leaves the channel. Essentially, the trajectory is relatively straight, at least initially, or from the exit opening of each ejection channel to the corresponding impingement point. It is clear that the part of said channel further away from the exit opening (i.e. inside the nozzle body or nozzle bulk) can follow a direction different from said ejection trajectory. It is also clear that the liquid further away from the nozzle surface deviates from said straight line, due to the increasingly reduced momentum and the stronger influence of air resistance and gravity. The latter direction is primarily dictated by the direction of the channel exactly at the respective exit opening. However, the latter direction can also be influenced by the exact shape of the exit opening and, optionally, deflectors etc., placed just behind the exit opening, capable of redirecting the ejected fluid.

[0032] At least two of the trajectories intersect at at least one of the collision points, thereby achieving collision-type (or collision-based) aerosol formation. According to the present invention, since at least a third ejection channel is present, the channel can also be directed toward the collision point, resulting in a larger amount of liquid being atomized. However, in this case, an additional channel must be present so that a second collision point is formed, or the third channel can be directed away from the collision point, for example against a baffle, so that a second collision point is also formed.

[0033] According to one embodiment, each jet trajectory preferably intersects with at least one other jet trajectory, meaning that no jet trajectory does not intersect with other jet trajectories, and every jet trajectory collides with at least one other jet trajectory. In the case of four channels, there are two collision points.

[0034] According to one embodiment, all of the ejection angles at which the individual trajectories exit the nozzle are identical with respect to the main axis, and typically with respect to the front face of the nozzle (if it is essentially flat and perpendicular to the main axis). If the ejection trajectories are in a common plane, i.e., in a two-dimensional setting, by using identical angles, multiple impingement points can be provided.

[0035] According to another embodiment, still with respect to the main axis of the nozzle, in a setting where the lateral distance between the main axis and the channel outlet openings is the same, at least one of the above-mentioned ejection angles, preferably at least two, is different from the other ejection angles so as to provide different impingement points. Using the example of a truncated cone, by using four ejection channels, a nozzle can be provided with two impingement points, one or both of which are offset laterally from the imaginary tip of the truncated cone, with a first pair of channels providing a first impingement point and a second pair of channels providing a second impingement point. In this case, not all ejection angles are the same with respect to the main axis (e.g. of the truncated cone). Optionally, each of the two ejection trajectories corresponding to the first pair of channels exhibits a first ejection angle, and each of the two ejection trajectories corresponding to the second pair of channels exhibits a second ejection angle, the first ejection angle being different from the second ejection angle. If the outlet openings of all channels are arranged symmetrically around the main axis (at the same lateral distance to the main axis), such a configuration will have two collision points, namely a first collision point with the main axis at the intersection of the two trajectories corresponding to the first pair of channels, and a second collision point with the main axis at the intersection of the trajectories corresponding to the second pair of channels.

[0036] In a two-dimensional configuration, the channels are preferably symmetrically arranged such that there is a plane in which the main axis lies ("vertical") dividing the nozzle into two substantially mirroring halves. For each trajectory, the impact angle, which is the angle between the ejection trajectory at the impact point and the main axis, is preferably in the range of 15° (acute) to 75° (obtuse), more preferably in the range of 30° to 60°, with an angle of about 45° also being considered particularly preferred.

[0037] In one embodiment, at least two impingement points are provided, each impingement point being formed by at least two ejection trajectories having the same ejection angle, such that two ejection channels have a first ejection angle and the other two ejection channels have a second ejection angle different from the first ejection angle.

[0038] One advantage of an embodiment with an impingement point fed by more than two ejection channels is that a larger volume of liquid can be sprayed for this particular impingement point without the need to enlarge the cross section of the individual ejection channels, and therefore the fluid parameters of each channel can remain the same by simply adding additional channels.

[0039] A general advantage of multiple impact points is that they potentially reduce the risk of large droplet formation, especially when larger volumes of liquid are nebulized, since in certain circumstances too high a liquid concentration at one point (= impact point) can promote the formation of undesirable large droplets. By splitting one large impact point into two (or more) smaller impact points, the amount of liquid required to nebulize at each impact point is significantly less. In this context, large droplets refer to droplets that cannot be inhaled or do not reach the lungs due to their large size.

[0040] The inhalation device of the present invention is therefore particularly useful for delivering medically active liquids containing active ingredients that, due to their high dosage or low (e.g., aqueous) solubility, require aerosolization of relatively large amounts of liquid per single dose and cannot be delivered by currently known inhalation devices based on aerosolization by impaction using a single impaction point.

[0041] Also, since there are multiple impingement points, each of these can be fed with a liquid flow of a different individual liquid between the impingement points, so that no mixing of the liquids occurs until the atomization stage is complete, which may be advantageous for certain liquids that should not come into contact with each other.

[0042] In this regard, the inhalation device of the present invention addresses the need to simultaneously deliver, in aerosolized form, two or more active ingredients that are not readily compatible chemically and / or physically.

[0043] All ejection channels are integrated into one nozzle body, reducing the space required, and this structure also makes it easy to provide more than two impingement points that can connect to two or more liquid reservoirs, allowing the nozzle to spray more than two liquids if required.

[0044] According to another embodiment, at least two or all of the impingement points are arranged along the main axis of the nozzle in the same vertical plane, i.e. perpendicular to the main axis. This means that the distance between each impingement point and the front face of the nozzle is essentially the same. This is advantageous if the individual atomized liquids (sprays, mists) are approximately the same size and are inhaled in similar amounts.

[0045] In another embodiment, at least two or all of the impingement points lie in different vertical planes along the major axis of the nozzle, meaning that at least two of the impingement points are at different distances relative to the front face of the nozzle.

[0046] For example, if two impact points are both on the main axis, it is possible to generate a central aerosol stream from the first liquid and a surrounding sheath stream of aerosol from the second liquid. Such core and sheath streams can be advantageously used for inhalation purposes, for example, where one component of the stream (the sheath) is distributed to the trachea and another component (the core of the stream) is distributed to the bronchioles.

[0047] According to another embodiment, with respect to the main axis of the nozzle, all the collision points are located on the main axis (symmetrical arrangement). This means that there are several collision points, but they are located in parallel planes that intersect with the main axis. At the same time, when viewed from the direction of the main axis, only one collision point is visible.

[0048] In another embodiment, at least one collision point is laterally offset from the main axis (asymmetric arrangement). This means that when viewed in the direction of the main axis, multiple collision points are visible, one or all of which are laterally offset from the main axis. The collision points can be located in different planes or in one common plane.

[0049] According to one embodiment, the ejection channels of the nozzle all have the same cross section. Such an embodiment is particularly useful when atomizing several liquids of similar physical parameters and of comparable amounts.

[0050] In another embodiment, at least one of the ejection channels or pairs of ejection channels of the nozzle has a cross section different from another ejection channel or pair of ejection channels, i.e. the cross sections of the individual channels or pairs of channels are different from each other. Such a setup is advantageous when atomizing two or more liquids with different physical parameters and / or in different amounts.

[0051] For all the above embodiments in which multiple impingement points are provided, the preferred total number of impingement points is 2 or 3, in particular 2. Furthermore, the preferred number of ejection channels is 2 per impingement point.

[0052] According to one embodiment, all the ejection channels of a nozzle are fluidly connected (directly or indirectly) to the same liquid reservoir so that all the impingement points can be supplied with the same liquid. This means that only one liquid is atomized by the nozzle, regardless of the number of ejection channels. Furthermore, since the type of liquid is the same for all channels, it is preferable that all the ejection channels have the same dimensions.

[0053] If the inhalation device has multiple pump chambers or pump units, all pump chambers or pump units are connected to the same reservoir or to reservoirs holding the same liquid type.

[0054] If the suction device has only one pump chamber, one or more reservoirs can supply liquid to the pump chamber, which also acts as a mixing chamber before the liquid is delivered to the nozzle.

[0055] According to another embodiment, at least two ejection channels of the nozzle are in fluid connection (directly or indirectly) with separate liquid reservoirs, thus providing at least one impingement point at which a different liquid (i.e. a second liquid, the composition of which differs from the first or aforementioned liquid) can be supplied. Such a configuration thus serves to generate multiple aerosols simultaneously. It is also clear that at least two inlet openings of the nozzle must be connected to respective reservoirs so that at least two different liquids can be atomized.

[0056] It should be noted that even when only one liquid composition is to be nebulized, an inhalation device with multiple reservoirs may be advantageous. The shape of the reservoirs may be standardized. Thus, one inhalation device containing such standardized reservoirs can be used to produce mixtures of individual liquids, as well as "mixtures" of the same liquid resulting from multiple reservoirs. Moreover, the mixing ratio of different liquids can be easily adjusted by simply using the desired number of reservoirs filled with individual liquids. For example, if one liquid contains a medically active agent and another liquid is a solvent or diluent, and the housing holds three reservoirs, the ratio of agent:diluent can be 1:1 (one is a dummy reservoir), 1:2, or 2:1.

[0057] In another embodiment, at least two ejection channels of the nozzle are connected to a common mixing chamber located upstream of the channels and downstream of the respective reservoirs. Here, a separate volume is provided located between the pump chamber and the nozzle, with the purpose of mixing liquids from several (possibly the same) sources before feeding them to the ejection channels.

[0058] According to one embodiment, at least two ejection channels of the nozzle form a pair (or a group in case of three or more compound ejection channels), sharing a common inlet and intersecting trajectories. A pair or group of channels is preferably composed of two (or three or more) channels of identical shape to obtain the most uniform atomization results. A pair or group produces an aerosol at one impact point. Each pair or group has a unique impact point. These different impact points may be located in the same horizontal plane or in different horizontal planes.

[0059] In another embodiment, all the ejection channels of a nozzle have separate inlets. Thus, the ejection channels are not paired, since the pairs are characterized by the same liquid flowing through the channels. However, they may still have ejection trajectories that cross each other, so that multiple impact points are provided.

[0060] According to one embodiment of the nozzle, where two ejection channels are paired, one main supply channel is arranged to connect to the upstream end of the first ejection channel, and there is a cross channel connecting said main supply channel to the upstream end of the second ejection channel. The upstream end of the main supply channel is connected to a liquid reservoir directly or indirectly via a pump unit. Such a structure is preferably realized in a two-dimensional configuration, where all channels are arranged in the same plane.

[0061] The crossover channels may have a perpendicular direction to said main feed channels, thus providing the shortest possible fluid connection. The crossover channels may also follow another path, such as an arched path in a plane perpendicular to the main axis. The crossover channels may also be offset with respect to the plane in which the respective pair of ejection channels lies, but in any case it is clear that a fluid connection must be provided between the crossover channels and the corresponding ejection channels.

[0062] Since the two ejection channels of a pair are arranged on opposite sides of the main axis and a cross channel connects the two ejection channels of the pair, only one (common) main supply channel is sufficient for the pair. Thus, there is only one inlet opening that needs to be coupled to the pump chamber or reservoir. In this way, a space-saving solution is provided in terms of the amount of area required to connect a pair of nozzles to a component arranged upstream.

[0063] In one embodiment of an inhalation device with a nozzle having multiple pairs, such as two pairs, the outlet openings of the first pair of ejection channels are in a rotational position, for example 60° (or another integer factor of 360°), relative to the outlet openings of the second pair of ejection channels, with respect to a main axis that also forms an axis of (rotational) symmetry, and the respective cross channels are spaced apart from each other along said axis of symmetry so as not to cross each other. In other words, the aforementioned cross channel configuration is repeated several times, for example doubly or triply, and is placed apart from each other by rotating the respective units comprising a pair of ejection channels, the corresponding cross channel and the main supply channel around the main axis. If the individual cross channels are located in different planes along the main axis, they do not cross each other. The result is a turret-like arrangement of the inlet openings of the different pairs (and therefore different liquids) on a circular path located at the interface between the nozzle body and the component that supplies the liquid.

[0064] According to another embodiment, the nozzle exhibits a front face and a rear face opposite the front face. The front face, which is the face of the device that faces the user when the device is operated, comprises the outlet openings of the ejection channels. The rear or back face of the nozzle, which faces the interior of the device, is essentially flat and comprises a number of openings that form the entrances to the main feed channels.

[0065] Preferably, the device component that connects to the back of the nozzle provides a corresponding surface with supply openings, so that each supply opening of said device component connects to an inlet opening of the nozzle. In other words, the interface between the nozzle and the component that supplies it, for example the outlet side of the pump chamber, is designed so that a simple flat gasket is sufficient. Such a gasket essentially consists of a flat sheet of elastic material with holes in the appropriate places.

[0066] The advantages of such a structure are that fluid connections can be safely and easily established, and the cost of providing seals and interface surfaces is low.

[0067] In some embodiments, the nozzle is constructed as a stack of relatively flat plates. Such plates can preferably be manufactured by material removal techniques such as etching. Wafers of various materials such as silicon, glass, metal, ceramic or plastic can form the semi-finished product. The channels are introduced into either or both of the two flat sides of the substrate. Several such plates can then be stacked to manufacture a stack of nozzles offering multiple pairs of ejection channels.

[0068] In other embodiments, the nozzle is constructed from a three-dimensional rotationally symmetric basic shape. Such a basic shape can be a (preferably truncated) cone, cylinder, or pyramid. Typically, the axis of rotation or axis of symmetry of the basic shape coincides with the main axis of the finished nozzle.

[0069] Thereafter, advantageous combinations of the above mentioned features are provided, which are based on certain main features, each of which can be advantageously combined with the following additional features, which can be combined with one, several or all of the respective additional features.

[0070] For the sake of brevity, instead of repeating the description of each subsequent feature, reference is made to the above description.

[0071] According to one embodiment, as a main feature, the nozzle has at least two impingement points.

[0072] Advantageous additional features include that at least one of the ejection angles is different from the other ejection angles, and / or that at least two or all of the impingement points are located in different planes, and / or that at least two ejection channels of the nozzle are connected to a common mixing chamber arranged upstream, and / or that the nozzle is constructed as a stack of two-dimensional plates.

[0073] According to another embodiment, as a main feature, the nozzle has at least three ejection channels.

[0074] As an advantageous additional feature, at least one of said exit angles of the nozzle is different from the other exit angles.

[0075] Advantageous additional features include that the nozzle has at least one impingement point offset from the main axis, and / or at least two or all of the impingement points are located on different planes, and / or at least one impingement point is offset from the main axis of the nozzle, and / or the cross-section of at least one ejection channel of the nozzle differs from the cross-section of the other ejection channels, and / or at least two ejection channels of the nozzle are connected to individual liquid reservoirs so as to provide at least one impingement point to which different liquids can be supplied, and / or at least two of the ejection channels of the nozzle are connected to a common mixing chamber arranged upstream, and / or the nozzle is constructed as a stack of two-dimensional plates.

[0076] According to another embodiment, the main feature is that at least two, or even all, of the impingement points of the nozzle are located on different planes.

[0077] As advantageous additional features, all the features already described can be combined with the main features described above.

[0078] According to another embodiment, the main feature is that, with respect to a main axis of the nozzle, at least one impingement point of the nozzle is offset from the main axis.

[0079] Advantageous additional features include that the nozzle has at least two collision points at which at least two of the ejection trajectories intersect each other, and / or at least one of the ejection angles is different from the other ejection angles, and / or at least two or all collision points are located on different planes, and / or the cross-section of at least one ejection channel of the nozzle is different from the cross-section of another ejection channel, and / or the nozzle is constructed from a three-dimensional rotationally symmetric basic shape.

[0080] According to another embodiment, as a main feature, at least one of the ejection channels of the nozzle has a cross section which differs from the cross section of another of the ejection channels.

[0081] Advantageous additional features include that at least one of the ejection angles is different from the other ejection angles, and / or that at least two or all of the impingement points are located in different planes, and / or that at least two ejection channels of the nozzle are connected to a common mixing chamber arranged upstream, and / or that the nozzle is constructed as a stack of two-dimensional plates.

[0082] According to another embodiment, as a main feature, at least two ejection channels of the nozzle are connected to respective liquid reservoirs to provide at least one impingement point to which different liquids can be supplied.

[0083] Advantageous additional features include that at least two collision points are provided at which at least two of the ejection trajectories intersect each other, and / or that at least one of the ejection angles is different from the other ejection angles, and / or that at least two or all collision points are located in different planes, and / or that at least one ejection channel of the nozzle has a cross-section which differs from the cross-section of another ejection channel, and / or that at least two ejection channels of the nozzle are connected to a common mixing chamber which is arranged upstream, and / or that the nozzle is constructed as a stack of two-dimensional plates, and / or that the nozzle is constructed from a three-dimensional rotationally symmetric basic shape.

[0084] According to another embodiment, as a main feature, at least two ejection channels of the nozzle are connected to a common mixing chamber arranged upstream.

[0085] Advantageous additional features include that at least two of the ejection trajectories have at least two collision points that intersect with each other, and / or that at least one of the ejection angles is different from the other ejection angles, and / or that at least two or all collision points are located on different planes, and / or that the cross-section of at least one ejection channel of the nozzle is different from the cross-section of another ejection channel, and / or that the nozzle is constructed from a three-dimensional rotationally symmetric basic shape.

[0086] According to another embodiment, as a main feature, the nozzle is constructed as a stack of two-dimensional plates.

[0087] Advantageous additional features include at least two of the ejection trajectories having at least two collision points that intersect with each other, and / or at least one of the ejection angles is different from the other ejection angles, and / or at least two or all of the collision points are located on different planes, and / or the cross-section of at least one ejection channel of the nozzle is different from the cross-section of another ejection channel.

[0088] According to another embodiment, as a main feature, the nozzle is constructed from a three-dimensional rotationally symmetric basic shape.

[0089] Advantageous additional features include the provision of at least two collision points at which at least two of the ejection trajectories intersect each other, and / or at least one of the ejection angles is different from the other ejection angles, and / or at least two, or all, of the collision points are located on different planes, and / or at least one collision point is offset from the main axis of the nozzle, and / or the cross-section of at least one ejection channel of the nozzle is different from the cross-section of the other ejection channels, and / or at least two ejection channels of the nozzle are connected to respective liquid reservoirs such that at least one collision point is provided at which different liquids can be supplied, and / or at least two ejection channels of the nozzle are connected to a common mixing chamber arranged upstream.

[0090] All combinations of the above main features with one, some or all of each of the additional features result in advantageous embodiments that require little space, can deliver medically active liquids including active ingredients that would require a relatively high volume of liquid to be aerosolized per single dose, and can nebulize two or more liquids.

[0091] All relevant embodiments, options and preferences regarding the nozzle above also apply to an inhalation device, inhaler or aerosol generator comprising the nozzle described above. [Brief description of the drawings]

[0092] [Figure 1] FIG. 1 shows a nozzle according to the prior art. [Diagram 2] FIG. 2 shows details of a nozzle according to the prior art. [Diagram 3] FIG. 2 shows a nozzle according to a first embodiment. [Figure 4] FIG. 4 shows a nozzle according to a second embodiment. [Diagram 5] FIG. 6 is a diagram showing details of a nozzle according to a second embodiment. [Figure 6] FIG. 1 shows a nozzle according to the prior art. [Figure 7] FIG. 11 shows a nozzle according to a third embodiment. [Figure 8] FIG. 11 shows a cross section of a nozzle according to a third embodiment. [Figure 9] FIG. 11 shows a cross section of a nozzle according to a third embodiment. [Figure 10] FIG. 11 shows a cross section of a nozzle according to a third embodiment. [Figure 11] FIG. 13 shows a three-dimensional view of the third embodiment. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0093] In FIG. 1, which represents the prior art, a nozzle is depicted that includes three ejection channels 1A, 1B, 1C. The ejection trajectories (dotted lines) intersect at one common impact point X. This impact point is located in a plane P with a perpendicular direction to the main axis Z (this is the common direction of the plane in which the impact points lie throughout this document, unless otherwise stated). All channels 1A, 1B, 1C are arranged symmetrically and three-dimensionally around the main axis Z. The ejection angles defined here (also plotted in FIG. 2, a detailed view of the nozzle tip, where only the ejection angles A1, A2 are shown) are identical. The line on which the intermediate angle I is measured is the main axis, and therefore the intermediate angle is the impact angle. In this example, all of the individual trajectories are arranged on the surface of a truncated cone. In this example, the surface 1' of the truncated cone is parallel to the base circle (without reference number), so the angles A1, A2 measured at both positions are identical. The channels 1A, 1B, 1C are preferably closed (laterally) with a closure such as a lid (not shown) so that liquid (not shown) can pass through the channels but cannot exit in an undesired (lateral) direction. This can be achieved, for example, by placing a truncated cone inside a cone-shaped cap (not shown) whose walls form the lid of the channel. The channels can be manufactured in the surface of the truncated cone as shown, but can also be manufactured as grooves in the surface of the cap.

[0094] Both types can be combined with each other in that the channels are provided alternating with cones and openings or in that the associated half-channels are provided with cones and openings.

[0095] In FIG. 3, a cross-sectional view of the nozzle 1 is shown, where again, with respect to the main axis Z of the nozzle 1, all the ejection angles A are identical (only one reference A is plotted), and therefore all the intermediate angles are also identical, all of which are measured relative to the main axis Z. However, the ejection channels 1A-1D are in a common cross section (hatching omitted) and are provided with different collision points X1, X2. They are located in different planes P1, P2 perpendicular to the main axis Z, i.e. the collision points X1 and X2 have different distances to the front surface 1' of the nozzle 1. At the same time, all the collision points X1, X2 are on the main axis Z. The ejection channels 1A and 1B form a first pair, and the ejection channels 1C and 1D form a second pair. In this example, the nozzle 1 is built as / from a "two-dimensional" block.

[0096] This embodiment can be used to generate a central flow of an aerosol of a first liquid (not shown) and a surrounding sheath flow of an aerosol of a second liquid.

[0097] In Fig. 4 an embodiment is shown in which the ejection channels 1A-1D are also located on the surface of a truncated cone. In this configuration the ejection angles A1, A1' of the first pair of ejection channels 1A, 1B correspond to the ejection angles A2, A2' of the second pair of ejection channels 1C, 1D. However, in this configuration the ejection offset results in two different impingement points X1 and X2. Fig. 5 is a detail of the tip of the nozzle. Note that the angles A1, A2 in Fig. 4 are the same as in Fig. 5, since the base circle of the cone is parallel to the surface 1' of the truncated cone.

[0098] For example, as can be seen in FIG. 4, the trajectory of channel 1B is tilted slightly from the main axis Z in one direction, i.e., angle A1'', while the trajectory of channel 1D is tilted in the opposite direction, i.e., angle A2''. Also, the angles A1 and A2 (as they are now) are inclined relative to the thin dashed line starting from angle A1''. * and A2 *5. These represent lines starting at the base circle of the cone and ending at its imaginary tip, the channels along the thin dashed lines also have the same angles A1, A2 (and A1', A2', A1'', A2''), but also result in one common collision point. Thus, in this example, two sets of ejection channels 1A, 1B and 1C, 1D are provided, all with the same ejection angles A1, A2, A1', A2' (see FIG. 5), and thus two collision points X1, X2 are provided as in the previous example. As a result of the aforementioned angular arrangement, there is a lateral ejection offset D. In this embodiment, along the main axis Z of the nozzle, all the collision points X1, X2 are located in the same plane (not shown) relative to the front surface 1' of the nozzle 1. At the same time, all the collision points X1, X2 are located with a lateral offset from the main axis Z (lateral ejection offset D).

[0099] Figure 6 shows a prior art nozzle 1 with four ejection channels 1A-1D with ejection trajectories with different ejection angles per pair (similar for A1 and A1', similar for A2 and A2'), where the ejection channels (and trajectories) lie in a common plane (hatched cross section). The nozzle 1 is of the "two-dimensional" block type. The angles A1, A1', A2, A2' are arranged such that all ejection trajectories (dotted lines) intersect at one common impact point X.

[0100] In Figure 7 a transparent top view of another embodiment of the nozzle 1 is shown. For further details please refer to the following description of Figures 8 to 11 relating to the same embodiment.

[0101] In figures 8 and 9 two cross sections AA and BB of the nozzle 1 of figure 7 are shown (hatching omitted) in which the ejection channels 1A, 1B and 1C, 1D are connected to a common dividing chamber 2A, 2B arranged upstream, thus providing a separate chamber or volume arranged between the pump chamber (not shown) and the ejection channels 1A, 1B / 1C, 1D and having the purpose of dividing the liquid supplied to the nozzle (optionally from several sources) before supplying it to the ejection channels 1A, 1B / 1C, 1D.

[0102] In the illustrated embodiment, the two ejection channels 1A and 1B, as well as 1C and 1D of the nozzle 1, respectively, form a pair, one main supply channel 3A, 3B is arranged to connect with the beginning of the first ejection channel 1A, 1C, and there is a cross channel 4A, 4B connecting said main supply channel 3A, 3B to the end of the respective second ejection channel 1A, 1C. The cross channel 4A, 4B, which serves as the dividing chamber 2A, 2B, runs perpendicular to the main supply channel 3A, 3B. There is only one inlet opening 5A, 5B, respectively, which must be coupled to a pump chamber or pump unit (not shown).

[0103] In the depicted embodiment, the pairs of ejection channels that initially overlap with respect to a main axis Z (not shown), which also forms an axis of symmetry, are at a rotational position of, for example, 60° (or another integer factor of 360°) relative to each other, and the respective intersecting channels 4A, 4B are spaced apart from each other along said axis of symmetry so as not to intersect each other.

[0104] In the see-through side view of Figure 10, a cross section containing hidden lines is drawn so that all the axially separated main cross channels (with the third cross channel reference number omitted) are clearly visible. Due to the viewing direction, only two pairs of erupting channels are visible.

[0105] The aforementioned design can also be seen in Fig. 11, which is a three-dimensional perspective view of the nozzle 1 containing the cross sections of Fig. 8 and Fig. 9. By virtually rotating the cross section, a compact and simple nozzle is obtained, whose inlet opening (reference numbers omitted) lies on a circular path (dash-dotted circle). The respective interfaces to components located upstream (i.e. pump chamber, valve section, not shown) can therefore be designed to be relatively simple. [Explanation of symbols]

[0106] 1 nozzle 1' front 1A-1D Eruption Channel 2A, 2B split room 3, 3A, 3B Main supply channel 4, 4A, 4B Cross Channels 5, 5A, 5B Inlet Openings F, F1, F2 Liquids X, X1, X2 Collision Points A, A1, A2 Jet Angles A1 * , A2 * , A1’, A2’, A1’’, A2’’ Angles I Intermediate Angle Z Main Axis D Jet Offset P, P1, P2 Planes

Claims

1. 1. An aerosol generator for a medically active liquid configured and adapted for the generation of an inhalable aerosol, comprising: a) a housing; b) a reservoir within said housing for holding a medically active liquid; c) a pump unit; and d) a nozzle (1); Equipped with said nozzle (1) is constructed as a stack of plates, has a main axis (Z) and at least four ejection channels (1A, 1B, 1C, 1D) adapted to eject liquids (F, F1, F2) along respective ejection trajectories, and is provided with at least two impingement points (X1, X2) at which at least two of said ejection trajectories cross each other; All channels are on the same plane The channels are introduced into either or both of the two flat sides of the plate and are formed by stacking a plurality of plates, said main axis (Z) being disposed in the same plane as said channel and perpendicular to the front face of said nozzle; All of the ejection angles (A, A1, A2) at which each of the ejection trajectories exit the nozzle (1) are the same; An aerosol generator comprising:

2. all said ejection channels (1A, 1B, 1C, 1D) of said nozzle (1) are connected to the same liquid reservoir, so that all impingement points (X, X1, X2) are supplied with the same liquid (F); 2. The aerosol generator of claim 1.

3. at least two of said ejection channels (1A, 1B, 1C, 1D) of said nozzle (1) are connected to separate liquid reservoirs, thereby providing at least one impingement point (X, X1, X2) which can be supplied with different liquids (F1, F2); 2. The aerosol generator of claim 1.

4. At least two of the ejection channels (1A, 1B, 1C, 1D) of the nozzle (1) are connected to a common mixing chamber arranged upstream, The aerosol generator according to any one of claims 1 to 3.

5. At least two of the ejection channels (1A, 1B, 1C, 1D) of said nozzle (1) share a common inlet and have ejection trajectories that cross each other to form pairs or groups of ejection channels (1A, 1B, 1C, 1D), 5. The aerosol generator according to claim 1 .

6. All the ejection channels (1A, 1B, 1C, 1D) of the nozzle (1) have separate inlets, 5. The aerosol generator according to claim 1 .

7. two ejection channels (1A, 1B, 1C, 1D) form a pair, said nozzle further comprising a main supply channel (3, 3A, 3B) arranged to connect the upstream end of the first ejection channel (1A, 1B, 1C, 1D) and a cross channel (4, 4A, 4B) connecting said main supply channel (3, 3A, 3B) to the upstream end of the second ejection channel (1A, 1B, 1C, 1D), An aerosol generator according to any one of claims 1 to 6.

8. 8. The aerosol generator of any one of claims 1 to 7, which is a handheld device.

9. 9. The aerosol generator of claim 1, further comprising an applicator piece for oral use.

10. 10. The aerosol generator of claim 9, wherein the applicator piece is a mouthpiece.

Images