The present invention relates to a spray nozzle for liquid, in particular for coating liquid under high pressure. Furthermore, the invention relates to a device for spraying liquid, in particular for coating liquid under high pressure, comprising such a nozzle.
A device for spraying liquid or sprayer, either of the manual type or of the automatic type, generally comprises a spray nozzle, sometimes several, which is(are) mounted at the downstream end of the sprayer. The terms “upstream” and “downstream” herein refer to the direction of flow of the liquid in the sprayer. The term “upstream” denotes elements located on the side of the sprayer where the liquid to be sprayed arrives from a supply source. The term “downstream” denotes elements located on the side of the sprayer where the liquid is sprayed in droplets.
Such a sprayer may, for example, be intended for spraying coating liquids such as waterborne or solvent-based paints. To produce the spraying of the liquid in droplets, the sprayer is connected, by means of one of more tube(s), to a pump designed to put the liquid under high pressure, for example 70 bars. The spraying is carried out at the downstream end of the nozzle, which has a geometry determined depending on the desired shape for the jet of droplets of the sprayed liquid.
To the aim of shaping the jet of sprayed liquid into a “fan”, usually called a “flat” spray, a nozzle such as that illustrated by
In nozzles of the prior art, the dome 5 has the shape of an ogive or triangular arch or a hemispherical shape, the length of which approximately equals the diameter of the channel 4. As
When the nozzle 1 sprays a liquid under high pressure, for example 70 bars, the geometry of the orifice 7 shapes the jet into a cone with an elliptical cross section. With the nozzle 1, the flow rate of the sprayed liquid is not uniformly distributed in this elliptical cross section. On the contrary, it has higher concentrations towards the distant edges of the ellipse. In the field of spraying coating liquids, this type of distribution of liquid is called the “tails effect”. It has been observed that the more rounded the edges of the ellipse are, the larger are the “tails” in the flow of liquid.
The “tails effect” has the drawback of leading to asymmetric wear of the nozzle 1, by overwearing down the edges of the orifice 7. The more abrasive the sprayed liquid is, the greater this wear is. This wear increases the “tails effect” and therefore leads to a reduction in the quality of the spraying. In addition, it reduces the service life of the nozzle 1, even when the material of the body 2 has a high hardness.
GB-A-1 312 052 describes a flat spray nozzle comprising a discontinuity at the junction between the channel and the dome connecting the channel and the slot of the nozzle. However, the nozzle of GB-A-1 312 052 does not permit to significantly decrease the “tails effect” so as to get a sufficient spraying quality.
The present invention aims in particular to solve these drawbacks by proposing a spray nozzle with a longer service life and enabling a flat jet to be produced with a relatively uniform distribution of liquid, and therefore to improve the spraying quality.
To this aim, the subject-matter of the invention is a spray nozzle for liquid, in particular for coating liquid under high pressure, comprising:
Said dome has a plane cross section that is symmetric relative to said longitudinal axis. Said plane cross section is defined by at least two circle arcs which extend between a downstream end portion of said channel and said longitudinal axis and which have different radii and centers located on the side of said channel.
According to other advantageous, but optional, features of the invention, taken in isolation or in any technically feasible combination:
Furthermore, the subject-matter of the invention is a device for spraying liquid, in particular coating liquid under high pressure, characterized in that it comprises a nozzle such as disclosed above.
The invention will be well understood, and its advantages will become apparent, in the light of the following description, provided only by way of non limiting example and with reference to the annexed drawings, in which:
As
The chamber 103 and the channel 104 extend along a longitudinal axis X101-X′101 of the nozzle 101. In the example of
The nozzle 101 furthermore comprises a dome 105 connecting the channel 104 and the slot 106. “Dome” denotes the one-eyed base of the channel 104, which is obtained in the body 102 before milling the slot 106. “Connecting” means bringing into fluid communication.
The length L105 of the dome 105, measured parallel to the longitudinal axis X101-X′101, here represents 25% of the diameter D104 of the channel 104. In practice, the length L105 of the dome 105 represents less than 50%, preferably between 20% and 45%, of the diameter D104 of the channel 104. In other words, the dome 105 has a short or flattened shape in relation to the dome 5 of the nozzle 1 of the prior art illustrated in
The tubular channel of the nozzle subject-matter of the invention may, as a variant, be prismatic in shape or be in a cylindrical shape with a non-circular base, for example an elliptical base. In this case too, the length of the dome is less than 50%, preferably between 20% and 45%, of the largest transverse dimension of the channel, measured in a plane orthogonal to the longitudinal axis of the nozzle.
The dome 105 has rotational symmetry around the axis X101-X′101. A cross section of the dome 105 through a plane containing the axis X101-X′101, for example through the plane P106, is defined by two circle arcs C1051 and C1052 that extend between a downstream end portion 1041 of the channel 104 and the axis X101-X′101. The circle arcs C1051 and C1052 have the respective radii R1051 and R1052 and respective centres O1051 and O1052 located on the side of the channel 104, i.e. opposite the downstream portion of slot 106.
On the right-hand part of
In addition, the circle arc C1051 is tangent to the end portion 1041 of the channel 104 and the circle arc C1052 is tangent to the circle arc C1051. Thus the arcs C1051 and C1052 are joined in a continuous manner and without any singularity. By symmetry, the geometry of the arcs C′1051 and C′1052 is identical to that of the arcs C1051 and C1052. The dome 105 thus has a shape that is overall trapezoidal or a shape of half a convex lens.
The shape of the dome 105 may be comprised of more than two circle arcs joined to each other. In such a case, the radius of the circle arc closest to the downstream end portion of the channel is less than half the largest transverse dimension of the channel, the radius of the circle arc furthest from the downstream end portion of the channel is greater than half the largest transverse dimension of the channel; and each other circle arc has a radius of a size greater than the radius of the preceding circle arc and less than the radius of the following circle arc. In addition, in such a case, each circle arc is tangent to the preceding circle arc.
In the example of
The channel 104 has a length L104, measured along the axis X101-X′101, of around 1.1 mm. In practice, the length L104 may be between 0.4 mm and 3.5 mm. Moreover, the diameter D104 of the channel 104 has a value of around 0.55 mm and may in practice be between 0.1 mm and 1.8 mm.
As
The geometry and the dimensions of the nozzle 101, in particular of its flattened dome 105, define the approximately rectangular shape of the outlet orifice 107. Such a nozzle enables to considerably reduce the “tails effect”, hence to render the liquid flow rate more uniform in the jet sprayed under, for example, 70 bars, or even under lower pressure, for example 40 bars. To the extent that this sprayed jet is more uniform, the quality of the spraying, hence of the application of this jet for example the coating of an object, is significantly improved. In addition, as the “tails effect” is reduced, the wearing of the edges of the outlet orifice 107 of a nozzle 101 according to the invention is greatly reduced, thereby increasing the service life of the nozzle 101.
The description of
One thus defines a nozzle 201, a longitudinal axis X201-X′201, a body 202, a channel 204 with a diameter D204 and a radius R204, a dome 205 with a length L205, a slot 206 with an outlet orifice 207, circle arcs C2051 and C2052 with respective radii R2051 and R2052 and respective centers O2051 and O2052 and a downstream end portion 2041.
The nozzle 201 differs from the nozzle 101, because the plane cross section of the dome 205 is defined by three circle arcs C2051, C2052 and C2053, instead of two for the dome 105. Alike the plane cross section of
The radius R2053 is greater than the radius R2052, the latter being itself greater than the radius R2051. Furthermore, the radius R2051 is less than the radius R204 of the channel 204 and the radius R2053 is greater than the radius R204.
The geometry and the dimensions of the nozzle 201, in particular of its dome 205, permit to further decrease the “tails effect”, hence to render more uniform the liquid flow rate in the sprayed jet, with respect to nozzle 101.
To the aim of further increasing the service life of the nozzle 101, the latter may be made of a material having a high hardness, which may be selected from the group comprising the tungsten carbides and the ceramics or any other material having a high hardness. A high hardness means a hardness greater than 50 on the Rockwell C scale.
Number | Date | Country | Kind |
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08 51673 | Mar 2008 | FR | national |