The present invention relates to a device for measuring the flow rate of a fluid, and in particular of a liquid, in a conduit, usable, for example, in the field of devices for household washing appliances, such as dishwashers and washing machines, and/or in the field of components for equipment for the production of foods, in particular, drinks.
More specifically, the invention relates to a device for measuring flow rate of the type comprising
A flow measuring device of this type is described for example in European patent application EP 0 599 341 A2. In the solution described in that document, the impeller has a plurality of helical vanes and the associated diffuser also comprises a plurality of helical vanes, which are oriented in the opposite direction with respect to the vanes of the impeller.
The construction of impellers and diffusers provided with such helical vanes is relatively complex and expensive.
One object of the present invention is to provide a measuring device of the flow rate of a fluid and in particular a liquid, which has a simple structure that may be constructed in an easy and economical way and with a precise and reliable operation.
This and other objects are achieved according to the present invention with a flow measuring device of the above-defined type, characterized in that the impeller has
Further features and advantages of the invention will become apparent from the detailed description that follows, provided by way of non-limiting example with reference to the accompanying drawings, in which:
The drawings indicate collectively at 1 a measuring device of the flow rate of a fluid, in particular a liquid, according to the present invention.
In
In the embodiment illustrated in
Between the spokes 5 of the support element 3, passages 8 are defined for the flow of liquid directed toward the electric valve EV. The lateral surfaces 5a parallel to the axis of the conduit C allow to straighten/linearize the output flow from the flow measuring device 1.
The flow measuring device 1 also comprises an impeller indicated collectively at 10 in
In the embodiment according to
In a first axial portion 10a of the impeller 10 from the hub 11 a plurality of substantially flat vanes 13 extend radially, lying in planes passing through the axis of rotation X-X of the impeller 10 (
As will become clearer from the following, the vanes 13 of the impeller 10 are intended to be hit in operation by flows or jets of liquid flowing in the conduit C, in a manner such that said impeller 10 rotates with an angular velocity that is a function of the flow of liquid which passes through the conduit C.
As may be seen in
It is moreover possible to make the impeller also of a single piece of plastic material.
In a manner known per se, at least one permanent magnet 16 is mounted or incorporated in a second axial portion 10b of the impeller 10 (
To the impeller 10 is also associated a magnetic field detector device 17 (
As an alternative to the solution described above, the detection of the angular speed of the impeller 10 may be implemented by other means known per se, for example, by optical means.
With reference in particular to
The end appendixes 18 of the impeller 10 have respective flat surfaces 18a that extend in a plane essentially orthogonal to the axis of the impeller 10 and which are connected to the corresponding radial surfaces 18b (see in particular
The surfaces 18a and 18b form steps which extend circumferentially in the same direction, each from one flat radial vane 13 of the impeller towards the next flat radial vane 13.
As seen in
The function of the end appendixes or projections 18 of the impeller 10 will be described below.
The flow measuring device 1 also comprises a diffuser indicated collectively at 20.
In the embodiment according to
As best seen in
On the side facing the impeller 10, the body of the diffuser 20 defines a central recess, indicated at 20b in
In the central part of the internal transverse wall 20c of the diffuser 20 a recess 20f is made, which extends into the axial end 10c of the impeller 10 facing the entrance of the conduit C (
Appropriately, from the bottom transverse wall of the notch 20f of the diffuser 20 a protrusion 20g with a tapered shape extends toward the impeller 10 for example in the form of a spherical sector, which extends a short distance from the end 10c of said impeller 10, as seen in
The grooves 21 of the diffuser 20 combine to define, as will appear more clearly from the following, a corresponding plurality of passages adapted to place in communication the region upstream of such diffuser with the downstream region, in which is located the impeller 10, and appropriately direct the liquid flow at least partially towards the first axial portion 10a of the impeller 10 and in particular toward the flat radial vanes 13. In particular, each longitudinal groove 21 defines an inlet portion of the respective passage, which is delimited between a radially outer solid surface 21a formed on the conduit C and a radially inner solid surface 21b formed on the diffuser 20.
In the illustrated embodiment, the grooves 21 of the diffuser 20 extend in respective planes parallel to the axis X-X of rotation of the impeller 10, which also represents the longitudinal axis of such diffuser 20. In particular, the grooves 21 extend in respective planes that are inclined in the same direction around said axis X-X (see
As seen in
As may be seen in particular in
As seen for example in
By effect of the presence of the diffuser 20, the flow of liquid, which in operation enters the conduit C, is divided into a plurality of reduced flows, which propagate axially in the grooves 21 and tangentially in the transverse passages 22 of such diffuser.
The transverse passages 22 therefore emit nearly tangential flows or jets that at least partially hit the flat radial vanes 13 of the portion 10a of the impeller 10, as may be appreciated by observing in particular
The total liquid flow that hits the impeller 10 passes over the latter, through the gaps defined between consecutive pairs of vanes 13 and propagates finally through the openings 8 of the support device 3 (
The end appendixes 18 of the second axial portion 10b of the impeller 10 confer overall to the vanes of the same a configuration essentially in the form of an L, which allows the risks of cavitation to be reduced and the turbulence to be mitigated.
In the variant according to
Between the L-shaped notches 31 in the body wall 30, longitudinal grooves 21 are made, functionally similar to the grooves 21 of the diffuser according to the embodiment of
The body 30, on the side facing the impeller 10, has a thickening 30a (
The grooves 21 are connected with corresponding transverse passages 22, similar to the analogous transverse passages 22 of the diffuser according to
Also in the embodiment according to
In the embodiment according to
The plug-like closing body 32 has a reduced axial extension compared to the body 30 and abuts the thickened portion 30a of this body.
In this embodiment, the body 30 and the plug-like closing body 32 of the diffuser 20 combine to define the passages for the flow of fluid.
In particular, each longitudinal groove 21 defines an inlet portion of the respective passage, which is delimited between a radially outer solid surface 21a formed on the body 30 of the diffuser 20 and a radially inner solid surface 21b formed on the plug-like closing body 32 of the diffuser 20.
Each transverse passage 22 is delimited on the radially outer side from the radially outer solid surface 21a formed on the body 30, and in the axial direction between opposing solid surfaces formed on the body 30 and on the plug-like closing body 32 of the diffuser 20.
In the lower side of the plug-like closing body 32 (
For the rest, the embodiment according to
In relation to the version according to
Naturally, without altering the principle of the invention, the embodiments and the details of construction may vary widely with respect to those described and illustrated purely by way of non-limiting example, without thereby departing from the scope of the invention as defined in the appended claims.
Number | Date | Country | Kind |
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102016000012017 | Feb 2016 | IT | national |
Filing Document | Filing Date | Country | Kind |
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PCT/IB2017/050559 | 2/2/2017 | WO | 00 |