This invention relates to a method for manufacturing centrifugal fan impellers.
In particular, this invention relates to a method for forming impellers whose blades are inclined relative to its axis of rotation.
The impellers made with the method according to the invention can be used in fans suitable for several different applications, for example, for moving air through a heat exchanger in a motor vehicle heating system. The invention can also be applied to the manufacturing of impellers for fans for home air conditioning or heating installations.
Fan impellers with inclined blades are described in document EP 0 816 687 and also in document WO 2004/015275, the latter being in the name of the same Applicant as the present application.
Impellers of this kind are used to an increasing extent because they can meet many different requirements, including: low noise; good noise spectrum distribution; high efficiency; dimensional compactness; good pressure head and capacity.
Document EP-0 816 687 discloses a centrifugal fan having an impeller with inclined blades and a method for manufacturing the impeller.
The method described is slow because it involves making individual modules and then putting the modules together.
These characteristics of the production process constitute a serious drawback in the series production of the impellers.
The aim of this invention is to overcome this drawback by providing a method for forming centrifugal fan impellers that is effective and practical and easy to implement.
The technical characteristics of the invention, with reference to the above aim may be clearly inferred from the contents of the appended claims, especially claim 1, and any of the claims that depend, either directly or indirectly, on claim 1.
This invention also relates to an apparatus for manufacturing centrifugal fan impellers.
The apparatus according to the invention is described in claim 13 and in any of the claims that depend on it.
The advantages of the invention will become more apparent from the following detailed description provided by way of example with reference to the accompanying drawings which illustrate a preferred, non-restricting embodiment of the invention and in which:
FIGS. 2 to 6 are schematic perspective views of the apparatus according to the invention in a succession of different operating steps;
With reference to
In particular, but without limiting the scope of the invention, the impeller 1 comprises a rotation axis A and two modules 2 placed side by side lengthways along the axis A. Each module 2 comprises a plurality of blades 3 extending between a mounting disc 4 and a connecting ring 5.
The blades 3 are connected to the disc 4 and to the ring 5 at an angle α relative to the axis A of the impeller 1.
The angle α may advantageously be any angle between 5 and 30 (sexagesimal) degrees and is preferably 10 degrees.
In FIGS. 2 to 6, the reference numeral 6 denotes an apparatus for forming impellers 1.
The apparatus 6 extends lengthways along a first straight line D1 parallel with the impeller axis A during the formation of the impeller 1 itself in the apparatus 6.
The apparatus 6 comprises a main body 7 having, at its opposite longitudinal ends, a first bed 8 and a first platform 9.
As clearly illustrated in
The half-moulds 11, 12 are slidably engaged with respective guides 13 made on the table 10 so that they can slide on the table 10 along a line D2 at right angles to the first line D1.
The half-moulds 11, 12 are mobile relative to each other along the line D2 between a first position, shown in
As illustrated in
Each of the pins 14 passes through a respective slot 16 made in the table 10, shown in
Beside the table 10 on the line D1 in the direction of the arrow F1, the apparatus 6 comprises a second platform 17 and a second bed 18, positioned one after the other.
As clearly illustrated in
As illustrated in
Each forming element 21, 22 comprises a cylindrical head 21a, 22a and a portion 21b, 22b, also cylindrical in shape, that supports the head 21a, 22a.
Each cylindrical head 21a, 22a has a plurality of grooves 23 made all the way around it on its lateral surface.
The grooves 23, advantageously made by electron discharge machining, are designed to form the impeller 1 blades 3 by having the forming material in the fluid state injected into them.
As shown in
Advantageously, the protrusions 25 extend in helical fashion around the axis A.
The table 10 and the second platform 17 have respective cylindrical compartments 26 made in them—only the one in the table 10 being shown in
Each cylindrical compartment 26 is designed to accommodate a cylindrical member 24, with the protrusions 25 sliding into the cavities 27.
With reference to
The first guide profile 28 comprises a double protuberance 28a.
The first platform 9 has pivoted to it a slide 29 that extends lengthways along the line D1 in the direction indicated by the arrow F1 and is equipped with pins 29a that slidably engage the first guide profile 28.
As illustrated in
The second bed 18 has a first profile 28 also on its lower face, which is partially visible in
The main body 7 of the apparatus 6 further comprises a first plate 30 and a second plate 31 which are slidably engaged with a plurality of rods 32 connecting the first bed 8 to the first platform 9.
Four rods 33 and an extractor 34 are rigidly connected to the first plate 30 and move as one with the latter along the line D1.
The rods 33 go through respective through holes 35a, 35b made in the first platform 9 and in the table 10, respectively.
A plurality of unidirectional tie rods 36 connect the first plate 30 to the second plate 31.
A plurality of rods 37 connect the second plate 31 to the table 10 while keeping the distance between them fixed.
Looking in more detail, the tie rods 36 do not prevent the two plates 30, 31 from moving towards each other and enable the first plate 30 to move the second plate 31.
The rods 37 enable the second plate 31 to push the table 10 in the direction indicated by the arrow F1 and to pull it in the direction indicated by the arrow F2.
As shown in
As illustrated in
The second guide profile 38 comprises a double protuberance 38a.
The first plate 30 has pivoted to it a sheet 39 that extends lengthways along the line D1 in the direction indicated by the arrow F1 and is equipped with pins 39a that slidably engage the second guide profile 38.
As illustrated in
In use, with reference to
The plastic substance in a fluid state is injected into a forming volume defined by the two forming elements 21, 22 and by the two half-moulds 11, 12.
The two half-moulds 11, 12 together define a mould 40.
The injection step is followed by a cooling step in which the apparatus 6 is kept in the configuration illustrated in
After cooling, the impeller 1 is substantially formed in the two half-moulds 11, 12.
Starting from the configuration illustrated in
In particular, the second bed 18 is separated from the second platform 17.
As stated above, the forming element 22, shown in
The member 24 is inserted into the aforementioned compartment 26, made on the second platform 17 and on whose inside surface the aforementioned respective cavities 27, are made.
The cavities 27 are oriented in the direction of a winding helix and accommodate the protrusions 25 present on the outside surface of the cylindrical member 24.
The member 24, and hence also the forming element 22 integral with it, is free to rotate about the axis A relative to the second bed 18.
With reference to
The step of extracting the first of the forming elements 21, 22 is thus performed in the manner just described.
As described above, the forming element 22 is extracted from the mould 40 and from the formed impeller 1 by a roto-translational movement about and along the axis A of the impeller 1 itself.
More specifically, with reference to the forming element 22, this roto-translational movement consists of a rotational movement about the axis A and a translational movement along the line D1 in the direction indicated by the arrow F1.
With reference to
The second platform 17 remains attached to the second bed 18 whilst the rest of the apparatus 6 continues advancing in the direction of the arrow F2.
Thus, the assembly consisting of the second platform 17 and the second bed 18 is separated from the rest of the forming apparatus 6.
As illustrated in
As illustrated in
The first plate 30 is attached to the second plate 31 by the sheet 39 and thus, as it advances, the first plate 30 pushes the second plate 31 in the direction of the arrow F1; the second plate 31, through the rods 37, is attached to the table 10 which is thus moved away from the first platform 9 which remains in a fixed position.
The two half-moulds 11, 12 are moved apart by the action of the two diverging pins 14, and the forming element 21, thanks to the winding motion of the protrusions 25 in the helical cavities 27 made in the compartment 26, is unscrewed from the plastic blades 3 formed by injection of the plastic material into the half-moulds 11, 12 and constituting a second module 2 of the impeller 1.
The diverging pins 14, together with the respective holes 15 made in the half-moulds 11, 12 and with movement means that are not illustrated, constitute respective means 41 for actuating the half-moulds 11, 12.
The protrusions 25, together with the cylindrical compartments 26 in which the cavities 27 are made and with movement that are not illustrated, constitute respective means 42 for extracting the forming elements 11, 12.
The step of extracting the second of the forming elements 21, 22 and the step of opening the mould 40 are thus performed in the manner just described.
As described above, the forming element 21 is extracted from the mould 40 and from the formed impeller 1 by a roto-translational movement about and along the axis A of the impeller 1 itself.
More specifically, with reference to the forming element 21, this roto-translational movement consists of a rotational movement about the axis A and a translational movement along the line D1 in the direction indicated by the arrow F2.
As the sheet 39 is pushed by the first plate 30 in the direction of the arrow F2, the pins 39a on it engage the protuberance 38a of the second guide profile 38, thus disengaging the plates 30 and 31.
As illustrated in
The first plate 30 stops when it meets the second plate 31.
Advantageously, therefore, the forming method according to the invention can be used to form the impeller 1 integrally, without having to form the modules 2 individually and put them together at a later stage.
The term “integrally” referred to forming in this context means that the impeller 1 is formed directly as a single block.
In the embodiment of the invention illustrated herein, the impeller 1 blades 3 of one module 2 are inclined relative to the axis A in the direction opposite to that of the blades 3 of the other module 2.
In an alternative embodiment that is not illustrated but that obviously falls within the scope of the invention, the impeller 1 blades 3 of one module 2 are inclined relative to the axis A in the same direction as the blades 3 of the other module 2.
In this specification and with reference in particular to the rotation of the forming elements 21, 22, the term “same direction of rotation” means that to an observer on the axis of rotation A at any point not between the forming elements 21, 22, both these elements turn in the same direction.
The term “opposite directions of rotation”, on the other hand, means that to an observer on the axis of rotation A at any point not between the forming elements 21, 22, both these elements turn in opposite directions.
The actuating means and devices used to accomplish the movements described and illustrated in this specification are of substantially known type and have therefore not been illustrated or described.
Advantageously, metal alloys may be used instead of plastic to form the impeller without thereby departing from the scope of the inventive concept.
The invention described can be modified and adapted in several ways without thereby departing from the scope of the inventive concept, as defined in the claims herein.
Moreover, all the details of the invention may be substituted by technically equivalent elements.
Number | Date | Country | Kind |
---|---|---|---|
B02005A000049 | Jan 2005 | IT | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/IB06/00141 | 1/27/2006 | WO | 3/1/2007 |