[0001] The present invention relates to a manifold assembly for a filling machine apt to
fill a plurality of receptacles, in particular containers such as bottles or the like,
with a pourable product, preferably of the food type.
[0002] The present invention further relates to a method for filling a receptacle, in particular
a container such as a bottle or the like, with a pourable product, preferably of the
food type.
[0003] Rotary filling machines are known, which substantially comprise a carousel, rotatable
about a vertical axis, a tank containing the pourable product and a plurality of valve
filling devices peripherally carried by the carousel in respective radially outer
positions relatively to the aforementioned axis. More specifically, the filling devices
are advanced along a circular transfer path defined by the carousel.
[0004] In detail, each filling device is configured to feed a pre-set amount of pourable
product to a respective receptacle, while the latter advances below the relative filling
device along the aforementioned transfer path.
[0005] Typically, the known filling machines further comprise a manifold assembly configured
to fluidically connect the filling devices to the tank.
[0006] In detail, the manifold assembly is provided with a manifold, generally arranged
concentrically to the axis of the carousel and comprising:
- a stator having substantially cylindrical configuration and defining a first channel
for the pourable product fluidically connected to the tank by means of a duct; and
- a rotor also having a substantially cylindrical configuration, which defines a second
channel fluidically connected to the first channel, is rotatable, relatively to the
stator, about the axis of the carousel, and comprises a plurality of openings, each
fluidically connected to the second channel and to a respective filling device.
[0007] In detail, the first channel receives the pourable product from the tank through
the duct; the second channel receives, in use, the pourable product from the first
channel and is configured to distribute it to the filling devices through the respective
openings and through respective pipes.
[0008] In particular, each pipe is rotatable about the axis of the carousel integrally with
the respective filling device and is configured to fluidically connect the second
channel to a single respective filling device.
[0009] In this way, the pourable product can be conveyed from the tank, which is fixed,
to the filling devices, which are mobile, and, from the latter to respective receptacles
to be filled.
[0010] Therefore, the manifold enables a fluidic connection to be achieved between fixed
components and rotating components.
[0011] The manifolds of the known type further comprise one or more sealing elements, operating
in a dynamic manner, configured to enable a fluid-tight coupling between the stator
and the rotor.
[0012] Generally, said manifolds are further provided with one or more mechanical members
configured to allow the rotation of the rotor relatively to the stator, for example,
bearings, bushings or the like.
[0013] In particular the sealing elements, bearings and bushings mentioned above operate
at high speeds and, consequently, are subject to overheating which can cause a significant
wear and a reduction of their lifespan.
[0014] It is therefore an object of the present invention to provide a manifold assembly
for a filling machine, which allows to overcome the above-mentioned drawback in a
straightforward and low-cost manner.
[0015] According to the invention, this object is achieved by a manifold assembly for a
filling machine as claimed in claim 1.
[0016] The present invention further relates to a filling method as claimed in claim 12.
[0017] For a better understanding of the present invention, two preferred non-limiting embodiments
will be described in the following, purely by way of example and with the aid of the
attached figures, wherein:
- Figure 1 is a schematic side view, partially sectioned and with parts removed for
clarity, of a filling machine comprising a manifold assembly implemented according
to a first preferred embodiment of the present invention;
- Figure 2 is a larger-scale section view with parts removed for clarity of part of
the manifold assembly of figure 1;
- Figure 3 schematically illustrates some of the components of the manifold assembly
of figure 2;
- Figure 4 is a section view, with parts removed for clarity, of a manifold assembly
implemented according to a second preferred embodiment of the present invention; and
- Figure 5 schematically illustrates some of the components of the manifold assembly
of figure 4.
[0018] With reference to the attached figures, number 1 indicates as a whole a filling machine
adapted to fill a plurality of receptacles 2 (only one schematically illustrated in
figure 1), in particular containers such as bottles or the like, with a pourable product,
preferably a pourable food product.
[0019] The filling machine 1 substantially comprises a carousel 3, rotatable about a vertical
axis A, a fixed tank 4 (only schematically shown in figure 1) containing the pourable
product, and a plurality of filling devices 5, preferably valve filling devices 5.
[0020] In particular, each filling device 5 is peripherally carried by the carousel 3 in
a respective radially outer position relatively to the axis A.
[0021] Each filling device 5 is configured to feed a pre-set amount of pourable product
to a respective receptacle 2, while the latter advances below the relative filling
device 5 along a circular transfer path defined by the carousel 3.
[0022] Preferably, each filling device 5 is designed to be selectively moved, according
to a known manner and not described in detail, between a closed position, in which
it prevents the pourable product from flowing within the respective receptacle 2 and,
an open position, in which it allows the outflow of the pourable product within the
respective receptacle 2.
[0023] The filling machine 1 further comprises a manifold assembly 6 including, in turn,
a manifold 7, the latter having a substantially cylindrical configuration, being arranged
concentric to the axis A and being configured to fluidically connect the tank 4 to
the filling devices 5.
[0024] As can be seen in figure 2, the manifold 7 comprises:
- a hollow stator 8, substantially cylindrical and internally defining a channel 9 coaxial
to the axis A and fluidically connected to the tank 4 by means of a duct 4a (illustrated
in figure 1); and
- a rotor 10, also being hollow, substantially cylindrical and coaxial to the stator
8, defining a channel 11 coaxial to the channel 9 and fluidically connected thereto
by means of an axial opening 12, and rotatable about the axis A relatively to the
stator 8.
[0025] Preferably, the rotor 10 comprises, at one upper end portion 13 thereof, a plurality
of radial openings 14, in particular having a circular shape.
[0026] In detail, each opening 14 is fluidically connected to the channel 11 on one side
and, on the opposite side, it is connected to a respective filling device 5 through
a relative pipe 15 extending from the manifold 7 in a substantially radial manner
towards the outside relatively to the axis A. In particular, each pipe 15 is rotatable
about the axis A in an integral manner to the respective filling device 5 and to the
rotor 10, whereas the duct 4a is fixed and integral to the stator 8.
[0027] In light of what has been described above, the manifold 7 enables a fluidic connection
to be achieved between fixed components, namely the tank 4 and the duct 4a, and rotating
components, namely the filling devices 5 and the relative pipes 15.
[0028] According to the preferred and non-limiting embodiment illustrated in figure 2, the
rotor 10 comprises:
- a first rotor element 16 arranged, at least partly, within the stator 8 and externally
cooperating with the latter by means of first interface elements, in particular a
bearing 17 and a sealing element 18;
- a second rotor element 19 surrounding at least part of the rotor element 16 arranged,
at least partly, within the stator 8 and cooperating externally with the latter by
means of second interface elements, in particular a radial bearing 20 and two sealing
elements 21, arranged on axially opposite sides of the bearing 20;
- a third rotor element 22 surrounding at least part of the rotor elements 16 and 19
arranged, at least partly, inside the stator 8 and cooperating externally with the
latter by means of third interface elements, in particular a radial bearing 23 and
a sealing element 24.
[0029] Preferably, the rotor elements 16, 19 and 22 are coaxial to the axis A and have respective
cylindrical flanged shapes.
[0030] In detail, each rotor element 16, 19 and 22 comprises a hollow cylindrical portion
and a flange also being hollow and axially extending from the cylindrical portion.
In greater detail, the upper flange of the cylindrical element 16 defines the upper
portion 13 of the rotor.
[0031] As can be seen in figure 2, the interface elements are radially interposed between
the stator 8 and the rotor 10.
[0032] In particular, the bearings 17, 20 and 23 are configured to allow the rotation of
the rotor elements 16, 19 and 22 respectively, with respect to the relative portions
of the stator 8 with which they cooperate.
[0033] Preferably, the sealing elements 18, 21 and 24 are carried by the stator 8 and comprise
at least an operating portion configured to cooperate in contact, in a dynamic manner,
with the rotor 10.
[0034] In the specific case described herein, the sealing elements 18, 21 and 24 are housed
in respective dedicated radial grooves obtained in the stator 8 and are configured
to cooperate in contact, in a dynamic manner, with the rotor elements 16, 19 and 22,
respectively.
[0035] According to a known manner not described in detail, the sealing element 18 is configured
to prevent the leaking of the pourable product when the product flows from the channel
9 of the stator 8 to the channel 11 of the rotor 10.
[0036] In addition, the sealing elements 21 and 24 are configured to prevent the leaking
of gas (for example, carbon dioxide or air) from fluidic connection portions, between
the stator 8 and the rotor 10, of the pressurisation/discharge and decompression ducts
(partially illustrated in figures 1 and 2 and known per se and not described in detail).
In particular, said connection portions are defined, respectively, by the rotor elements
19 and 22.
[0037] According to a possible alternative not illustrated herein, the sealing elements
18, 21 and 24 could be carried by the rotor 10, in respective dedicated radial grooves
made in respective rotor elements 16, 19 and 22 and, could comprise at least an operating
portion configured to cooperate in contact, and in a dynamic manner, with the stator
8.
[0038] In use the interface elements, namely the bearings 17, 20 and 23 and, the sealing
elements 18, 21 and 24 are subjected to overheating, due to the friction to which
they are subjected to during their sliding onto the rotor 10 and due to the high operating
speeds.
[0039] Advantageously, the manifold assembly 6 further comprises feeding means 50 configured
to feed a coolant fluid to at least a heat exchange area 51 between at least one of
the aforementioned interface elements, namely the bearings 17, 20 and 23 and the sealing
elements 18, 21 and 24 and the coolant fluid.
[0040] Preferably the coolant fluid is water.
[0041] In particular, the heat exchange area 51 is arranged in a radially outer position
relatively to the channel 9 and to the channel 11, with respect to the axis A.
[0042] In detail, the manifold 7 comprises at least a wall 25 carried by the stator 8 and
defining the heat exchange area 51.
[0043] In greater detail, the coolant fluid is configured to lap, preferably externally,
the wall 25 in order to remove an amount of heat that the wall 25 absorbs, in use,
from the interface element and therefore to cool the latter.
[0044] According to the preferred yet non-limiting embodiment described and illustrated
herein, the manifold 7 comprises two walls 25 and 26 of the type described above,
carried by the stator 8.
[0045] In particular the wall 25 defines the heat exchange area between the coolant fluid
and: the bearings 20 and 23; one of the sealing elements 21 (the one axially interposed
between the bearings 20 and 23); the sealing element 24. Therefore, the wall 25 absorbs
the amount of accumulated heat, due to the friction, from said interface elements.
[0046] The wall 26 defines the heat exchange area 51 between the coolant fluid and: the
bearing 20; the other sealing element 21. Therefore, the wall 26 absorbs the amount
of accumulated heat, due to friction, from these interface elements.
[0047] In particular, the wall 25 is arranged in contact with the bearings 20 and 23 and
with the sealing elements 21 and 24, in order to absorb the amount of accumulated
heat from said interface elements by heat conduction.
[0048] In the same manner, the wall 26 is arranged in contact with the bearing 20 and with
the sealing element 21, in order to absorb the amount of accumulated heat from these
latter interface elements by heat conduction.
[0049] Preferably, the aforementioned feeding means 50 comprise two chambers 27, 28 delimited,
respectively, and at least partly, by the walls 25, 26.
[0050] In detail, the chamber 27 is delimited by a further radially outermost wall 29 parallel
and facing the wall 25, and by another two walls 30 facing one another and orthogonal
to the walls 25 and 29. The chamber 27 has, therefore, a rectangular cross-section
and annularly develops about the axis A.
[0051] In the same manner, the chamber 28 is delimited by a further radially outermost wall
31 parallel and facing the wall 26, and by another two walls 32 facing one another
and orthogonal to the walls 26 and 31. The chamber 28 has, therefore, rectangular
cross-section and annularly develops about the axis A.
[0052] In particular, the chamber 27 is arranged above the chamber 28 in respect to the
axis A.
[0053] In detail, the chambers 27 and 28 are configured to be supplied in a continuous manner
with a coolant fluid, through respective inlet openings I, and to be emptied (from
the coolant fluid) through respective outlet openings 0.
[0054] For this purpose, the feeding means 50 further comprise a circuit 33 (figure 3) configured
to supply the coolant fluid in a continuous manner within the chambers 27 and 28 through
the respective inlet openings I, and configured to extract the coolant fluid in a
continuous manner from the same chambers 27 and 28, through the respective outlet
openings 0.
[0055] As can be seen in figure 3, the circuit 33 comprises:
- a source, preferably a tank 34, containing the coolant fluid;
- ducts 35, configured to convey the coolant fluid from the tank 34 inside the respective
chambers 27 and 28; and
- a cooler 36 configured to lower the temperature of the coolant fluid, in respect to
a given network temperature, before the latter laps the walls 25 and 26.
[0056] In detail, the cooler 36 ensures an optimal adjustment of the coolant fluid temperature,
in order to obtain a effective heat exchange, in particular a cooling, between the
interface elements and the coolant fluid itself.
[0057] The operation of the manifold assembly 6 according to the present invention will
be described in the following, with reference to a regime operating condition wherein
the pourable products flows from the channel 9 of the stator 8 towards the channel
11 of the rotor 10 and from the latter towards each filling device 5 through the relative
opening 14 and the corresponding pipe 15.
[0058] In this condition, the rotor 10 rotates about the axis A at a given speed and the
interface elements are, therefore, subjected to an overheating caused by friction,
due to the sliding of the same onto the respective outer surfaces of the rotor elements
16, 19 and 22.
[0059] With the aim of removing the accumulated heat from the interface elements, the coolant
fluid is conveyed, by means of the circuit 33, to the inside of the cooler 36 and,
subsequently to the inside of the chambers 27 and 28, so as to lap the walls 25 and
26, respectively.
[0060] Therefore, the coolant fluid removes the heat absorbed by the walls 25 and 26.
[0061] Subsequently, the heated coolant fluid exits the chambers 27 and 28 through the respective
outlet openings 0 and is recirculated inside the cooler 36, in order to lower the
temperature.
[0062] Therefore, the cooled coolant fluid is again, redirected towards the chambers 27
and 28 and the cooling process is repeated.
[0063] In order to tackle the possible loss of coolant fluid, a new amount of coolant fluid,
drawn from the tank 34, is periodically added. Therefore, the circuit 33 is a closed
circuit.
[0064] In figure 4, number 106 indicates as a whole, a second preferred embodiment of the
manifold assembly according to the present invention.
[0065] Since the manifold assembly 106 is similar, in terms of its operation, to the manifold
assembly 6, the description that follows will be limited to the structural differences
between the two manifold assemblies 6, 106; the parts of the manifold assembly 106
that are the same or correspond to parts already described, in relation to the manifold
assembly 6, will be indicated by using, whenever possible, the same references.
[0066] In particular, the manifold 7 of the manifold assembly 106 comprises a thrust bearing
plate 117 that operates in the same manner as the bearing 17 of the manifold 7 of
the manifold assembly 6.
[0067] Furthermore, according to this second preferred embodiment of the present invention,
the manifold assembly 106 comprises feeding means 150 including, in turn, three spraying
members, preferably three nozzles 108 configured to spray the coolant fluid directly
on radially outer surfaces 25a and 26a of the walls 25 and 26, respectively, defining
the heat exchange area 51.
[0068] As illustrated in figure 5, the feeding means 150 further comprise, a circuit 133
configured to supply the coolant fluid in a continuous manner to the spraying members
108.
[0069] In particular, the circuit 133 of the manifold assembly 106 is similar to the circuit
33 of the manifold assembly 6. Even more in particular, the circuit 133 differs from
the circuit 33 due to the fact that it is an open circuit.
[0070] Furthermore, as can be seen in figure 4, the manifold assembly 106 is different from
the manifold assembly 6 due to the fact that the stator 8 of the manifold 7 of the
manifold assembly 106 comprises a hollow cylindrical stator element 110, radially
interposed between the rotor element 16 and the rotor element 19 and coaxial to the
axis A.
[0071] In particular, the stator element 110 externally cooperates with the rotor element
19 by means of a further sealing element 111, carried by the stator element 110 itself
in a dedicated radial groove.
[0072] Only the differences between the operation of the manifold assembly 6 and the operation
of the manifold assembly 106 are illustrated hereinafter.
[0073] In detail, the coolant fluid sprayed by the nozzles 108 laps the surfaces 25a and
26a, removing the heat accumulated by the interface elements and absorbed by the walls
25 and 26 and, therefore, cools said interface elements.
[0074] Furthermore, the coolant fluid runs axially, due to gravity, firstly along the surface
25a and then along the surface 26a, until lapping the area of the manifold 7 of the
manifold assembly 106 at which the sealing element 18 and the thrust bearing plate
117 are axially arranged.
[0075] In this manner, also the latter interface elements are cooled.
[0076] In light of what has been described above, the coolant fluid, after having been sprayed
by the nozzles 108, is not reintroduced in the circuit 133. Therefore, a new amount
of coolant fluid is added in a continuous manner within the circuit 133, drawn from
the relative tank 34.
[0077] From an examination of the characteristics of the manifold 6, 106 according to the
present invention, the advantages that it allows to obtain are obvious.
[0078] In particular, the presence of feeding means 50, 150 for the coolant fluid according
to the present invention allows an efficient cooling of the interface elements 17,
18, 20, 21, 23, 24, 111, 117 interposed between the stator 8 and the rotor 10, limiting
in this manner, the wear and increasing their lifespan.
[0079] It is clear that modifications and variations can be made to the manifold assembly
6, 106 described and illustrated herein, without departing from the scope of protection
defined by the claims.
[0080] In particular, the feeding means 50, 150 could comprise, simultaneously, both the
chambers 27 and 28, as well as the nozzles 108, or any one of their combinations,
for example, a single chamber 27, 28 and two nozzles 108, or two chambers 27, 28 and
one nozzle 108 apt to spray coolant fluid in the area of the sealing element 18 and
of the bearing 17/thrust bearing plate 117.
1. A manifold assembly (6; 106) for a filling machine (1) apt to fill a plurality of
receptacles (2) with a pourable product; said assembly (6; 106) comprising a manifold
(7) provided with:
- a stator (8) defining a first channel (9) configured to be fed with said pourable
product; and
- a rotor (10) rotatable in respect to said stator (8) about an axis (A) and defining
a second channel (11) fluidically connected to said first channel (9);
said rotor (10) comprising at least one opening (14) fluidically connected to said
second channel (11) and fluidically connectable, in use, to at least one respective
filling device (5) of said filling machine (1);
said manifold (7) further comprising at least one interface element (17, 18, 20, 21,
23, 24; 111, 117) interposed between said stator (8) and said rotor (10) and subject,
in use, to overheating;
characterized in that it further comprises feeding means (50, 150) configured to feed a coolant fluid to
at least a heat exchange area (51) between said interface element (17, 18, 20, 21,
23, 24; 111, 117) and said coolant fluid.
2. The manifold assembly according to claim 1, wherein said heat exchange area (51) is
arranged in a position radially external to said first channel (9) and said second
channel (11).
3. The manifold assembly according to claim 1 or 2, wherein said manifold (7) comprises
at least a wall (25, 26) defining said heat exchange area (51); said coolant fluid
lapping, in use, said wall (25, 26) in order to remove an amount of heat absorbed
by said wall (25, 26) and, therefore, to cool said interface element (17, 18, 20,
21, 23, 24; 111, 117).
4. The manifold assembly according to claim 3, wherein said wall (25, 26) is arranged
in contact with said interface element (17, 18, 20, 21, 23, 24; 111, 117), so that
said wall (25, 26) absorbs said amount of heat from said interface element (17, 18,
20, 21, 23, 24; 111, 117) through conduction; and/or wherein said wall (25, 26) is
carried by said stator (8).
5. The manifold assembly according to any one of the claims 2 to 4, wherein said feeding
means (50) comprise at least a chamber (27, 28) delimited, at least partly, by said
wall (25, 26) and configured to be fed in a continuous manner with said coolant fluid
through an inlet opening (I), and to be emptied via an outlet opening (0).
6. The manifold assembly according to claim 5, wherein said feeding means (50) further
comprise a circuit (33) configured to feed, in a continuous manner, said coolant fluid
to said chamber (27, 28), through said inlet opening (I), and to extract, in a continuous
manner, said coolant fluid from said chamber (27, 28), via said outlet opening (0).
7. The manifold assembly according to any one of the claims 2 to 4, wherein said feeding
means (150) comprise at least one spraying member (108) configured to spray said coolant
fluid directly on a radially outer surface (25a, 26a) of said wall (25, 26).
8. The manifold assembly according to claim 7, wherein said feeding means (150) further
comprise a circuit (133) configured to feed, in a continuous manner, said coolant
fluid to said spraying member (108).
9. The manifold assembly according to any one of the preceding claims, wherein said interface
element (17, 18, 20, 21, 23, 24; 111, 117) defines at least a sealing element (18,
21, 24; 111) comprising at least an operating portion configured to cooperate in contact
with one of said rotor (10) and said stator (8).
10. A filling machine (1) adapted to fill a plurality of receptacles (2) with a pourable
product; said filling machine (1) comprising:
- at least a filling device (5) configured to feed said pourable product to a respective
receptacle (2);
- a fixed tank (4) containing said pourable product and fluidically connectable to
said at least one filling device (5); and
- a manifold assembly (6; 106) according to any one of the preceding claims.
11. The filling machine according to claim 10, when depending from claim 6 or 8, wherein
said circuit (33; 133) further comprises a cooler (36) configured to lower the temperature
of said coolant fluid, in respect to a given network temperature, before the latter
laps said wall (25, 26).
12. A method for filling a receptacle (2) with a pourable product, by means of a filling
device (5), comprising the steps of:
i) feeding said pourable product to a manifold assembly (6; 106) comprising a manifold
(7) comprising, in turn:
- a stator (8), defining a first channel (9) which can be fed with said pourable product;
and
- a rotor (10) rotatable, in respect to said stator (8), about a given axis (A) and
defining a second channel (11) fluidically connected to said first channel (9);
- at least an interface element (17, 18, 20, 21, 23, 24; 111, 117) interposed between
said stator (8) and said rotor (10) and subject to heating;
ii) feeding said pourable product to said filling device (5) by means of an opening
(14) of said rotor (10) fluidically connected to said second channel (11) and fluidically
connectable to said filling device (5); and
iii) feeding said pourable product to said receptacle (2) by means of said filling
machine (5);
characterized in that it also comprises the step of:
iv) adducing a coolant fluid to a heat exchange area (51) between said interface element
(17, 18, 20, 21, 23, 24; 111, 117) and said coolant fluid.
13. The method according to claim 12, wherein said heat exchange area (51) is radially
external to said first channel (9) and said second channel (11).
14. The method according to claim 12 or 13, further comprising the steps of:
v) adducing said coolant fluid to a wall (25, 26) defining said heat exchange area
(51); said coolant fluid lapping, in use, said wall (25, 26) so as to remove an amount
of heat absorbed by said wall (25, 26) and, therefore, to cool said interface element
(17, 18, 20, 21, 23, 24; 111, 117).