[0001] This invention concerns a perfected burner for heat generator as set forth in the
main claim.
[0002] The perfected burner according to the invention is applied to heating systems substantially
for domestic use either inside or immediately outside the room to be heated.
[0003] The burner according to the invention can also be applied in cooperation with heating
systems of a certain size to heat halls, gymnasiums, warehouses etc.
[0004] The burner according to the invention may be of the type which uses liquid fuel,
such as oil, or gas fuel.
[0005] The need to obtain heat generators is known, particularly for domestic use or similar,
which have all the characteristics of safety, simplicity of use and adjustment, high
efficiency, ease and speed of installation and/or maintenance.
[0006] It is also known that there are problems in the state of the art when the user needs
to get to the heat generator to carry out even the simplest adjustments and overhauls.
[0007] In some cases in the state of the art, some characteristics have been favoured over
others when it was not possible to reach a compromise between the various needs.
[0008] There are for example some burners known to the state of the art which are difficult
to install and/or maintain quickly because the designers tried to make them more compact
and to reduce the space they occupy. For the same reason, it is not always simple
to carry out the necessary adjustments for a correct functioning.
[0009] In other cases, in the attempt to achieve high efficiency and reduced consumption,
bulky and unfunctional burners have been designed.
[0010] Often, in order to put together as many functional characteristics as possible, burners
have been made which are suitable only for one type of heat generator and therefore
cannot be adapted for generators which have a combustion chamber of a different type.
[0011] Another serious problem which is found in burners known to the state of the art,
particularly in those which use blown air, is that of the pulsations at the beginning
caused by the sudden overpressure which occurs at the moment of lighting.
[0012] That may cause the flame to be extinguished and therefore it becomes necessary to
repeat the lighting procedure several times or even, in the worst case, a blow-back
of the flame, with extremely dangerous consequences for the user.
[0013] Moreover, these initial pulsations often cause the exhaust gases to leak from the
combustion chamber.
[0014] This problem is partially resolved, in the state of the art, by increasing the dimensions
of the burners and thus creating problems in the size and compactness of the structure
of the heat generator itself.
[0015] In particular, some solutions known to the state of the art conform the air inlet
to the ventilator in a suitable way, but this in any case causes an increase in the
total size.
[0016] DE-C-4232178 teaches to use a ventilator system which obtains at least a partial
recircling of the air propelled by the air propellor, in order to increase the prevalence
of the air and thus limit any excessive pressure at the moment of ignition.
[0017] In this document, however, given the reciprocal positioning of the propellor and
the chassis of the ventilator, only a very limited quantity of air is subject to a
recircling action, and therefore the increase in the steepness of the prevalence/flow
curve is very limited.
[0018] Moreover, this document does not include the body of the motor inside the ventilator,
nor does it allow the motor to be included therein, and this causes an enormous increase
in the axial bulk of the heat generator in its entirety.
[0019] FR-A-2212864 discloses a ventilator structure to feed a burner where the flame pipe
is entirely associated with the chassis of the ventilator, which makes it impossible
to perform any kind of adjustment and positioning without modifying the overall bulk
of the heat generator.
[0020] Moreover, it is substantially impossible to perform any kind of maintenance work
and/or replacement of internal parts without dismantling the entire structure, and
this can only be performed by the appropriately authorised and specialised staff.
[0021] The present applicants have designed, tested and embodied this invention to overcome
the shortcomings of the state of the art and to realise a simplified burner, of compact
size, extremely functional in its installation, its maintenance and its adjustments,
as well as to achieve further advantages.
[0022] This invention is set forth and characterised in the main claim, while the dependent
claims describe variants of the idea of the main embodiment.
[0023] The purpose of this invention is to obtain a simple burner, easy to install, adjust
and maintain, which gives a high operating efficiency while maximizing safety and
minimizing the size.
[0024] The perfected burner according to the invention has a structure which allows the
combustion chamber to be connected with a heat generator without any limits of form
or configuration of the combustion chamber itself.
[0025] The various parts of the burner are connected by means of attaching elements which
also act as elements to adjust the burner easily and in a way which is immediately
accessible from outside, even for someone of no specific skill in the art, thus assisting
and accelerating assembly operations and any necessary work on the internal components
or parts.
[0026] By means of these adjustment elements it is possible to adjust with extreme precision
the functioning parameters of the burner, guaranteeing extreme versatility and flexibility
of the whole plant which can be adapted to different applications and vary its operating
conditions according to necessity.
[0027] Moreover, the type of connection between the various components according to the
invention guarantees an airtight seal between the inside and outside of the burner.
[0028] The burner according to the invention comprises a chassis of such a shape as to guarantee,
in an extremely limited space, both the support and/or containment of the various
components, and also a flow of air suitable for an efficient and complete combustion
and an efficient discharge of the fumes.
[0029] The chassis, or containing structure, is equipped with attachment means to attach
it to the outer wall of the combustion chamber associated with the burner.
[0030] The chassis defines an inner seating where the flame pipe is inserted, and the front
end of the flame pipe faces inside the combustion chamber.
[0031] Inside the flame pipe, advantageously in a coaxial position with the pipe, there
is the fuel feed pipe, connected outside to the fuel feed means.
[0032] The rear, or outer, end of the flame pipe is associated with a cover element by means
of which the flame pipe is attached to the chassis of the burner.
[0033] According to the invention, the connection between the cover element and the chassis
can be adjusted from the outside by means of screws, in cooperation with at least
one replaceable spacer element.
[0034] This makes it possible to move the flame pipe axially so that its front end protrudes
more or less inside the combustion chamber.
[0035] This adjustment makes it possible to adapt the flame of the burner to the different
configurations of the combustion chamber and the different types of heat generator
to which the burner is applied.
[0036] The fuel feed pipe, which is inside the flame pipe, has a nozzle conformation in
correspondence with its front end outlet.
[0037] In front of this nozzle there is a disk element, the function of which is to make
the comburent air fed to the burner turbulent, and therefore to optimize the mixture
with the fuel given by the fuel feed pipe to the nozzle.
[0038] According to the invention, by acting on an adjustment accessible from the outside,
the fuel feed pipe can be made to run axially to the flame pipe.
[0039] This adjustment is advantageously screw-type, and is arranged on the cover element
associated with the rear end of the flame pipe.
[0040] By varying the reciprocal position between the turbulence disk and the front end
of the flame pipe outlet, the adjustment makes it possible to vary the turbulence
of the flow of comburent air and therefore to vary the mixture of comburent material
and combustible material.
[0041] By adjusting the axial position of the fuel pipe, it is also possible to vary the
position of the air shutter which regulates the flow of comburent air fed to the burner.
[0042] According to the invention, the position of this shutter, which is placed downstream
of the air intake propellor, can be adjusted autonomously and independently of the
position of the fuel feed pipe by acting on specific adjustment means accessible from
outside.
[0043] In the preferred embodiment of the invention, the adjustment means for the position
of the shutter are screw-type too, and are arranged on the cover element.
[0044] This double adjustment makes it possible to optimize the combustion in an extremely
precise way and therefore both to reduce consumption and to adapt the functioning
of the heat generator to the specific requirements.
[0045] The whole adjustment unit is easily removable for checking and maintenance inside
the burner, even without removing the burner itself from the wall of the combustion
chamber.
[0046] Since the whole adjustment system is on the flame pipe, rather than on the air inlet
opening on the chassis, the air inlet area, in the burner according to the invention,
can be put in a pipe and therefore the initial intake point can be placed at a considerable
distance from the burner.
[0047] One possible case is that an air intake point is placed outside the building where
the heat generator is found.
[0048] This allows a balanced flow of air to be achieved and thus guarantees greater safety
and comfort; moreover, it is possible to install auxiliary devices, such as filters
or silencers, on the pipes which feed the air to the burner.
[0049] According to the invention, the air propellor which feeds the comburent air to the
burner acts as a housing for the motor of the ventilator, which considerably reduces
the space occupied.
[0050] Moreover, the conformation of the air propellor and the motor is such as to guarantee
at least a partial recircling of the air aspired for combustion, which causes on one
side an increase in the prevalence of the air, or rather the vertical height to which
the air can be lifted, and on the other side an accentuation of the steepness in the
prevalence/flow curve.
[0051] By obtaining a high steepness in this curve, it is possible to combat efficiently
the high pressures which occur at the moment of ignition, and thus to limit significantly
the problems connected with these pressures, including the leakage of exhaust gas
from the combustion chamber.
[0052] According to the invention, this partial recircling of the aspirated air is obtained
by allowing the air which has not entered the flame pipe to circle outside the flame
pipe and then move near the air propellor again.
[0053] This recircled air, which is already under pressure, Is directed along a peripheral
zone of the propellor, and then later picked up by the propellor itself, from which
it receives new energy.
[0054] The new air, aspired through the opening in the body of the burner, is attracted
both by the normal depression determined by the action of the propellor and by the
induction effect generated by the flow of air under pressure generated by the recircling
air thus obtained.
[0055] The attached figures are given as a non-restrictive example and show a preferred
embodiment of the invention as follows:
- Fig. 1
- shows a longitudinal cross section of the perfected burner according to the invention;
- Fig. 2
- shows the diagram of a perfected burner according to the invention, with particular
reference to the area of the ventilator;
- Fig. 3
- shows a cross section seen from A of the burner according to the invention;
- Fig. 4
- shows the flow/prevalence curve of the flow of air given by the ventilator of a state
of the art burner and the same curve obtained by a burner according to the invention.
[0056] Fig. 1 shows the preferred embodiment of the perfected burner 10 according to the
invention.
[0057] The burner 10 comprises a chassis 11 which has at its lower end a hole 12 which allows
for the installation of a suitable ventilator 13, which has an air propellor 40 and
a motor 37, and defines the opening 15 for the flow of air, indicated by 14.
[0058] The chassis 11 is attached to the outer wall of the combustion chamber 26, in this
case, by means of a screw attachment element.
[0059] In the upper part of the chassis 11 there is a through hole 16 into which the flame
pipe 17 is inserted in such a way that its forward end, a truncated cone 17a, is substantially
placed inside the combustion chamber 26.
[0060] The rear end of the flame pipe 17 is associated with a cover element 18 by means
of a solid connection by the attachment element 24.
[0061] Between the cover element 18 and the flame pipe 17 there are holding elements 19,
in this case an O-ring packing, which make the flame pipe 17 airtight with the outside.
[0062] In this case, the holding elements 19 are inside a relative channel 20 which follows
the perimeter edge of the cover element 18.
[0063] In this case, the cover element 18 is attached to the chassis 11 of the burner by
means of a screw-type attachment element.
[0064] Between the attachment element 25 and the chassis 11 there is a spacer element 28
which can be replaced or modified.
[0065] The attachment element 25, cooperating with the spacer element 28, makes it possible
to adjust the axial position of the flame pipe 17 inside the chassis 11 and, therefore,
the position of the forward end 17a with respect to the combustion chamber 26 with
which the burner 10 is associated.
[0066] The length of the spacer element 28 can be adapted according to requirements, or
replaced.
[0067] By varying the position of the forward end 17a of the flame pipe 17 with respect
to the combustion chamber 26, it is possible to adapt the flame of the burner 10 to
the various forms and dimensions of the combustion chamber 26 and the different applications,
such as boiler, hot air generators, etc., which can be used with the burner 10.
[0068] The cover element 18 has a hole 21, in this case situated on the axis, inside which
there is the fuel feed pipe 22.
[0069] On the outside too, in cooperation with the hole 21 there is a channel 20 in which
an O-type packing is inserted.
[0070] On the outside the fuel feed pipe 22 has an attachment 38 to the conventional fuel
feeding means, whether they be liquid or gas.
[0071] The fuel feed pipe 22, contained in the flame pipe 17, can be made to run axially
through the hole 21.
[0072] The axial position of the fuel feed pipe 22 in the flame pipe 17 can be adjusted,
in this case, by acting on a screw-type attachment and adjustment element 23. This
element 23 is solid with the fuel feed pipe 22 and its position can be adjusted with
respect to the cover element 18.
[0073] By acting on the attachment and adjustment element 23, the fuel feed pipe 22 is moved
backwards or forwards axially inside the flame pipe 17.
[0074] The axial movement of the fuel feed pipe 22 is assisted, in this case, by a runner
element 29, of a shape mating with the inner section of the flame pipe 17, which is
also used to support and guide the fuel feed pipe 22.
[0075] The fuel feed pipe 22 has at its ends nozzle-type outlet means 30 in front of which
there is a turbulence disk 31.
[0076] In this way, by moving one way or the other the fuel feed pipe 22 with respect to
the flame pipe 17, it is possible to vary the turbulence of the comburent air fed
into the combustion area, and therefore it is possible to vary the combustion itself.
[0077] The rear or outer end of the fuel feed pipe 22 is associated with a removable plug
32 where a device to pre-heat the fuel could possibly be housed.
[0078] The flame pipe 17, in that part of its surface contained inside the chassis 11 and
facing the ventilator 13, has a slit 33 through which the air fed by the ventilator
13 passes.
[0079] The section of this slit 33 through which the air passes is determined by the position
of an air shutter 34 contained inside the flame pipe 17 and positioned, in this case,
downstream of the ventilator unit 13.
[0080] The position of the air shutter 34 can be adjusted independently of the flame pipe
17 by acting on the appropriate screw-type adjustment element 35, arranged on the
cover element 18, of which the activating mechanism is accessible from the outside.
[0081] In this way, the flow of air fed to the combustion area at the outlet of the fuel
feed pipe 22 can be adjusted in an extremely quick and simple way to vary the combustion.
[0082] By dismantling the cover element 18, which can be done extremely easily even by non-specialist
users, it is possible to accede to the inside of the burner 10 very quickly, to check
it or for maintenance.
[0083] Figure 2 shows a partial drawing of the perfected burner 10 according to the invention.
[0084] In this Figure, it can be seen how the space occupied is very small as the motor
37 of the ventilator 13 is substantially housed in the space defined by the air propellor
40 itself.
[0085] The motor 37 is attached to the chassis 11 by means of a flange 53.
[0086] In this way, most of the motor 37 is contained inside the space taken up by the chassis
11, and, in this case, only the pump 39 remains outside this space.
[0087] In the perfected burner 10, moreover, the opening 15 for the flow of air 14 is on
the same side as the motor 37 and this gives a further reduction in the overall space
occupied.
[0088] Figure 3 shows a cross section seen from A of the perfected burner 10 according to
the invention.
[0089] In this case, on the outer surface of the motor 37 there are two fins in a diametric
position: upper longitudinal fin 41 and lower longitudinal fin 42. In cooperation
with the inner surface of the propellor 40, these fins 41 and 42 define an upper intake
area 43 and a lower intake area 44.
[0090] The chassis 11, on its lower part, defines an area 48 where the air passes through.
This area 48 widens progressively from its initial area until it reaches a width equal
to at least 30% of the width of the propellor 40 in the area substantially diametric
to the initial area.
[0091] The flow of air 14 aspired from the outside through the opening 15 is pushed by the
air propellor 40 towards the slit 35 of the flame pipe 17.
[0092] This flow of air is conveyed through a space 54 which communicates with the slit
33, the space 54 being between the head of the air propellor 40 and the inner wall
of the chassis 11 which is placed on the side of the flange 53 which mounts the motor
37.
[0093] In this case, the head of the propellor 40 is closed by a screen 55 which prevents
air entering.
[0094] In this case, the width of the area 48, together with the rounded conformation of
the inner surface of the chassis 11, causes part of the air, indicated by 49, to enter
the recircling conduit 45 which is placed around the flame pipe 17, rather than entering
directly the flame pipe 17 itself through the slit 33.
[0095] From the recircling conduit 45 the recircled air, which already has a certain pressure,
is aspired downwards through the conveyor space 54, as it is prevented from entering
the slit 33 by the deflector element 46.
[0096] The deflector element 46 is attached to the chassis 11 on the inner side from where
the flange 53 is positioned and extends substantially on a horizontal plane to cover
approximately the width of the propellor 40.
[0097] The recircled air, indicated by the arrows 50, is confined in the upper intake area
43 by the diametric fins 41 and 42, after passing over the deflector element 46. From
here it is forced by the propellor 40 into the sickle-shaped tangential area 47 between
the propellor 40 and the chassis 11, acquiring new energy from the propellor 40.
[0098] The tangential area 47 grows progressively wider towards the bottom and is found
substantially at the same axial height as the air propellor 40.
[0099] The recircled air, indicated by 51, mixes with the flow of new air, indicated by
52, aspired by the air propellor 40 itself through the opening 15, which is found
substantially in correspondence with the end of the tangential area 47.
[0100] According to this configuration, the new air is therefore aspired by the double depression
created by the air propellor 40 and the induction effect determined by the flow of
recircled air fed through the upper intake area 43 and the sickle-shaped tangential
area 47.
[0101] This makes it possible to modify the characteristics of the air sent to the flame
pipe 17 in terms of flow/prevalence, as shown in the graph in Fig. 4.
[0102] The graph, where the flow expressed in cu.m. per hour is indicated in x-coordinate
and the prevalence expressed in mm. using a column of water as a parameter of measurement
is indicated in y-coordinate, gives a curve L which is obtained with a substantially
conventional burner, and a curve L' which is obtained with the perfected burner 10
according to the invention.
[0103] The greater steepness of the curve L' causes, when the system is working, a good
compensation of the overpressures which occur during ignition and which cause the
initial pulsations known to the state of the art.
[0104] This guarantees a more efficient combustion and makes it possible to overcome efficiently
the resistences which the fumes encounter in conventional burners as they leave the
heat generator.
1. Perfected boiler for heat generator, which can be used in cooperation with heating
plants such as boilers, hot air generators etc. for heating rooms in general, the
burner comprising at least a containing structure (11) associated with the outer wall
of a combustion chamber (26) and defining inside the seating for at least a flame
pipe (17) and for a ventilator unit (13), the flame pipe (17) containing inside a
fuel feed pipe (22) and having at its periphery a slit (33) through which the air
passes associated with the ventilator unit (13), the ventilator unit (13) having an
air propellor (40) carried by an actuating motor (37) supported by a mounting flange
(53), the slit (33) cooperating with a shutter element (34), the fuel feed pipe (22)
having at its end a nozzle outlet (30) cooperating with a turbulence disk (31), there
also being an intake opening (15), the burner being characterised in that the containing structure (11) defines, laterally to the air propellor (40), an area
(48) through which the air passes which increases progressively to a width equal to
at least 30% of the diameter of the air propellor (40) in the area substantially diametric
to its initial part, and around the flame pipe (17) an annular recircling conduit
(45) which communicates at its inlet with that area (48), the burner also being characterised in that the air propellor (40) defines inside a housing space for at least part of the motor
(37), between the motor (37) and the inner diameter of the air propellor (40) there
being longitudinal fins (41, 42) substantially diametrically arranged and defining,
together with the air propellor (40), a lower intake area (44) communicating wih the
opening (15), and a higher intake area (43) communicating with the annular recircling
conduit (45), between the air propellor (40) and the inner side of the containing
structure (11) on the side of the flange (53) there being an annular space (54) to
convey the air.
2. Burner as in Claim 1, in which between the annular recircling conduit (45) and the upper intake area (43) there
is a deflector element (46) which extends on a substantially horizontal plane as far
as the proximity of the flame pipe (17) and the proximity of the slit (33) through
which air passes, the deflector element (46) being solid with the inner side of the
containing structure (11) on the part opposite the flange (53) and extending at a
right angle as far as the width of the air propellor (40), between the air propellor
(40) and the containing structure (11) there being a tangential area (47) which communicates
at its upper end with the upper intake area (43) and at its lower end with the air
intake opening (15).
3. Burner as in Claim 2, in which the tangential area (47) is substantially at the same axial height as the air propellor
(40), is sickle-shaped and becomes progressively wider towards the bottom.
4. Burner as in any of the claims hereinbefore, in which the air propellor (40) has a screen (55) to close the annular space (54) which conveys
the air.
5. Burner as in any of the claims hereinbefore, in which the air intake opening (15) communicates with the lower intake area (44) and substantially
begins at the lower longitudinal fin (42).
6. Burner as in any of the claims hereinbefore, in which at least the axial position of the flame pipe (17) with respect to the combustion
chamber (26) can be adjusted manually and independently of the other components of
the burner (10).
7. Burner as in Claim 6, in which the means to adjust the axial position of the flame pipe (17) are accessible from
outside, at the front of the burner (10) and comprise at least screw-type adjustment
means (25) and replaceable deflector means (28).
8. Burner as in any of the claims hereinbefore, in which at least the axial position of the shutter (34) with respect to the flame pipe (17)
can be adjusted manually and independently of the other components of the burner (10).
9. Burner as in Claim 8, in which the means to adjust the axial position of the air shutter (34) are accessible from
the outside at the front of the burner (10) and have at least screw-type adjustment
means (35).
10. Burner as in any of the claims hereinbefore, in which the adjustment means (25,28, 35) are anchored on a removable cover element (18) associated
with the rear end of the flame pipe (17).
11. Burner as in any of the claims hereinbefore, in which the insertion seating of the flame pipe (17) is defined by a hole (16) made in the
cover element (18) and has means (19) to create an airtight seal at its periphery.
12. Burner as in any of the claims hereinbefore, in which the insertion seating of the fuel feed pipe (22) is defined by a hole (21) made in
the cover element (18) and has means (19) to create an airtight seal at its periphery.