WO2010042079A1 - Device for generating and transmitting heat capable of operating with fuel in any physical state and combustion flame - Google Patents

Device for generating and transmitting heat capable of operating with fuel in any physical state and combustion flame Download PDF

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Publication number
WO2010042079A1
WO2010042079A1 PCT/SV2008/000003 SV2008000003W WO2010042079A1 WO 2010042079 A1 WO2010042079 A1 WO 2010042079A1 SV 2008000003 W SV2008000003 W SV 2008000003W WO 2010042079 A1 WO2010042079 A1 WO 2010042079A1
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WO
WIPO (PCT)
Prior art keywords
air
cylinder
fuel
flat
combustion
Prior art date
Application number
PCT/SV2008/000003
Other languages
Spanish (es)
French (fr)
Inventor
Rene Mauricio Nuñez Suarez
Original Assignee
Nunez Suarez Rene Mauricio
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nunez Suarez Rene Mauricio filed Critical Nunez Suarez Rene Mauricio
Priority to MX2011003817A priority Critical patent/MX2011003817A/en
Priority to BRPI0823153-2A priority patent/BRPI0823153A2/en
Priority to CN200880132274.9A priority patent/CN102245967B/en
Priority to PCT/SV2008/000003 priority patent/WO2010042079A1/en
Priority to EP08813763.3A priority patent/EP2345842A4/en
Priority to PA20098845101A priority patent/PA8845101A1/en
Priority to ARP090103900A priority patent/AR076439A1/en
Priority to UY0001032170A priority patent/UY32170A/en
Priority to PE2009001182A priority patent/PE20100614A1/en
Publication of WO2010042079A1 publication Critical patent/WO2010042079A1/en
Priority to US13/081,691 priority patent/US20110239916A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C1/00Combustion apparatus specially adapted for combustion of two or more kinds of fuel simultaneously or alternately, at least one kind of fuel being either a fluid fuel or a solid fuel suspended in a carrier gas or air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36Details, e.g. burner cooling means, noise reduction means
    • F23D11/40Mixing tubes or chambers; Burner heads
    • F23D11/404Flame tubes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/20Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D17/00Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23LSUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L1/00Passages or apertures for delivering primary air for combustion 
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23LSUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L9/00Passages or apertures for delivering secondary air for completing combustion of fuel 
    • F23L9/02Passages or apertures for delivering secondary air for completing combustion of fuel  by discharging the air above the fire
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23MCASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M3/00Firebridges
    • F23M3/12Firebridges characterised by shape or construction
    • F23M3/14Firebridges characterised by shape or construction with apertures for passage of combustion products
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23MCASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M9/00Baffles or deflectors for air or combustion products; Flame shields
    • F23M9/06Baffles or deflectors for air or combustion products; Flame shields in fire-boxes

Definitions

  • the present invention aims to provide a heat generating and transmitting apparatus capable of operating with fuel in any physical state, that is to say it can be fed with fuel in solid, liquid state or gaseous. At the same time, it is the object of the invention to maximize the combustion efficiency, that is, to optimize fuel consumption, in order to result in considerable fuel savings and minimize the emission of pollutants.
  • the present invention has for its object to describe a combustion flame generated within the described heat generating and transmitting apparatus, flame whose properties are highly advantageous in terms of heat transfer and to avoid the production of contaminants.
  • the present invention is encompassed within the methods of obtaining energy through combustion processes, within the processes of heat transfer and its generating and transmitting devices .. It has general application in the field of combustion and heat transfer, both for applications for industrial use and for domestic use.
  • NOx nitrogen oxides
  • the object of the present invention is to provide a heat generating and transmitting apparatus capable of operating with fuel in any physical state, ie fuel in the solid, liquid or gaseous state, which in turn allows reaching the desired objectives and overcoming the drawbacks of the heat generators existing in the prior art.
  • the new heat generator and transmitter apparatus comprises at least one combustion chamber of preferably tubular shape, preferably constituted by a cylinder.
  • Said cylinder is preferably divided into two sections, a lower section and another upper section of variable height. The height can be varied depending on the heat density per unit volume of the combustion flame that will be obtained in the combustion chamber.
  • the apparatus of the present invention comprises a pressurized air chamber disposed below the lower section of the cylinder that composes the combustion chamber, and a plurality of air injectors.
  • the air injectors are arranged resting on a first flat ring that forms the upper part of the pressurized air chamber and embedded in a second flat ring arranged in contact with the lower end of the cylinder forming the combustion chamber.
  • These air injectors are preferably disposed following the circular path of the flat rings, in a substantially radial direction from the center to the outside.
  • a replaceable set of parts can be arranged whose configuration is determined according to the physical state of the fuel to be used, whether solid, liquid or gaseous.
  • the second flat ring is fixed by fixing means preferably in the style of a bolt, bolt or screw arranged so that they are interposed between the air injectors.
  • the number of injectors in principle is not relevant and depends on the diameter of the cylinder that makes up the combustion chamber.
  • the minimum number of injectors necessary to obtain said rotational flow will be that which , depending on the diameter of the cylinder that makes up the combustion chamber, and with the arrangement described, resembles a circle.
  • an even number of injectors be available to ensure that the flame resulting from the combustion remains equidistant from all the points of the cylinder forming the combustion chamber.
  • the apparatus of the present invention comprises a replaceable set of parts, disposed in the free center of the flat rings, at the lower end of the lower section of the cylinder forming the combustion chamber and attached to the combustion chamber.
  • second flat ring by means of an expansion joint and whose configuration is determined by the physical state of the fuel to be used.
  • the apparatus of the present invention comprises at least one fan or a set of fans disposed below the pressurized air chamber, to supply air to the pressurized air chamber itself.
  • a preferred embodiment of the fan or set of fans also provides for the existence of a sliding sheet that is placed by closing or opening the air intake space to the fan or set of fans to regulate the air intake.
  • the two sections of the cylinder forming the combustion chamber are formed by the interposition of a third flat splitter ring.
  • the two sections of the cylinder are formed from, for example, a collapse or narrowing in the walls of the cylinder itself, adopting for example a shape similar to that of an "hourglass" will also be admissible.
  • holes for pressure relief are provided in the walls of the upper section of the cylinder forming the combustion chamber.
  • the cylinder forming the combustion chamber is complemented by a thermal insulation system composed of a series of concentric cylinders, separated by spaces through which air circulates.
  • the pressurized air chamber is constituted by a second cylinder arranged concentrically and below the lower section of the combustion chamber and whose diameter will preferably be equal to or greater than that of the combustion chamber .
  • the diameter of the second cylinder forming the air chamber under pressure is greater than that of the cylinder constituting the combustion chamber, in such a way that it coincides with a fourth concentric cylinder forming part of the thermal insulation system, as it will be explained later in the present report.
  • the pressurized air chamber supplies pressurized air to the plurality of air injectors supported on the first flat ring and the central air injector, comprised within the replaceable assembly of parts.
  • the upper part of the pressurized air chamber forms the first flat ring where the air injectors rest.
  • the first flat ring comprises, in turn, a vertical skirt whose upper part has a preferably crown-shaped finish.
  • Each air injector has
  • the lateral opening allows to inject air flows in a substantially horizontal direction, that is, air that is used for combustion.
  • the upper opening allows to inject air flows in a substantially vertical direction, that is air that has dual functionality, combustion and cooling.
  • the central air injector comprised within the replaceable set of parts, has only an upper opening that allows to inject air flow in a substantially vertical direction.
  • This flow of air in a substantially vertical direction feeds the center of the combustion chamber, that is, it injects air that is used directly for combustion.
  • the inclusion of the central air injector achieves that the central air flow has the necessary force to feed the center of the flame, since it is not only a hole through which air enters as far as it can enter, but of a pressurized air injection.
  • each air injector has, in its lateral opening, a nozzle for air outlet.
  • the nozzles serve to improve the direction of air flows within the combustion chamber.
  • the replaceable parts set will depend on the physical state of the fuel to be used, whether solid, liquid or gaseous, but in any case it comprises a central air injector arranged in the geometric center of the assembly and embedded between two flat and parallel discs that they are part of said set.
  • the replaceable set of parts in addition to comprising the central air injector, comprises a flat disk, joined to the second flat ring by means of an expansion joint, and a second flat disk supported on the first flat ring ; in such a way that the central air injector is embedded between both disks, in its geometric center.
  • a plurality of openings is provided by where pressurized air comes from the pressurized air chamber, in such a way that the incoming air by said openings when striking against the first flat disc contributes to its cooling.
  • the incoming air follows a substantially horizontal trajectory until it exits through the recesses of the crown shape of the vertical skirt. In this way, the function of this air flow in a substantially horizontal direction will be that of cooling.
  • the replaceable parts set includes, in addition:
  • the fuel injectors preferably have a lateral opening in such a way that the injection of fuel in gaseous or liquid state is carried out following a substantially horizontal direction in such a way as to contribute to the rotational sense of the air flows.
  • the fuel injectors are fed, preferably, by their lower part because the fuel distributor is arranged below them.
  • the fuel to be used is liquid
  • it is additionally arranged to place a collecting plate for liquid retention and the configuration of the fuel distributor is modified in such a way that the fuel supply travels substantially horizontally and parallel to the first flat disk before to get the fuel to the fuel injector.
  • the use of the collector plate for liquid retention is not essential, but it is convenient in the case of using fuel in a liquid state.
  • the heat generating and transmitting apparatus independently of the physical state of the fuel to be supplied, entails a thermal insulation system.
  • Said system consists of a series of cylinders concentric with the cylinder that forms the combustion chamber and will be explained in detail in the section "embodiment of the invention".
  • Materials The materials for the different component elements of the combustion chamber are preferably metallic and within these the use of stainless steel is preferred.
  • the walls inside the combustion chamber are reflective and preferably bright silvery in color, so that the return of heat radiation from the walls of the cylinder to the interior is optimized. The more reflective it is, the greater the return and the lower the heat loss.
  • the heat sink is not an integral part of the apparatus of the present invention, it is preferable that it be placed on top of the combustion chamber, leaving an air space in the middle.
  • the air in the upper part of the combustion chamber will be used as a heat insulator, when it is air in the horizontal direction, or as a heat transmitter, when it is air in the vertical direction.
  • liquid or gaseous fuel could also be used for solid fuels, for example in cases of solid fuels difficult to ignite.
  • combustion could be started with a gaseous or a liquid fuel and then passed on to the solid fuel.
  • the fuel injectors gas or liquid
  • the fuel injectors in the liquid or gaseous state are lowered until they are level with the first flat disc. Description of the combustion flame:
  • combustion flame formed by a plurality of combustion discs formed, in turn, by combustion gases, the combustion discs being separated from each other by means of air discs formed by the combustion discs.
  • air flows that are supplied for the oxidation of the fuel when the air supply is carried out in such a way that the combined action of the air flows causes a rotational air flow as described inside the combustion chamber of the apparatus of the present invention.
  • This rotational air flow gives the flame the shape of a pulsating vortex, being able to have central air zones and continuity sections between the combustion gas discs. Additionally, the combustion discs acquire a certain upward vertical velocity inside the combustion chamber, and as at a higher speed of the combustion discs there is less heat transfer to the medium, therefore as a function of the ascending vertical velocity of the combustion discs and the thickness thereof, the transfer (or loss) of heat to the medium will be greater or lesser. The same will be smaller, the thinner the combustion discs are and the higher vertical velocity ascending will be printed.
  • one or more terminations may be formed more or less elongated.
  • this new geometrical form of combustion flame manages to considerably increase the surface of the combustion flame, i.e. the oxidation surface, or area where the oxygen of the air comes into contact with the combustion flame.
  • the air supplied for the oxidation of the fuel is at very short distances from any zone inside the combustion flame and therefore maximizes the fuel efficiency. It has also been found that the described combustion flame will have a greater oxidation surface the thinner the combustion discs that make up the combustion flame.
  • Figure 1 shows a schematic of a complete longitudinal section of the generating apparatus and heat transmitter capable of operating with fuel in any physical state object of the present invention, in which the replaceable parts set (A) for fuel in gaseous state or fuel in liquid state, has been represented, but without a retention plate
  • Figure 2 shows a diagram of a longitudinal section of the heat generating and transmitting apparatus capable of operating with fuel in any physical state of the previous figure, where the replaceable set of parts (A) has been schematically represented, the system has been removed thermal insulation and the lower area of the pressurized air chamber (26) has been cut to allow more detail of the rest of the apparatuse-
  • Figures 3a, 3b and 3c respectively show a perspective view of the replaceable parts set (A) in the case of solid fuel, gaseous fuel (or liquid without holding plate (53))
  • Figure 11 shows a sectional view of the section A-A of Figure 9
  • Figure 12 shows a diagram of a longitudinal section of a specific embodiment that contemplates only the possibility of using gaseous or liquid fuels, without holding plate of the apparatus of the present invention, where the lower area of the air chamber has been cut to pressure (26) to allow more detail of the rest of the apparatus
  • Figure 13 shows a diagram of a longitudinal section similar to that of Figure 12, but for a specific embodiment that only contemplates the use for solid fuels
  • Figure 14 shows a sectional view of the section A-A of Figure 12
  • Figure 15 shows an enlarged view of Figure 14 to better see the movement of the air flows; and the injection of liquid or gaseous fuel; the references of a particular injector are numbered, but it should be understood that each air injector has a fuel injector associated
  • Figure 16 shows an alternative embodiment of Figure 15, where 14 air injectors (14) are available instead of 10 air injectors as in figure 15
  • Figure 17 shows a schematic of a longitudinal section for an alternative embodiment
  • FIG. 19 shows a sectional view of section A-
  • Figure 20 shows another sectional view of the cut
  • FIG. 1 A-A of figure 12, but with retaining plate (53);
  • Figure 21 shows a top view of the hot air flows that the heat receiver (41) will receive in the upper part of the heat generating and transmitting apparatus;
  • Figure 22 shows a diagram of at least one fan (63);
  • Figure 23 shows a diagram of the sliding sheet (55), and
  • Figure 24 shows a schematic of a combustion flame obtained inside the combustion chamber of the present invention.
  • cylinder pressure relief holes that make up the combustion chamber 22 third cylinder, concentric with the cylinder that makes up the combustion chamber
  • Figure 2 shows a general scheme of a heat generating and transmitting apparatus capable of operating with fuel in any physical state comprising:
  • a cylindrical combustion chamber 9 divided into two sections, one lower (11) and another upper section (12), the height of the lower section preferably being smaller than that of the upper section;
  • a pressurized air chamber (26) preferably constituted by a second cylinder (42), whose diameter is preferably equal to that of the cylinder forming the combustion chamber (9) and which is disposed below the lower section (11) of the combustion chamber,
  • a plurality of air injectors (14) having a lateral opening (14a) and an upper opening (14b) and which are disposed resting on a first flat ring (43) that forms the upper part of the pressurized air chamber (26) and embedded in a second flat ring (52), arranged in contact with the lower end of the first cylinder (9) that forms the combustion chamber,
  • FIG 1 a complete scheme of the apparatus of the present invention is shown, in which has represented the replaceable parts set (A), for the case of use of gaseous fuel or liquid fuel, but without holding plate.
  • an apparatus is seen comprising: • a cylindrical combustion chamber (9) divided into two sections, one lower (11) and another upper section (12),
  • a pressurized air chamber (26) constituted by a second cylinder (42), whose diameter is greater than that of the cylinder that forms the combustion chamber (9) and which is arranged below the lower section (11) of the chamber of combustion,
  • a plurality of air injectors (14) having a lateral opening (14a) and an upper opening (14b) and which are disposed resting on a first flat ring (43) that forms the upper part of the pressurized air chamber (26) and embedded in a second flat ring (52), arranged in contact with the lower end of the first cylinder (9) that makes up the combustion chamber, • a set of parts, which turns out to be the replaceable set of parts (A ) of figure 2 for the case of fuel in gaseous or liquid state without holding plate.
  • Said set of pieces is arranged in the free center of both rings (43 and 52), at the lower end of the lower section (11) and consists of:
  • the fuel distributor (30) is arranged below the fuel injectors (19); the central air injector is arranged embedded between both flat discs (13 and 44), in the geometric center thereof; the plurality of openings (16 ') arranged in circular distribution in the second flat disk (44) and around the central air injector (16).
  • the holes of the first flat disc (13) is joined to the second flat ring (52) by means of an expansion joint (54);
  • the second flat disk (44) forms the upper part of the fuel distributor (30) and rests on the first flat ring (43) and parallel to the first flat disk (13);
  • the fuel injectors (19) are disposed supported on the second flat disk (44) and passed through their corresponding holes in the first flat disk (13);
  • the fuel distributor (30) is arranged below the fuel injectors (19);
  • the central air injector is arranged embedded between both flat discs (13 and 44), in the
  • the pressurized air chamber (26) supplies pressurized air (18) to the plurality of air injectors (14) and the central air injector (16).
  • Each air injector (14) has a side opening (14a) and an upper opening (14b), of so that the lateral opening (14a) allows to inject air flows in a substantially horizontal direction (2) into the lower section (11) of the combustion chamber.
  • the upper opening (14b) allows, in turn, to inject air flows in a substantially vertical direction (15) into the lower section (11) of the combustion chamber.
  • the central air injector (16) injects an air flow in a substantially vertical direction (17) into the lower section (11) of the combustion chamber. In this way it is achieved that the combined action of all the air flows (2, 15 and 17) produces an upward rotational air flow in the lower section (11) of the cylinder (9) that forms the combustion chamber.
  • the scheme of FIG. 1 being a preferred embodiment, it also contemplates the presence of pressure relief holes (21) in the walls of the upper section (12) of the cylinder (9) that forms the combustion chamber. Also, as it is a preferred embodiment, the third flat ring (10) is shown, dividing the two sections (11 and 12) of the cylinder (9) that forms the combustion chamber.
  • the thermal insulation system composed of:
  • the apparatus of the invention preferably has a sixth flat ring (45) disposed on the upper end of the second cylinder (42) forming the pressurized air chamber (26). In said sixth flat ring (45) the fourth cylinder (28) is supported.
  • the invention provides an additional advantage in order to reduce heat losses to the medium, since the fourth cylinder (28) is displaced downwards, with respect to the area where combustion takes place and therefore both receives less heat, is better insulator and produces less heat loss to the medium.
  • Figures 3a, 3b and 3c show respectively a perspective view of the replaceable parts set (A) for the case of solid fuel, gaseous or liquid fuel without holding plate (53) and liquid fuel with holding plate (53).
  • the first flat disk (13), the central air injector (16), the expansion joint (54) and the second flat disk (44) are shown.
  • the fuel injectors (19), the fuel distributor (30) and the fuel supply pipe (29) are additionally shown.
  • the retention plate (53) of liquids is further represented and it is observed how the configuration of the fuel distributor (30) is modified, in order to allow an additional travel to the liquid, said path (20 ') being ) horizontally and parallel to the flat disk (13).
  • Said course (20 ') is not represented in this figure 3c, but will be represented in figure 9.
  • the fuel injectors (19) have a lateral opening in such a way that the injection of the fuel in the gaseous or liquid state is carried out following a substantially horizontal direction (5). In this way the fuel injection contributes to the upward rotational sense produced by the air flows (2, 15, 17) mentioned above.
  • the fuel injectors (19) are preferably fed by their lower part (20).
  • the flat disc (44) coincides with the upper part of the fuel distributor (30).
  • Figure 4 shows the pressure air chamber (26) and it is observed that it consists of: - a cylinder (42) that can be of equal or greater diameter than the cylinder (9) that composes the combustion chamber,
  • the first flat ring (43) which forms its upper part has, in its central part, holes (59) to allow the passage of air to the air injectors (14) and holes (60), of different sizes and sizes.
  • the scheme includes the thermal insulation system includes holes (61) for air supply to the space (23) of separation between the cylinder (9) which forms the combustion chamber and the third concentric cylinder (22) belonging to the thermal insulation system and orifices (62) for supplying air to the space (34) for separation between the cylinders (22 and 28) of the thermal insulation system.
  • the holes (61 and 62) being arranged in a circular distribution, following the curvature of the first flat ring (43) and in the radial direction towards the outside.
  • the lower end of the defined space (23) corresponds to a separation between the vertical skirt (51) that forms the pressurized air chamber (26) and the third cylinder (22) of the thermal insulation system and is also fed by air (18) coming from the pressurized air chamber (26) forming the air flow (24), this air flow (24) joins, in its path vertically upwards, with the air (31) flowing in substantially horizontal direction described above and together make up the air flow (32) flowing through the space (23) and directed towards the upper end of the cylinders (9 and 22), towards the outlet (33).
  • pressure relief holes (25) are provided in the third cylinder (22), aligned with the pressure relief holes (21) of the cylinder (9) forming the combustion chamber.
  • the fourth flat ring (37) at the upper edge of the cylinder (22).
  • FIG 8 Also shown in figure 8 is the space (34) of separation between the cylinders (22 and 28) of the thermal insulation system, it is also fed by air (18) coming from the pressurized air chamber (26) in such a way that through said space (34) flows an air flow (35) that is directed towards the upper end of the cylinders (22 and 28), towards an outlet (36).
  • the fourth cylinder (28) there are also provided pressure relief holes (27) aligned with the pressure relief holes (21 and 25) of the other cylinders (9 and 22).
  • the fifth flat ring (38) which is placed on the upper edge of the fourth cylinder (28) and which has on its outer edge a ring (39) which, together with the outer edge of the fourth ring plane (37) of the upper edge of the third cylinder (22) define the outlet (36).
  • the apparatus of the invention has a sixth flat ring (45) disposed on the upper end of the cylinder (42) forming the pressurized air chamber (26). Furthermore, in the sixth flat ring (45) the fourth cylinder (28) is supported, said flat ring being fixed
  • each air injector (14) is represented with a nozzle (47) to direct the air outlet, in its lateral opening (14a).
  • the fastening means are composed of fasteners (48) aided by pins (49), arranged substantially circularly on the sixth flat ring (45).
  • the preferred embodiment contemplates use as an additional safety means a pin (50), to secure the fastener union (48) and pin (49).
  • the fasteners (48) and the pins (49) described can be replaced by any conventional fixing means without altering the essence of the invention.
  • the central air injector (16) is centered and, following a radial trajectory from the center and towards the outside, where the fuel injectors are located first (19). ) distributed in a substantially circular arrangement. Continuing with this radial direction, also in substantially circular arrangement, are the air injectors (14), which are represented by each incorporating a nozzle (47) for air outlet.
  • FIGs 8, 9, 10 and 11 clearly show the expansion joint (54).
  • Figures 13, 17, 18 and 19 show concrete embodiments for the case where the apparatus only admits solid fuel and here, in these figures, shows that there is no expansion joint (54).
  • the second flat ring (52) and the first flat disk (13) of the embodiments that admitted fuel in any physical state are replaced by a single flat disk (13 '), while the first flat ring (43) and the second flat disk (44) are replaced by a single flat disk (43 ').
  • the different air injectors (14-1, 14-2, 14-3, 14-4, 14-5, 14-6, 14-7, 14-8, 14-9 and 14-10) emit the respective air flows in substantially horizontal direction (2-1, 2-2, 2-3, 2-4, 2-5, 2-6, 2-7, 2-8, 2-9 and 2-10), of such that, for example, the air flow 2-1 of the air injector 14-1 is oriented towards an intermediate position between the air injectors 14-5 and 14-6.
  • the air flow 2-2 of the air injector 14-2 is oriented towards an intermediate position between the injectors 14-6 and 14-7, and so on with each air flow of each injector. This orientation of the air flows is what causes the rotational air flow.
  • the fuel injection has been drawn gaseous or liquid (5-1, 5-2 and 5-3) in a substantially horizontal direction and contributing to the rotational sense of the air flows. Only the numerical references of the fuel injection (5-1, 5-2 and 5-3) of three of the fuel injectors have been indicated so that the figure does not lose clarity, but it is understood that each fuel injector emerges its fuel injection in a substantially horizontal direction.
  • Figure 22 shows the diagram of the air intake assembly to the pressurized air chamber (26). In said figure only one fan (63) is shown, however, as already mentioned, the invention admits a larger number of fans.
  • Figure 23 shows a sliding sheet (55) which is used to close and / or open the air intake to the fan, in this way a preferred way of regulating said intake is achieved.
  • Figure 21 shows a top view of the distribution of air flows in the upper area of the apparatus, ie at the outlet of the combustion chamber.
  • the figure represents a preferred embodiment, that is to say the one that involves the thermal insulation system formed by the two concentric cylinders (22 and 28) with the cylinder (9) that forms the combustion chamber and said structure is applicable to fuel in any state physical.
  • the central air area (6) of the last combustion disk (3) of the combustion flame towards the exterior five zones can be defined that will be at different temperatures.
  • the different zones, from the inside and towards the outside, that is to say ordered according to decreasing temperature gradient, are:
  • the heat generating and transmitting apparatus described by the present invention in any of its embodiments, provides that a heat receiver (41) is disposed thereon, at the outlet of the combustion chamber and separated by a space (40). ). Furthermore, it has been shown that the bottom of the heat receiver (41) should preferably be flat.
  • a preferred embodiment contemplates placing a mound (56) as illustrated in Figure 17 between the different concentric cylinders, to ensure the concentricity of the cylinders (9, 22 and 28) .
  • the mound (56) can be replaced by a bending (57) of the walls of the cylinders (9, 22 and 28).
  • a support (58) for the heat receiver (41) is placed.

Abstract

Device for generating and transmitting heat capable of operating with fuel in any physical state that includes at least one cylindrical combustion chamber (9) divided into a lower section (11) and an upper section (12) of variable height, a pressurized air chamber (26) arranged below the lower section (11) of the combustion chamber, and a plurality of air injectors (14). The device is characterized in that the air injectors (14) are supported on a flat ring (43) and set in a second flat ring (52) and in that it also includes a set of replaceable parts (A) arranged in the free centre of both flat rings (43 and 52) and whose specific configuration depends on the physical state of the fuel being used. Furthermore said set of replaceable parts (A) includes at least one central air injector (16) located in the geometric centre of the unit.

Description

TÍTULO DE IA INVENCIÓN TITLE OF THE INVENTION
APARATO GENERADOR Y TRANSMISOR DE CALOR CAPAZ DE FUNCIONAR CON COMBUSTIBLE EN CUALQUIER ESTADO FÍSICO Y LLAMA DEGENERATOR AND HEAT TRANSMITTER APPARATUS CAPABLE OF OPERATING WITH FUEL IN ANY PHYSICAL CONDITION AND FLAME OF
COMBUSTIÓNCOMBUSTION
OBJETO DE LA INVENCIÓNOBJECT OF THE INVENTION
La presente invención, según se expresa en el enunciado de la presente memoria descriptiva, tiene por objeto proporcionar un aparato generador y transmisor de calor capaz de funcionar con combustible en cualquier estado fisico, es decir que puede ser alimentado con combustible en estado sólido, liquido o gaseoso. A su vez, es objeto de la invención maximizar el rendimiento de la combustión, es decir que se pretende optimizar el consumo de combustible, para resultar en considerables ahorros de combustible y minimizar la emisión de contaminantes.The present invention, as expressed in the wording of the present specification, aims to provide a heat generating and transmitting apparatus capable of operating with fuel in any physical state, that is to say it can be fed with fuel in solid, liquid state or gaseous. At the same time, it is the object of the invention to maximize the combustion efficiency, that is, to optimize fuel consumption, in order to result in considerable fuel savings and minimize the emission of pollutants.
Asimismo, la presente invención tiene por objeto describir una llama de combustión generada dentro del aparato generador y transmisor de calor descrito, llama cuyas propiedades son altamente ventajosas en términos de transferencia de calor y de evitar la producción de contaminantes .Likewise, the present invention has for its object to describe a combustion flame generated within the described heat generating and transmitting apparatus, flame whose properties are highly advantageous in terms of heat transfer and to avoid the production of contaminants.
CAMPO TÉCNICO DE LA INVENCIÓNTECHNICAL FIELD OF THE INVENTION
La presente invención se engloba dentro de los métodos de obtención de energia mediante procesos de combustión, dentro de los procesos de transferencia de calor y de sus aparatos generadores y transmisores.. Tiene aplicación general en el campo de la combustión y la transferencia de calor, tanto para aplicaciones de uso industrial como para uso doméstico.The present invention is encompassed within the methods of obtaining energy through combustion processes, within the processes of heat transfer and its generating and transmitting devices .. It has general application in the field of combustion and heat transfer, both for applications for industrial use and for domestic use.
Entre las aplicaciones prácticas y concretas de la presente invención puede mencionarse su uso en el campo de la generación de vapor para calefacción o para generación de potencia eléctrica. Además entre las aplicaciones no industriales de la invención puede mencionarse su uso en calefactores, estufas, hornos, cocinas y similares.Among the practical and concrete applications of the present invention, its use in the field of steam generation for heating or power generation can be mentioned. Furthermore, among the non-industrial applications of the invention, its use in heaters, stoves, ovens, stoves and the like can be mentioned.
ESTADO DE LA TÉCNICA ANTERIOR A LA INVENCIÓN En la actualidad existen gran cantidad de aparatos generadores y transmisores de calor, cámaras de combustión cuya pretensión es obtener una combustión lo más "perfecta" o "completa" posible, para lograr ahorros en el consumo de combustible, a la vez que pretenden minimizar la generación de contaminantes.STATE OF THE ART PRIOR TO THE INVENTION There are currently a large number of heat generators and transmitters, combustion chambers whose aim is to obtain the most "perfect" or "complete" combustion possible, in order to achieve savings in fuel consumption , at the same time that they try to minimize the generation of pollutants.
Como antecedente más cercano a la presente invención, se conoce la Patente US 6.651.645 Bl que describe un aparato generador de calor para combustibles sólidos. Si bien en dicho documento se indica expresamente que el aparato descrito puede ser usado "para otros distintos tipos de combustibles como combustibles en polvo, combustibles líquidos o combustibles gaseosos", la práctica muestra que no es posible usar ninguna de las soluciones descritas en dicha patente con combustibles líquidos o gaseosos. Entre las soluciones descritas en dicho documento, ninguna describe, o sugiere un aparato que pueda funcionar con combustible liquido o gaseoso y tampoco se menciona, ni se sugiere que el mismo aparato admita combustible en cualquier estado físico (sólido, liquido o gaseoso) .As a background closer to the present invention, US Pat. No. 6,651,645 Bl describes a heat generating apparatus for solid fuels. Although said document expressly states that the apparatus described can be used "for other types of fuels such as powdered fuels, liquid fuels or gaseous fuels", practice shows that it is not possible to use any of the solutions described in said patent with liquid or gaseous fuels. Among the solutions described in said document, none describes, or suggests an apparatus that can operate with liquid or gaseous fuel and neither is it mentioned, nor is it suggested that the same apparatus admits fuel in any physical state (solid, liquid or gaseous).
Adicionalmente, el aparato generador de calor descrito en la Patente US 6.651.645 Bl presenta ciertos inconvenientes, tales como el hecho que debido a las altas temperaturas que se alcanzan dentro de la cámara de combustión, los platos o discos sustancialmente paralelos donde se encastran los inyectores de aire pandean, lo cual puede producir rotura de los mismos.Additionally, the heat generating apparatus described in US Pat. No. 6,651,645 Bl has certain drawbacks, such as the fact that due to the high temperatures that are reached inside the combustion chamber, the plates or disks are substantially parallel where the plates are embedded. Air injectors buckle, which can cause them to break.
Por lo tanto, era deseable obtener un aparato generador y transmisor de calor que: - pudiera ser utilizado con combustibles en cualquier estado físico, ya sea sólido, liquido o gaseoso, a la vez queTherefore, it was desirable to obtain a heat generating and transmitting apparatus which: - could be used with fuels in any physical state, whether solid, liquid or gaseous, at the same time as
- lograra maximizar el rendimiento de la combustión de manera que se obtengan considerables ahorros de combustible,- succeed in maximizing combustion performance so that considerable fuel savings are obtained,
- lograra transmitir la máxima cantidad del calor producido hacia el lugar de su utilización, es decir minimizando las pérdidas de calor hacia el medio, - evitara la emisión de contaminantes tales como óxidos de nitrógeno (NOx) , y- manage to transmit the maximum amount of heat produced to the place of use, ie minimizing heat losses to the environment, - avoid the emission of pollutants such as nitrogen oxides (NOx), and
- sea resistente a las altas temperaturas que se generan dentro de la cámara de combustión.- be resistant to the high temperatures that are generated inside the combustion chamber.
DESCRIPCIÓN DE IA INVENCIÓNDESCRIPTION OF THE INVENTION
La presente invención tiene por objeto proporcionar un aparato generador y transmisor de calor, capaz de funcionar con combustible en cualquier estado fisico, es decir combustible en estado sólido, liquido o gaseoso, que permita a su vez alcanzar los objetivos buscados y superar los inconvenientes de los generadores de calor existentes en la técnica anterior.The object of the present invention is to provide a heat generating and transmitting apparatus capable of operating with fuel in any physical state, ie fuel in the solid, liquid or gaseous state, which in turn allows reaching the desired objectives and overcoming the drawbacks of the heat generators existing in the prior art.
Asi, el nuevo aparato generador y transmisor de calor, objeto de la presente invención, comprende al menos una cámara de combustión de forma preferentemente tubular, constituida preferentemente por un cilindro. Dicho cilindro está dividido, preferentemente, en dos secciones, una sección inferior y otra sección superior de altura variable. La altura podrá variarse en función a la densidad de calor por unidad de volumen de la llama de combustión que se obtendrá en la cámara de combustión.Thus, the new heat generator and transmitter apparatus, object of the present invention, comprises at least one combustion chamber of preferably tubular shape, preferably constituted by a cylinder. Said cylinder is preferably divided into two sections, a lower section and another upper section of variable height. The height can be varied depending on the heat density per unit volume of the combustion flame that will be obtained in the combustion chamber.
Además el aparato de la presente invención comprende una cámara de aire a presión dispuesta debajo de la sección inferior del cilindro que compone la cámara de combustión, y una pluralidad de inyectores de aire. Los inyectores de aire se disponen apoyados sobre un primer anillo plano que conforma la parte superior de la cámara de aire a presión y encastrados en un segundo anillo plano dispuesto en contacto con el extremo inferior del cilindro que conforma la cámara de combustión. Estos inyectores de aire se disponen, preferentemente, siguiendo la trayectoria circular de los anillos planos, en dirección sustancialmente radial desde el centro hacia el exterior. El hecho de disponer los inyectores de aire apoyados sobre el primer anillo plano en lugar de encastrarlos en un disco o plato consigue las siguientes ventajas:Furthermore, the apparatus of the present invention comprises a pressurized air chamber disposed below the lower section of the cylinder that composes the combustion chamber, and a plurality of air injectors. The air injectors are arranged resting on a first flat ring that forms the upper part of the pressurized air chamber and embedded in a second flat ring arranged in contact with the lower end of the cylinder forming the combustion chamber. These air injectors are preferably disposed following the circular path of the flat rings, in a substantially radial direction from the center to the outside. The fact of arranging the air injectors supported on the first flat ring instead of being encased in a disc or plate achieves the following advantages:
- que los inyectores de aire puedan deslizar sobre el primer anillo plano, de esta manera ante las altas temperaturas que se generan dentro de la cámara de combustión y las consiguientes dilataciones que puede sufrir dicho anillo, la presencia de los inyectores no provoca su pandeo y posible rotura, y- that the air injectors can slide on the first flat ring, in this way before the high temperatures that are generated inside the combustion chamber and the consequent dilatations that the ring can suffer, the presence of the injectors does not cause its buckling and possible breakage, and
- que en el interior de los anillos planos, es decir en la zona central o libre, pueda disponerse un conjunto de piezas reemplazable cuya configuración está determinada según el estado físico del combustible a emplear, ya sea sólido, liquido o gaseoso.- that in the interior of the flat rings, that is to say in the central or free zone, a replaceable set of parts can be arranged whose configuration is determined according to the physical state of the fuel to be used, whether solid, liquid or gaseous.
El segundo anillo plano se fija mediante medios de fijación preferentemente del estilo de un perno, bulón o tornillo dispuestos de modo que estén intercalados entre los inyectores de aire.The second flat ring is fixed by fixing means preferably in the style of a bolt, bolt or screw arranged so that they are interposed between the air injectors.
El número de inyectores en principio no es relevante y depende del diámetro del cilindro que conforma la cámara de combustión. No obstante, como lo que se pretende conseguir con esta disposición particular de los inyectores de aire es un flujo rotacional a partir de la inyección de los distintos flujos de aire, asi, el número mínimo de inyectores necesario para obtener dicho flujo rotacional será aquel que, en función al diámetro del cilindro que conforma la cámara de combustión, y con la disposición descrita, se asemeje a un círculo. Así, por ejemplo se puede indicar que a partir de 6 inyectores de aire, es decir conformando un hexágono, la configuración empieza a asemejarse a un círculo. Además es preferible que se disponga de un número par de inyectores para conseguir que la llama resultante de la combustión permanezca equidistante a todos los puntos del cilindro que conforma la cámara de combustión.The number of injectors in principle is not relevant and depends on the diameter of the cylinder that makes up the combustion chamber. However, as what is intended to be achieved with this particular arrangement of the air injectors is a rotational flow from the injection of the different air flows, thus, the minimum number of injectors necessary to obtain said rotational flow will be that which , depending on the diameter of the cylinder that makes up the combustion chamber, and with the arrangement described, resembles a circle. Thus, for example, it can be indicated that from 6 air injectors, that is, forming a hexagon, the configuration begins to resemble a circle. It is also preferable that an even number of injectors be available to ensure that the flame resulting from the combustion remains equidistant from all the points of the cylinder forming the combustion chamber.
Así, como se ha indicado anteriormente, el aparato de la presente invención comprende un conjunto de piezas reemplazable, dispuesto en el centro libre de los anillos planos, en el extremo inferior de la sección inferior del cilindro que conforma la cámara de combustión y unido al segundo anillo plano por medio de una junta de dilatación y cuya configuración está determinada por el estado físico del combustible a emplear.Thus, as indicated above, the apparatus of the present invention comprises a replaceable set of parts, disposed in the free center of the flat rings, at the lower end of the lower section of the cylinder forming the combustion chamber and attached to the combustion chamber. second flat ring by means of an expansion joint and whose configuration is determined by the physical state of the fuel to be used.
Por último, el aparato de la presente invención comprende al menos un ventilador o un conjunto de ventiladores dispuesto debajo de la cámara de aire a presión, para proveer aire a la propia cámara de aire a presión. Una realización preferente del ventilador o conjunto de ventiladores prevé también la existencia de una lámina deslizante que se coloca cerrando o abriendo el espacio de admisión de aire al ventilador o conjunto de ventiladores para regular la admisión de aire.Finally, the apparatus of the present invention comprises at least one fan or a set of fans disposed below the pressurized air chamber, to supply air to the pressurized air chamber itself. A preferred embodiment of the fan or set of fans also provides for the existence of a sliding sheet that is placed by closing or opening the air intake space to the fan or set of fans to regulate the air intake.
Descripción adicional del cilindro que conforma la cámara de combustión:Additional description of the cylinder that makes up the combustion chamber:
En una realización preferente, las dos secciones del cilindro que conforma la cámara de combustión se forman mediante la interposición de un tercer anillo plano divisor. También serán admisibles realizaciones en las que las dos secciones del cilindro se formen a partir de, por ejemplo, un hundimiento o estrechamiento en las paredes del propio cilindro, adoptando por ejemplo una forma similar a la de un "reloj de arena". En una realización preferente se prevén, en las paredes de la sección superior del cilindro que conforma la cámara de combustión, agujeros para alivio de presión.In a preferred embodiment, the two sections of the cylinder forming the combustion chamber are formed by the interposition of a third flat splitter ring. Embodiments in which the two sections of the cylinder are formed from, for example, a collapse or narrowing in the walls of the cylinder itself, adopting for example a shape similar to that of an "hourglass" will also be admissible. In a preferred embodiment, holes for pressure relief are provided in the walls of the upper section of the cylinder forming the combustion chamber.
En la realización preferente, además, el cilindro que conforma la cámara de combustión se complementa con un sistema de aislamiento térmico compuesto por una serie de cilindros concéntricos, separados por espacios por donde circula aire.In the preferred embodiment, in addition, the cylinder forming the combustion chamber is complemented by a thermal insulation system composed of a series of concentric cylinders, separated by spaces through which air circulates.
Descripción de la cámara de aire a presión: La cámara de aire a presión está constituida por un segundo cilindro dispuesto de manera concéntrica y debajo de la sección inferior de la cámara de combustión y cuyo diámetro será preferentemente igual o superior al de la cámara de combustión. En la realización preferente el diámetro del segundo cilindro que conforma la cámara de aire a presión es mayor que el del cilindro que constituye la cámara de combustión, de forma tal que coincida con un cuarto cilindro concéntrico que forma parte del sistema de aislamiento térmico, como se explicará más adelante en la presente memoria .Description of the pressurized air chamber: The pressurized air chamber is constituted by a second cylinder arranged concentrically and below the lower section of the combustion chamber and whose diameter will preferably be equal to or greater than that of the combustion chamber . In the preferred embodiment, the diameter of the second cylinder forming the air chamber under pressure is greater than that of the cylinder constituting the combustion chamber, in such a way that it coincides with a fourth concentric cylinder forming part of the thermal insulation system, as it will be explained later in the present report.
La cámara de aire a presión provee aire a presión a la pluralidad de inyectores de aire apoyados en el primer anillo plano y al inyector de aire central, comprendido dentro del conjunto de piezas reemplazable.The pressurized air chamber supplies pressurized air to the plurality of air injectors supported on the first flat ring and the central air injector, comprised within the replaceable assembly of parts.
La parte superior de la cámara de aire a presión conforma el primer anillo plano donde se apoyan los inyectores de aire.The upper part of the pressurized air chamber forms the first flat ring where the air injectors rest.
El primer anillo plano comprende, a su vez, un faldón vertical cuya parte superior presenta un acabado preferentemente en forma de corona.The first flat ring comprises, in turn, a vertical skirt whose upper part has a preferably crown-shaped finish.
Descripción de los inyectores de aire:Description of the air injectors:
Cada inyector de aire poseeEach air injector has
• una apertura lateral y • una apertura superior. La apertura lateral permite inyectar flujos de aire en dirección sustancialmente horizontal, es decir, aire que se usa para la combustión. La apertura superior permite inyectar flujos de aire en dirección sustancialmente vertical, es decir aire que posee doble funcionalidad, combustión y enfriamiento.• a lateral opening and • a superior opening. The lateral opening allows to inject air flows in a substantially horizontal direction, that is, air that is used for combustion. The upper opening allows to inject air flows in a substantially vertical direction, that is air that has dual functionality, combustion and cooling.
Por otra parte el inyector de aire central, comprendido dentro del conjunto de piezas reemplazable, posee tan solo una apertura superior que permite inyectar flujo de aire en dirección sustancialmente vertical. Este flujo de aire en dirección sustancialmente vertical alimenta el centro de la cámara de combustión, es decir que inyecta aire que se usa directamente para la combustión.On the other hand, the central air injector, comprised within the replaceable set of parts, has only an upper opening that allows to inject air flow in a substantially vertical direction. This flow of air in a substantially vertical direction feeds the center of the combustion chamber, that is, it injects air that is used directly for combustion.
De esta manera se consigue que la acción combinada de los distintos flujos de aire dentro de la cámara de combustión produzca un flujo de aire rotacional.In this way it is achieved that the combined action of the different air flows inside the combustion chamber produces a rotational air flow.
La inclusión del inyector de aire central consigue que el flujo de aire central tenga la fuerza necesaria para alimentar el centro de la llama, dado que no se trata tan solo de un agujero por el cual entra aire en la medida en que puede ingresar, sino de una inyección de aire a presión .The inclusion of the central air injector achieves that the central air flow has the necessary force to feed the center of the flame, since it is not only a hole through which air enters as far as it can enter, but of a pressurized air injection.
En una realización preferente, cada inyector de aire posee, en su apertura lateral, una boquilla para salida de aire. Las boquillas sirven para mejorar el direccionamiento de los flujos de aire dentro de la cámara de combustión.In a preferred embodiment, each air injector has, in its lateral opening, a nozzle for air outlet. The nozzles serve to improve the direction of air flows within the combustion chamber.
Descripción de la estructura del conjunto de piezas reemplazable :Description of the structure of the replaceable parts set:
La configuración del conjunto de piezas reemplazable dependerá del estado físico del combustible a utilizar, ya sea sólido, liquido o gaseoso, pero en cualquier caso comprende un inyector de aire central dispuesto en el centro geométrico del conjunto y encastrado entre dos discos planos y paralelos que forman parte de dicho conjunto. Asi, en todos los casos, además de comprender el inyector de aire central, el conjunto de piezas reemplazable comprende un disco plano, unido al segundo anillo plano por medio de una junta de dilatación, y un segundo disco plano apoyado en el primer anillo plano; de forma tal que el inyector de aire central quede encastrado entre ambos discos, en su centro geométrico.The configuration of the replaceable parts set will depend on the physical state of the fuel to be used, whether solid, liquid or gaseous, but in any case it comprises a central air injector arranged in the geometric center of the assembly and embedded between two flat and parallel discs that they are part of said set. Thus, in all cases, in addition to comprising the central air injector, the replaceable set of parts comprises a flat disk, joined to the second flat ring by means of an expansion joint, and a second flat disk supported on the first flat ring ; in such a way that the central air injector is embedded between both disks, in its geometric center.
Además, en el centro geométrico del segundo disco plano, alrededor y concéntrico con el inyector de aire central, se prevé una pluralidad de aperturas por donde ingresa aire a presión proveniente de la cámara de aire a presión, de tal modo que el aire que ingresa por dichas aperturas al incidir contra el primer disco plano contribuya a su enfriamiento. Además, y debido al acabado en forma de corona de la parte superior del faldón vertical, el aire que ingresa sigue con una trayectoria sustancialmente horizontal hasta salir fuera por los rebajes de la forma de corona del faldón vertical. De esta manera, la función de este flujo de aire en dirección sustancialmente horizontal será la de enfriamiento.In addition, in the geometrical center of the second flat disk, around and concentric with the central air injector, a plurality of openings is provided by where pressurized air comes from the pressurized air chamber, in such a way that the incoming air by said openings when striking against the first flat disc contributes to its cooling. In addition, and due to the crown-like finish of the upper part of the vertical skirt, the incoming air follows a substantially horizontal trajectory until it exits through the recesses of the crown shape of the vertical skirt. In this way, the function of this air flow in a substantially horizontal direction will be that of cooling.
Para combustibles en estado gaseoso o liquido, el conjunto de piezas reemplazable comprende, además:For fuels in gaseous or liquid state, the replaceable parts set includes, in addition:
- una pluralidad de inyectores de combustible dispuestos apoyados sobre el segundo disco plano y encastrados en el primer disco plano, distribuidos siguiendo, preferentemente, la trayectoria circular de los discos,- a plurality of fuel injectors disposed resting on the second flat disk and embedded in the first flat disk, distributed preferably following the circular path of the discs,
- un distribuidor de combustible, dispuesto debajo de los inyectores de combustible y cuya parte superior conforma el segundo disco plano, y- a fuel distributor, arranged below the fuel injectors and whose upper part forms the second flat disk, and
- un tubo de alimentación de combustible que alimenta el distribuidor de combustible.- a fuel supply pipe that feeds the fuel distributor.
Los inyectores de combustible poseen, preferentemente, una apertura lateral de tal manera que la inyección de combustible en estado gaseoso o liquido se realice siguiendo una dirección sustancialmente horizontal de forma tal que contribuya al sentido rotacional de los flujos de aire .The fuel injectors preferably have a lateral opening in such a way that the injection of fuel in gaseous or liquid state is carried out following a substantially horizontal direction in such a way as to contribute to the rotational sense of the air flows.
Además, los inyectores de combustible son alimentados, preferentemente, por su parte inferior gracias a que el distribuidor de combustible se encuentra dispuesto debajo de los mismos.In addition, the fuel injectors are fed, preferably, by their lower part because the fuel distributor is arranged below them.
Cuando el combustible a emplear es liquido, se dispone adicionalmente la colocación de un plato recogedor para retención del liquido y se modifica la configuración del distribuidor de combustible de forma tal que la alimentación de combustible realice un recorrido sustancialmente horizontal y paralelo al primer disco plano antes de llegar el combustible al inyector de combustible. La utilización del plato recogedor para retención del liquido no es indispensable, pero si conveniente para el caso de emplear combustible en estado liquido.When the fuel to be used is liquid, it is additionally arranged to place a collecting plate for liquid retention and the configuration of the fuel distributor is modified in such a way that the fuel supply travels substantially horizontally and parallel to the first flat disk before to get the fuel to the fuel injector. The use of the collector plate for liquid retention is not essential, but it is convenient in the case of using fuel in a liquid state.
En una realización preferente, el aparato generador y transmisor de calor, independientemente del estado físico del combustible a suministrar, conlleva un sistema de aislamiento térmico. Dicho sistema consta de una serie de cilindros concéntricos con el cilindro que conforma la cámara de combustión y será explicado en detalle en la sección "forma de realización de la invención". Materiales : Los materiales para los distintos elementos componentes de la cámara de combustión son preferentemente metálicos y dentro de éstos es preferente el uso de acero inoxidable. Asimismo, en la realización preferente las paredes del interior de la cámara de combustión son reflectantes y preferentemente de color plateado brillante, de manera que se optimiza el retorno de la radiación del calor desde las paredes del cilindro al interior. Cuanto más reflectante sea, mayor será el retorno y menor será la pérdida de calor. Cabe destacar que, si bien el receptor de calor no forma parte integral del aparato de la presente invención, es preferible que él mismo sea colocado encima de la cámara de combustión dejando un espacio de aire en el medio. El aire en la parte superior de la cámara de combustión se usará como aislante de calor, cuando sea aire en dirección horizontal, o como transmisor de calor, cuando sea aire en dirección vertical.In a preferred embodiment, the heat generating and transmitting apparatus, independently of the physical state of the fuel to be supplied, entails a thermal insulation system. Said system consists of a series of cylinders concentric with the cylinder that forms the combustion chamber and will be explained in detail in the section "embodiment of the invention". Materials: The materials for the different component elements of the combustion chamber are preferably metallic and within these the use of stainless steel is preferred. Also, in the preferred embodiment, the walls inside the combustion chamber are reflective and preferably bright silvery in color, so that the return of heat radiation from the walls of the cylinder to the interior is optimized. The more reflective it is, the greater the return and the lower the heat loss. It should be noted that, although the heat sink is not an integral part of the apparatus of the present invention, it is preferable that it be placed on top of the combustion chamber, leaving an air space in the middle. The air in the upper part of the combustion chamber will be used as a heat insulator, when it is air in the horizontal direction, or as a heat transmitter, when it is air in the vertical direction.
Además, es destacable que las realizaciones que se describen para combustible liquido o gaseoso podrían ser empleadas también para combustibles sólidos, por ejemplo en casos de combustibles sólidos de difícil ignición. Asi se podria comenzar la combustión con un combustible gaseoso o uno liquido y posteriormente se pasarla al combustible sólido. En estos casos, los inyectores de combustible (gas o liquido) incluirán, además, una tapadera. 0 alternativamente, los inyectores de combustible en estado liquido o gaseoso se hacen descender hasta quedar a nivel con el primer disco plano. Descripción de la llama de combustión:In addition, it is noteworthy that the embodiments described for liquid or gaseous fuel could also be used for solid fuels, for example in cases of solid fuels difficult to ignite. Thus combustion could be started with a gaseous or a liquid fuel and then passed on to the solid fuel. In these cases, the fuel injectors (gas or liquid) will also include a cover. Alternatively, the fuel injectors in the liquid or gaseous state are lowered until they are level with the first flat disc. Description of the combustion flame:
Por último, dentro del aparato generador y transmisor de calor descrito por la presente invención se genera una llama de combustión de forma geométrica y características técnicas ventajosas en lo referente a rendimiento del combustible y emisión de contaminantes.Finally, within the heat generator and transmitter apparatus described by the present invention, a combustion flame of geometric shape and advantageous technical characteristics are generated in terms of fuel efficiency and emission of contaminants.
Asi, es también un objeto de la presente invención dicha llama de combustión formada por una pluralidad de discos de combustión formados, a su vez, por gases de combustión, estando los discos de combustión separados entre si por medio de discos de aire formados por los flujos de aire que se suministran para la oxidación del combustible cuando el suministro de aire se realiza de manera tal que la acción combinada de los flujos de aire provoque un flujo de aire rotacional como el descrito dentro de la cámara de combustión del aparato de la presente invención.Thus, it is also an object of the present invention said combustion flame formed by a plurality of combustion discs formed, in turn, by combustion gases, the combustion discs being separated from each other by means of air discs formed by the combustion discs. air flows that are supplied for the oxidation of the fuel when the air supply is carried out in such a way that the combined action of the air flows causes a rotational air flow as described inside the combustion chamber of the apparatus of the present invention.
Dicho flujo de aire rotacional confiere a la llama la forma de un vórtice pulsante, pudiendo tener zonas centrales de aire y secciones de continuidad entre los discos de gases de combustión. Adicionalmente, los discos de combustión adquieren una cierta velocidad vertical ascendente dentro de la cámara de combustión, y como a una mayor velocidad de los discos de combustión se produce una menor transferencia de calor al medio, por lo tanto en función de la velocidad vertical ascendente de los discos de combustión y del espesor de los mismos, será mayor o menor la transferencia (o pérdida) de calor al medio. La misma será menor, cuanto más delgados sean los discos de combustión y cuanta mayor velocidad vertical ascendente se les imprima.This rotational air flow gives the flame the shape of a pulsating vortex, being able to have central air zones and continuity sections between the combustion gas discs. Additionally, the combustion discs acquire a certain upward vertical velocity inside the combustion chamber, and as at a higher speed of the combustion discs there is less heat transfer to the medium, therefore as a function of the ascending vertical velocity of the combustion discs and the thickness thereof, the transfer (or loss) of heat to the medium will be greater or lesser. The same will be smaller, the thinner the combustion discs are and the higher vertical velocity ascending will be printed.
Adicionalmente, en el extremo superior de la llama de combustión se pueden formar una o más terminaciones de forma más o menos alargada. Asi esta nueva forma geométrica de llama de combustión consigue aumentar considerablemente la superficie de la llama de combustión, es decir la superficie de oxidación, o zona donde el oxigeno del aire se pone en contacto con la llama de combustión. Además, con esta forma de llama de combustión se consigue que el aire suministrado para la oxidación del combustible se encuentre a distancias muy cortas de cualquier zona del interior de la llama de combustión y por lo tanto se consigue maximizar el rendimiento del combustible. También se ha comprobado que la llama de combustión descrita tendrá mayor superficie de oxidación cuanto más delgados sean los discos de combustión que integran la llama de combustión.Additionally, at the upper end of the combustion flame one or more terminations may be formed more or less elongated. Thus this new geometrical form of combustion flame manages to considerably increase the surface of the combustion flame, i.e. the oxidation surface, or area where the oxygen of the air comes into contact with the combustion flame. Furthermore, with this form of combustion flame it is achieved that the air supplied for the oxidation of the fuel is at very short distances from any zone inside the combustion flame and therefore maximizes the fuel efficiency. It has also been found that the described combustion flame will have a greater oxidation surface the thinner the combustion discs that make up the combustion flame.
BREVE DESCRIPCIÓN DE LAS FIGURAS La presente invención será completamente comprendida sobre la base de la breve descripción que figura a continuación y de los dibujos acompañantes que se presentan, solamente a modo de ejemplo y, de esta manera, no son restrictivos dentro de la presente invención y donde : la figura 1 muestra un esquema de un corte longitudinal completo del aparato generador y transmisor de calor capaz de funcionar con combustible en cualquier estado físico objeto de la presente invención, en el cual se ha representado el conjunto de piezas reemplazable (A) para combustible en estado gaseoso o combustible en estado liquido, pero sin plato de retención; la figura 2 muestra un esquema de un corte longitudinal del aparato generador y transmisor de calor capaz de funcionar con combustible en cualquier estado físico de la figura anterior, donde se ha representado esquemáticamente el conjunto de piezas reemplazable (A) , se ha quitado el sistema de aislamiento térmico y se ha cortado la zona inferior de la cámara de aire a presión (26) para permitir mayor detalle del resto del aparate- las figuras 3a, 3b y 3c muestran respectivamente una vista en perspectiva del conjunto de piezas reemplazable (A) para el caso de combustible sólido, combustible gaseoso (o liquido sin plato de retención (53) ) y combustible liquido con plato de retención (53); la figura 4 muestra una vista en perspectiva de la cámara de aire a presión (26) ; la figura 5 muestra una vista lateral de la cámara de aire a presión (26) ; la figura 6 muestra una vista desde arriba de la cámara de aire a presión (26) ; las figura 7a, 7b y 7c muestran respectivamente una vista desde arriba de la cámara de aire a presión (26) con el conjunto de piezas reemplazable (A) de las figuras 3a, 3b y 3c respectivamente; Ia figura 8 muestra un esquema de un corte longitudinal del aparato generador y transmisor de calor capaz de funcionar con combustible en cualquier estado físico de la figura anterior, en donde se ha cortado la zona inferior de la cámara de aire a presión (26) para permitir mayor detalle del resto del aparato y en el cual se ha representado el conjunto de piezas reemplazable (A) , descrito en la figura 3b, para uso de combustible gaseoso o liquido sin plato de retención (53) ; la figura 9 muestra un esquema de un corte longitudinal similar al de la figura 8, pero en el cual se ha representado el conjunto de piezas reemplazable (A) , descrito en la figura 3c, para uso de combustible líquido con plato de retención (53); la figura 10 muestra un esquema de un corte longitudinal similar al de la figura 8, pero en el cual se ha representado el conjunto de piezas reemplazable (A) , descrito en la figura 3a, para uso de combustible sólido;BRIEF DESCRIPTION OF THE FIGURES The present invention will be completely understood on the basis of the brief description that follows and the accompanying drawings that are presented, by way of example only and, thus, are not restrictive within the present invention and where: Figure 1 shows a schematic of a complete longitudinal section of the generating apparatus and heat transmitter capable of operating with fuel in any physical state object of the present invention, in which the replaceable parts set (A) for fuel in gaseous state or fuel in liquid state, has been represented, but without a retention plate; Figure 2 shows a diagram of a longitudinal section of the heat generating and transmitting apparatus capable of operating with fuel in any physical state of the previous figure, where the replaceable set of parts (A) has been schematically represented, the system has been removed thermal insulation and the lower area of the pressurized air chamber (26) has been cut to allow more detail of the rest of the aparate- Figures 3a, 3b and 3c respectively show a perspective view of the replaceable parts set (A) in the case of solid fuel, gaseous fuel (or liquid without holding plate (53)) and liquid fuel with holding plate (53); Figure 4 shows a perspective view of the pressurized air chamber (26); Figure 5 shows a side view of the pressurized air chamber (26); Figure 6 shows a top view of the pressurized air chamber (26); Figures 7a, 7b and 7c respectively show a top view of the pressurized air chamber (26) with the replaceable parts set (A) of Figures 3a, 3b and 3c respectively; Figure 8 shows a diagram of a longitudinal section of the heat generating and transmitting apparatus capable of operating with fuel in any physical state of the previous figure, where the lower area of the pressurized air chamber (26) has been cut for allowing greater detail of the rest of the apparatus and in which the replaceable assembly of parts (A), described in Figure 3b, has been represented for use of gaseous or liquid fuel without holding plate (53); figure 9 shows a diagram of a longitudinal section similar to that of figure 8, but in which the replaceable parts set (A), described in figure 3c, has been represented for use of liquid fuel with holding plate (53) ); figure 10 shows a diagram of a longitudinal section similar to that of figure 8, but in which the replaceable assembly of parts (A), described in figure 3a, has been represented for the use of solid fuel;
La figura 11 muestra una vista en sección del corte A- A de la figura 9; la figura 12 muestra un esquema de un corte longitudinal de una realización concreta que contempla sólo la posibilidad de usar combustibles gaseosos o líquidos, sin plato de retención del aparato de la presente invención, donde se ha cortado la zona inferior de la cámara de aire a presión (26) para permitir mayor detalle del resto del aparato; la figura 13 muestra un esquema de un corte longitudinal similar al de la figura 12, pero para una realización concreta que sólo contempla el uso para combustibles sólidos; la figura 14 muestra una vista en sección del corte A- A de la figura 12; la figura 15 muestra una vista ampliada de la figura 14 para ver mejor el movimiento de los flujos de aire; y la inyección de combustible líquido o gaseoso; se numeran las referencias de un inyector concreto, pero se debe entender que cada inyector de aire lleva asociado un inyector de combustible, la figura 16 muestra una realización alternativa de la figura 15, donde se dispone de 14 inyectores de aire (14) en lugar de 10 inyectores de aire como en la figura 15; la figura 17 muestra un esquema de un corte longitudinal para una realización alternativa de la figura 13, y en el detalle se muestra una realización alternativa del montículo (56) descrito y que es realizar un dobladoFigure 11 shows a sectional view of the section A-A of Figure 9; Figure 12 shows a diagram of a longitudinal section of a specific embodiment that contemplates only the possibility of using gaseous or liquid fuels, without holding plate of the apparatus of the present invention, where the lower area of the air chamber has been cut to pressure (26) to allow more detail of the rest of the apparatus; Figure 13 shows a diagram of a longitudinal section similar to that of Figure 12, but for a specific embodiment that only contemplates the use for solid fuels; Figure 14 shows a sectional view of the section A-A of Figure 12; Figure 15 shows an enlarged view of Figure 14 to better see the movement of the air flows; and the injection of liquid or gaseous fuel; the references of a particular injector are numbered, but it should be understood that each air injector has a fuel injector associated, Figure 16 shows an alternative embodiment of Figure 15, where 14 air injectors (14) are available instead of 10 air injectors as in figure 15; Figure 17 shows a schematic of a longitudinal section for an alternative embodiment of Figure 13, and in the detail there is shown an alternative embodiment of the mound (56) described and that is to perform a bending
(57) en las paredes de los cilindros concéntricos; la figura 18 muestra una vista en sección del corte A-(57) on the walls of the concentric cylinders; Figure 18 shows a sectional view of the section A-
A de la figura 13; la figura 19 muestra una vista en sección del corte A-A of figure 13; Figure 19 shows a sectional view of section A-
A de la figura 17; la figura 20 muestra otra vista en sección del corteA of figure 17; Figure 20 shows another sectional view of the cut
A-A de la figura 12, pero con plato de retención (53); la figura 21 muestra una vista superior de los flujos de aire caliente que recibirá el receptor de calor (41) en la parte superior del aparato generador y transmisor de calor; la figura 22 muestra un esquema de, al menos, un ventilador (63); la figura 23 muestra un esquema de la lámina deslizante (55), y la figura 24 muestra un esquema de una llama de combustión obtenida dentro de la cámara de combustión de la presente invención. En estas figuras aparecen unas referencias numéricas asociadas a los siguientes elementos:A-A of figure 12, but with retaining plate (53); Figure 21 shows a top view of the hot air flows that the heat receiver (41) will receive in the upper part of the heat generating and transmitting apparatus; Figure 22 shows a diagram of at least one fan (63); Figure 23 shows a diagram of the sliding sheet (55), and Figure 24 shows a schematic of a combustion flame obtained inside the combustion chamber of the present invention. In these figures there are numerical references associated with the following elements:
A: conjunto de piezas reemplazableA: replaceable parts set
2: flujos de aire en dirección sustancialmente horizontal emergentes de los inyectores de aire 3: discos de combustión de la llama de combustión discos de aire de la llama de combustión inyección de combustible gaseoso o liquido zona central de aire de la llama de combustión secciones de continuidad de la llama de combustión terminaciones de la llama de combustión primer cilindro, que conforma la cámara de combustión2: substantially horizontal air flows emerging from the air injectors 3: combustion flame combustion discs combustion flame air discs gaseous or liquid fuel injection central air zone of the combustion flame continuity sections of the combustion flame ends of the combustion flame first cylinder, which forms the combustion chamber
10: tercer anillo plano, divisor de las dos secciones de la cámara de combustión10: third flat ring, divider of the two sections of the combustion chamber
11: sección inferior del cilindro que conforma la cámara de combustión11: lower section of the cylinder that makes up the combustion chamber
12: sección superior del cilindro que conforma la cámara de combustión12: upper section of the cylinder that makes up the combustion chamber
13: primer disco plano13: first flat disk
13' : disco plano para realizaciones concretas donde el aparato solo admite combustible en un estado fisico, definido en el momento de su construcción13 ': flat disc for specific embodiments where the device only admits fuel in a physical state, defined at the time of its construction
14: inyectores de aire14: air injectors
14a: apertura lateral de los inyectores de aire14a: lateral opening of the air injectors
14b: apertura superior de los inyectores de aire 15: flujos de aire en dirección sustancialmente vertical emergentes de los inyectores de aire14b: upper opening of the air injectors 15: air flows in a substantially vertical direction emerging from the air injectors
16: inyector de aire central16: central air injector
16' : pluralidad de aperturas alrededor del inyector de aire central 17: flujo de aire en dirección sustancialmente vertical emergente del inyector de aire central16 ': plurality of openings around the central air injector 17: airflow in substantially vertical direction emerging from the central air injector
18: aire a presión proveniente de la cámara de aire a presión18: pressurized air from the pressurized air chamber
19: inyectores de combustible 20: alimentación de combustible liquido o gaseoso19: fuel injectors 20: liquid or gaseous fuel feed
20' : recorrido sustancialmente horizontal de la alimentación de combustible liquido20 ': substantially horizontal route of the liquid fuel feed
21: agujeros de alivio de presión del cilindro que conforma la cámara de combustión 22: tercer cilindro, concéntrico con el cilindro que conforma la cámara de combustión21: cylinder pressure relief holes that make up the combustion chamber 22: third cylinder, concentric with the cylinder that makes up the combustion chamber
23: espacio de separación entre el cilindro que conforma la cámara de combustión y el tercer cilindro 24: flujo de aire que circula por el extremo inferior del espacio (23) de separación entre el cilindro que conforma la cámara de combustión y el tercer cilindro, es decir el espacio definido entre el faldón vertical (51) que conforma la cámara de aire a presión (26) y el tercer cilindro (22) 25: agujeros de alivio de presión del tercer cilindro23: separation space between the cylinder forming the combustion chamber and the third cylinder 24: air flow circulating through the lower end of the space (23) of separation between the cylinder forming the combustion chamber and the third cylinder, that is, the space defined between the vertical skirt (51) that makes up the air chamber under pressure (26) and the third cylinder (22) 25: pressure relief holes of the third cylinder
26: cámara de aire a presión26: pressurized air chamber
27: agujeros de alivio de presión del cuarto cilindro27: fourth cylinder pressure relief holes
28: cuarto cilindro, concéntrico con los anteriores (9 y28: fourth cylinder, concentric with the previous ones (9 and
22) 29: tubo alimentador de combustible22) 29: fuel feeder tube
30: distribuidor de combustible30: fuel distributor
31: flujo de aire en dirección sustancialmente horizontal que emerge por los rebajes que conforman la corona del faldón vertical 32: flujo de aire que circula por el espacio de separación entre el cilindro que conforma la cámara de combustión y el tercer cilindro31: air flow in a substantially horizontal direction emerging from the recesses forming the crown of the vertical skirt 32: air flow through the space between the cylinder forming the combustion chamber and the third cylinder
33: salida o extremo superior del espacio de separación entre el cilindro que conforma la cámara de combustión y el tercer cilindro33: outlet or upper end of the gap between the cylinder that makes up the combustion chamber and the third cylinder
34: espacio de separación entre el tercer y cuarto cilindro34: space between the third and fourth cylinder
35: flujo de aire que circula por el espacio de separación entre el tercer y cuarto cilindro35: air flow circulating in the space between the third and fourth cylinder
36: salida o extremo superior del espacio de separación entre el tercer y cuarto cilindro36: exit or upper end of the separation space between the third and fourth cylinder
37: cuarto anillo plano del borde superior del tercer cilindro37: fourth flat ring of the upper edge of the third cylinder
38: quinto anillo plano del borde superior del cuarto cilindro 39: aro que posee en su borde exterior el quinto anillo plano del borde superior del cuarto cilindro38: fifth flat ring of the upper edge of the fourth cylinder 39: ring that has on its outer edge the fifth flat ring of the upper edge of the fourth cylinder
40: espacio de separación entre el aparato generador y transmisor de calor y un receptor de calor40: separation space between the generator and heat transmitter and a heat sink
41: receptor de calor41: heat sink
42: segundo cilindro, que constituye la cámara de aire a presión42: second cylinder, which constitutes the pressurized air chamber
43: primer anillo plano donde apoyan los inyectores de aire43: first flat ring where the air injectors support
43' : disco plano para realizaciones concretas donde el aparato solo admite combustible en un estado fisico, definido en el momento de su construcción43 ': flat disk for specific embodiments where the device only admits fuel in a physical state, defined at the time of its construction
44: segundo disco plano del distribuidor de combustible44: second flat disc of the fuel distributor
45: sexto anillo plano en el que se apoya el extremo inferior del cilindro más externo, concéntrico con el cilindro que conforma la cámara de combustión45: sixth flat ring on which the lower end of the outermost cylinder rests, concentric with the cylinder that makes up the combustion chamber
46 medios de fijación 47 boquilla para aire 48 sujetadores 49 clavijas 50 pasador 51 faldón vertical con acabado en forma de corona 52 segundo anillo plano en contacto con el extremo inferior del cilindro que conforma la cámara de combustión46 fastening means 47 air nozzle 48 fasteners 49 dowels 50 pin 51 vertical skirt with crown-shaped finish 52 second flat ring in contact with the lower end of the cylinder forming the combustion chamber
53 plato de retención del combustible liquido53 liquid fuel holding plate
54: junta o ranura de dilatación 55: lámina deslizante 56: montículo 57 : doblado54: expansion joint or groove 55: sliding plate 56: mound 57: folded
58: soporte para receptor de calor58: support for heat sink
59: orificios para permitir la alimentación de aire a los inyectores de aire59: holes to allow air supply to the air injectors
60: orificios para fijación del segundo anillo plano (52) 61: orificio para alimentación de aire al espacio (23) de separación entre el cilindro (9) que conforma la cámara de combustión y el tercer cilindro (22) 62: orificio para alimentación de aire al espacio (34) de separación entre el tercer y cuarto cilindro (22 y 28) 63: ventilador para presurizar el aire en la cámara de aire a presión (26) . FORMA DE REALIZACIÓN DE LA INVENCIÓN60: holes for fixing the second flat ring (52) 61: hole for supply of air to the gap (23) between the cylinder (9) that makes up the combustion chamber and the third cylinder (22) 62: hole for air supply to the space (34) of separation between the third and fourth cylinder (22 and 28) 63: fan for pressurizing the air in the pressurized air chamber (26). FORM OF EMBODIMENT OF THE INVENTION
Con el objeto de llegar a una mejor comprensión del objeto y funcionalidad de esta patente, y sin que se entienda como soluciones restrictivas.In order to reach a better understanding of the object and functionality of this patent, and without being understood as restrictive solutions.
En la figura 2 se muestra un esquema general de un aparato generador y transmisor de calor capaz de funcionar con combustible en cualquier estado físico que comprende:Figure 2 shows a general scheme of a heat generating and transmitting apparatus capable of operating with fuel in any physical state comprising:
• una cámara de combustión cilindrica (9) dividida en dos secciones, una inferior (11) y otra sección superior (12), siendo preferentemente la altura de la sección inferior menor que la de las sección superior;• a cylindrical combustion chamber (9) divided into two sections, one lower (11) and another upper section (12), the height of the lower section preferably being smaller than that of the upper section;
• una cámara de aire a presión (26) constituida preferentemente por un segundo cilindro (42), cuyo diámetro es preferentemente igual al del cilindro que conforma la cámara de combustión (9) y que se dispone debajo de la sección inferior (11) de la cámara de combustión,• a pressurized air chamber (26) preferably constituted by a second cylinder (42), whose diameter is preferably equal to that of the cylinder forming the combustion chamber (9) and which is disposed below the lower section (11) of the combustion chamber,
• una pluralidad de inyectores de aire (14) que poseen una apertura lateral (14a) y una apertura superior (14b) y que se disponen apoyados sobre un primer anillo plano (43) que conforma la parte superior de la cámara de aire a presión (26) y encastrados en un segundo anillo plano (52), dispuesto en contacto con el extremo inferior del primer cilindro (9) que conforma la cámara de combustión,• a plurality of air injectors (14) having a lateral opening (14a) and an upper opening (14b) and which are disposed resting on a first flat ring (43) that forms the upper part of the pressurized air chamber (26) and embedded in a second flat ring (52), arranged in contact with the lower end of the first cylinder (9) that forms the combustion chamber,
• un conjunto de piezas reemplazable (A) dispuesto en el centro libre de ambos anillos (43 y 52), y • al menos un ventilador, que no se ve en la figura 2, puesto que se ha quitado la zona inferior de la cámara de aire a presión (26) para permitir mayor detalle del resto del aparato.• a replaceable set of parts (A) arranged in the free center of both rings (43 and 52), and • at least one fan, which is not seen in figure 2, since the lower area of the chamber has been removed of pressurized air (26) to allow more detail of the rest of the device.
En la figura 1, como ya se ha indicado, se muestra un esquema completo del aparato de la presente invención, en el cual se ha representado el conjunto de piezas reemplazable (A) , para el caso de uso de combustible gaseoso o combustible liquido, pero sin plato de retención. Asi, se ve un aparato que comprende: • una cámara de combustión cilindrica (9) dividida en dos secciones, una inferior (11) y otra sección superior (12),In figure 1, as already indicated, a complete scheme of the apparatus of the present invention is shown, in which has represented the replaceable parts set (A), for the case of use of gaseous fuel or liquid fuel, but without holding plate. Thus, an apparatus is seen comprising: • a cylindrical combustion chamber (9) divided into two sections, one lower (11) and another upper section (12),
• una cámara de aire a presión (26) constituida por un segundo cilindro (42), cuyo diámetro es mayor al del cilindro que conforma la cámara de combustión (9) y que se dispone debajo de la sección inferior (11) de la cámara de combustión,• a pressurized air chamber (26) constituted by a second cylinder (42), whose diameter is greater than that of the cylinder that forms the combustion chamber (9) and which is arranged below the lower section (11) of the chamber of combustion,
• una pluralidad de inyectores de aire (14) que poseen una apertura lateral (14a) y una apertura superior (14b) y que se disponen apoyados sobre un primer anillo plano (43) que conforma la parte superior de la cámara de aire a presión (26) y encastrados en un segundo anillo plano (52), dispuesto en contacto con el extremo inferior del primer cilindro (9) que conforma la cámara de combustión, • un conjunto de piezas, que resulta ser el conjunto de piezas reemplazable (A) de la figura 2 para el caso de combustible en estado gaseoso o liquido sin plato de retención. Dicho conjunto de piezas está dispuesto en el centro libre de ambos anillos (43 y 52), en el extremo inferior de la sección inferior (11) y se compone de:• a plurality of air injectors (14) having a lateral opening (14a) and an upper opening (14b) and which are disposed resting on a first flat ring (43) that forms the upper part of the pressurized air chamber (26) and embedded in a second flat ring (52), arranged in contact with the lower end of the first cylinder (9) that makes up the combustion chamber, • a set of parts, which turns out to be the replaceable set of parts (A ) of figure 2 for the case of fuel in gaseous or liquid state without holding plate. Said set of pieces is arranged in the free center of both rings (43 and 52), at the lower end of the lower section (11) and consists of:
- un primer disco plano (13), un segundo disco plano (44),- a first flat disk (13), a second flat disk (44),
- un inyector de aire central (16),- a central air injector (16),
- una pluralidad de inyectores de combustible (19), - un distribuidor de combustible (30),- a plurality of fuel injectors (19), - a fuel distributor (30),
- un tubo de alimentación de combustible (29) del distribuidor de combustible (30) , y una pluralidad de aperturas (16' ), alrededor del inyector de aire central (16) de forma tal que, el primer disco plano (13) se une al segundo anillo plano (52) por medio de una junta de dilatación (54); el segundo disco plano (44) conforma la parte superior del distribuidor de combustible (30) y se apoya en el primer anillo plano (43) y paralelo al primer disco plano (13); los inyectores de combustible (19) se disponen apoyados en el segundo disco plano (44) y pasados a través de sus correspondientes orificios en el primer disco plano (13); el distribuidor de combustible (30) se dispone debajo de los inyectores de combustible (19); el inyector de aire central se dispone encastrado entre ambos discos planos (13 y 44), en el centro geométrico de los mismos; la pluralidad de aperturas (16') dispuestas en distribución circular en el segundo disco plano (44) y alrededor del inyector de aire central (16) . El tubo de alimentación de combustible (29) si bien está ubicado, preferentemente, en un lateral del distribuidor de combustible (30) podría admitir cualquier ubicación que permita el ingreso de combustible en el distribuidor de combustible (30) . Además, los orificios del primer disco plano (13) por donde pasan los inyectores de combustible- a fuel supply pipe (29) of the fuel distributor (30), and a plurality of openings (16 '), around the central air injector (16) in such a way that the first flat disk (13) is joined to the second flat ring (52) by means of an expansion joint (54); the second flat disk (44) forms the upper part of the fuel distributor (30) and rests on the first flat ring (43) and parallel to the first flat disk (13); the fuel injectors (19) are disposed supported on the second flat disk (44) and passed through their corresponding holes in the first flat disk (13); the fuel distributor (30) is arranged below the fuel injectors (19); the central air injector is arranged embedded between both flat discs (13 and 44), in the geometric center thereof; the plurality of openings (16 ') arranged in circular distribution in the second flat disk (44) and around the central air injector (16). The fuel supply pipe (29), although it is preferably located on one side of the fuel distributor (30) could admit any location that allows fuel to enter the fuel distributor (30). In addition, the holes of the first flat disc (13) through which the fuel injectors pass
(19) poseen un diámetro ligeramente mayor que el diámetro de los inyectores de combustible (19) de forma tal de permitir la dilatación del disco plano (13) que se produce por las altas temperaturas que se generan dentro de la cámara de combustión.(19) have a diameter slightly larger than the diameter of the fuel injectors (19) in order to allow the expansion of the flat disk (13) that is produced by the high temperatures that are generated inside the combustion chamber.
Además, en la figura 1, se representa al menos un ventilador (63) ubicado debajo de la zona inferior de la cámara de aire a presión (26) . En la figura 1 también se representan algunas flechas que indican el sentido de los flujos de aire. Asi, la cámara de aire a presión (26), provee aire a presión (18) a la pluralidad de inyectores de aire (14) y al inyector de aire central (16) . Cada inyector de aire (14) posee una apertura lateral (14a) y una apertura superior (14b), de modo que la apertura lateral (14a) permita inyectar flujos de aire en dirección sustancialmente horizontal (2) al interior de la sección inferior (11) de la cámara de combustión. La apertura superior (14b) permite, a su vez, inyectar flujos de aire en dirección sustancialmente vertical (15) al interior de la sección inferior (11) de la cámara de combustión. Y el inyector de aire central (16) inyecta un flujo de aire en dirección sustancialmente vertical (17) al interior de la sección inferior (11) de la cámara de combustión. De esta manera se consigue que la acción combinada de todos los flujos de aire (2, 15 y 17) produzca un flujo de aire rotacional ascendente en la sección inferior (11) del cilindro (9) que conforma la cámara de combustión. Siendo el esquema de la figura 1 una realización preferente, él mismo contempla también la presencia de agujeros de alivio de presión (21) en las paredes de la sección superior (12) del cilindro (9) que conforma la cámara de combustión. También, al tratarse de una realización preferente, se representa el tercer anillo plano (10), divisor de las dos secciones (11 y 12) del cilindro (9) que conforma la cámara de combustión.In addition, in Figure 1, at least one fan (63) is shown located below the lower region of the pressurized air chamber (26). Figure 1 also shows some arrows that indicate the direction of the air flows. Thus, the pressurized air chamber (26) supplies pressurized air (18) to the plurality of air injectors (14) and the central air injector (16). Each air injector (14) has a side opening (14a) and an upper opening (14b), of so that the lateral opening (14a) allows to inject air flows in a substantially horizontal direction (2) into the lower section (11) of the combustion chamber. The upper opening (14b) allows, in turn, to inject air flows in a substantially vertical direction (15) into the lower section (11) of the combustion chamber. And the central air injector (16) injects an air flow in a substantially vertical direction (17) into the lower section (11) of the combustion chamber. In this way it is achieved that the combined action of all the air flows (2, 15 and 17) produces an upward rotational air flow in the lower section (11) of the cylinder (9) that forms the combustion chamber. The scheme of FIG. 1 being a preferred embodiment, it also contemplates the presence of pressure relief holes (21) in the walls of the upper section (12) of the cylinder (9) that forms the combustion chamber. Also, as it is a preferred embodiment, the third flat ring (10) is shown, dividing the two sections (11 and 12) of the cylinder (9) that forms the combustion chamber.
Además, y por tratarse de una realización preferente, se representa el sistema de aislamiento térmico compuesto por:In addition, and because it is a preferred embodiment, the thermal insulation system composed of:
- un tercer cilindro (22), concéntrico con el primer cilindro (9) que conforma la cámara de combustión, que se dispone separado de éste por - un espacio (23), dicho espacio (23) culmina, en la parte extrema superior de la sección superior (12) del cilindro (9) que conforma la cámara de combustión, en- a third cylinder (22), concentric with the first cylinder (9) that forms the combustion chamber, which is arranged separated from it by - a space (23), said space (23) culminates, in the upper end portion of the upper section (12) of the cylinder (9) that forms the combustion chamber, in
- una salida (33) por donde saldrá el aire que fluye (32) por dicho espacio (23) , - agujeros de alivio de presión (25), que se prevén, preferentemente, en las paredes del tercer cilindro (22), alineados con los agujeros de alivio de presión (21) del cilindro (9) que conforma la cámara de combustión, - un cuarto anillo plano (37), que se coloca preferentemente en el borde superior del tercer cilindro (22),- an exit (33) through which the air flowing (32) will exit through said space (23), - pressure relief holes (25), which are preferably provided in the walls of the third cylinder (22), aligned with the pressure relief holes (21) of the cylinder (9) forming the combustion chamber, - a fourth flat ring (37), which is preferably placed on the upper edge of the third cylinder (22),
- un cuarto cilindro (28), concéntrico con los cilindros anteriores (9 y 22), que se dispone separado del tercer cilindro (22) por- a fourth cylinder (28), concentric with the previous cylinders (9 and 22), which is arranged separately from the third cylinder (22) by
- un espacio (34), dicho espacio (34) culmina, en la parte extrema superior del tercer cilindro (22), en- a space (34), said space (34) culminates, in the upper end part of the third cylinder (22), in
- una salida (36) por donde saldrá el aire que fluye (35) por el espacio (34), - agujeros de alivio de presión (27), que se prevén, preferentemente en las paredes del cuarto cilindro (28), alineados con los agujeros de alivio de presión (21 y 25) de los otros cilindros (9 y 22),- an outlet (36) through which the flowing air (35) will exit through the space (34), - pressure relief holes (27), which are provided, preferably in the walls of the fourth cylinder (28), aligned with the pressure relief holes (21 and 25) of the other cylinders (9 and 22),
- un quinto anillo plano (38), que se coloca en el borde superior del cuarto cilindro (28),- a fifth flat ring (38), which is placed on the upper edge of the fourth cylinder (28),
- un aro (39) dispuesto en el borde exterior del cuarto cilindro (28) que, junto con el borde exterior del cuarto anillo plano (37) del borde superior del tercer cilindro (22) define la salida (36) del espacio (34) . Se observa también en la figura 1 que el aparato de la invención cuenta, preferentemente, con un sexto anillo plano (45) dispuesto sobre el extremo superior del segundo cilindro (42) que conforma la cámara de aire a presión (26) . En dicho sexto anillo plano (45) se apoya el cuarto cilindro (28) . Asi, con esta configuración preferente, la invención aporta una ventaja adicional en miras de conseguir reducir las pérdidas de calor al medio, dado que el cuarto cilindro (28) queda desplazado hacia abajo, respecto a la zona donde se produce la combustión y por lo tanto recibe menos calor, es mejor aislante y produce menores pérdidas de calor al medio.- a ring (39) arranged on the outer edge of the fourth cylinder (28) which, together with the outer edge of the fourth flat ring (37) of the upper edge of the third cylinder (22) defines the outlet (36) of the space (34) ). It is also observed in figure 1 that the apparatus of the invention preferably has a sixth flat ring (45) disposed on the upper end of the second cylinder (42) forming the pressurized air chamber (26). In said sixth flat ring (45) the fourth cylinder (28) is supported. Thus, with this preferred configuration, the invention provides an additional advantage in order to reduce heat losses to the medium, since the fourth cylinder (28) is displaced downwards, with respect to the area where combustion takes place and therefore both receives less heat, is better insulator and produces less heat loss to the medium.
Las figuras 3a, 3b y 3c muestran respectivamente una vista en perspectiva del conjunto de piezas reemplazable (A) para el caso de combustible sólido, combustible gaseoso o liquido sin plato de retención (53) y combustible liquido con plato de retención (53) . Asi, en la figura 3a se representa el primer disco plano (13), el inyector de aire central (16), la junta de dilatación (54) y el segundo disco plano (44) . En la figura 3b se representan adicionalmente, los inyectores de combustible (19), el distribuidor de combustible (30) y el tubo de alimentación de combustible (29) . Y en la figura 3c, se representa adicionalmente el plato de retención (53) de líquidos y se observa como la configuración del distribuidor de combustible (30) se modifica, de forma de permitir un recorrido adicional al liquido, siendo dicho recorrido (20') en sentido horizontal y paralelo al disco plano (13) . Dicho recorrido (20' ) no se representa en esta figura 3c, pero se representará en la figura 9.Figures 3a, 3b and 3c show respectively a perspective view of the replaceable parts set (A) for the case of solid fuel, gaseous or liquid fuel without holding plate (53) and liquid fuel with holding plate (53). Thus, in figure 3a, the first flat disk (13), the central air injector (16), the expansion joint (54) and the second flat disk (44) are shown. In FIG. 3b, the fuel injectors (19), the fuel distributor (30) and the fuel supply pipe (29) are additionally shown. And in Figure 3c, the retention plate (53) of liquids is further represented and it is observed how the configuration of the fuel distributor (30) is modified, in order to allow an additional travel to the liquid, said path (20 ') being ) horizontally and parallel to the flat disk (13). Said course (20 ') is not represented in this figure 3c, but will be represented in figure 9.
Los inyectores de combustible (19) poseen una apertura lateral de manera tal que la inyección del combustible en estado gaseoso o liquido se realice siguiendo una dirección sustancialmente horizontal (5) . De esta manera la inyección de combustible contribuye al sentido rotacional ascendente producido por los flujos de aire (2, 15, 17) anteriormente mencionado. Los inyectores de combustible (19) son alimentados preferentemente por su parte inferior (20) .The fuel injectors (19) have a lateral opening in such a way that the injection of the fuel in the gaseous or liquid state is carried out following a substantially horizontal direction (5). In this way the fuel injection contributes to the upward rotational sense produced by the air flows (2, 15, 17) mentioned above. The fuel injectors (19) are preferably fed by their lower part (20).
Además, en estos casos, en que se cuenta con un distribuidor de combustible (30), figuras 3b y 3c, el disco plano (44) coincide con la parte superior del distribuidor de combustible (30) .Moreover, in these cases, in which there is a fuel distributor (30), figures 3b and 3c, the flat disc (44) coincides with the upper part of the fuel distributor (30).
En la figura 4 se representa la cámara de aire a presión (26) y se observa que la misma está constituida por: - un cilindro (42) que puede ser de igual o mayor diámetro que el cilindro (9) que compone la cámara de combustión,Figure 4 shows the pressure air chamber (26) and it is observed that it consists of: - a cylinder (42) that can be of equal or greater diameter than the cylinder (9) that composes the combustion chamber,
-una parte superior que conforma un anillo plano (43) y- an upper part that forms a flat ring (43) and
-un faldón vertical (51) cuyo acabado superior presenta forma de corona.- a vertical skirt (51) whose top finish has a crown shape.
Concretamente, en la figura 4, si bien no se representa en la figura su relación con el cilindro que conforma la cámara de combustión (9), podemos indicar que corresponde a aquella realización preferente que posee sistema de aislamiento térmico y por lo tanto el cilindroSpecifically, in figure 4, although its relationship with the cylinder forming the combustion chamber (9) is not shown in the figure, we can indicate that it corresponds to that preferred embodiment that has a thermal insulation system and therefore the cylinder
(42) que conforma la cámara de aire a presión (26) posee mayor diámetro que el cilindro que conforma la cámara de combustión (9) . De esta forma el primer anillo plano (43) que conforma su parte superior posee, en su parte central, orificios (59) para permitir el paso del aire hacia los inyectores de aire (14) y orificios (60), de distinto tamaño e intercalados entre los anteriores que permiten fijar el segundo anillo plano (52) y además, dado que el esquema incluye el sistema de aislamiento térmico, incluye orificios (61) para alimentación de aire al espacio (23) de separación entre el cilindro (9) que conforma la cámara de combustión y el tercer cilindro (22) concéntrico perteneciente al sistema de aislamiento térmico y orificios (62) para alimentación de aire al espacio (34) de separación entre los cilindros (22 y 28) del sistema de aislamiento térmico. Siendo los orificios (61 y 62) dispuestos en distribución circular, siguiendo la curvatura del primer anillo plano (43) y en dirección radial hacia el exterior .(42) which forms the pressurized air chamber (26) has a larger diameter than the cylinder forming the combustion chamber (9). In this way, the first flat ring (43) that forms its upper part has, in its central part, holes (59) to allow the passage of air to the air injectors (14) and holes (60), of different sizes and sizes. interposed between the previous ones that allow fixing the second flat ring (52) and also, since the scheme includes the thermal insulation system, includes holes (61) for air supply to the space (23) of separation between the cylinder (9) which forms the combustion chamber and the third concentric cylinder (22) belonging to the thermal insulation system and orifices (62) for supplying air to the space (34) for separation between the cylinders (22 and 28) of the thermal insulation system. The holes (61 and 62) being arranged in a circular distribution, following the curvature of the first flat ring (43) and in the radial direction towards the outside.
En la figura 8 se representan, adicionalmente, flechas correspondientes a los flujos de aire, asi, a los inyectores de aire (14) ingresa aire (18) proveniente de la cámara de aire a presión (26) y por su apertura lateral (14a) sale aire que fluye en dirección sustancialmente horizontal (2) y por su apertura superior (14b) sale aire que fluye en dirección sustancialmente vertical (15) . Al inyector de aire central (16) ingresa aire (18) proveniente de la cámara de aire a presión (26) y sale aire en dirección sustancialmente vertical (17) . A la pluralidad de aperturas (16') previstas alrededor del inyector de aire central (16) ingresa aire (18) de la cámara de aire a presión (26) , dicho aire (31) circula primero verticalmente hasta incidir en el primer disco plano (13) y a partir de ahi continúa en trayectoria sustancialmente horizontal (31) y paralelo a dicho disco plano (13) , hasta salir por los rebajes de la forma de corona del faldón vertical (51) . El extremo inferior del espacio (23) definido corresponde a una separación entre el faldón vertical (51) que conforma la cámara de aire a presión (26) y el tercer cilindro (22) del sistema de aislamiento térmico y es alimentado, también, por aire (18) proveniente de la cámara de aire a presión (26) conformando el flujo de aire (24), este flujo de aire (24) se junta, en su recorrido verticalmente hacia arriba, con el aire (31) que fluye en dirección sustancialmente horizontal descrito anteriormente y juntos conforman el flujo de aire (32) que fluye por el espacio (23) y que se dirige hacia el extremo superior de los cilindros (9 y 22), hacia la salida (33) . Preferentemente, en el tercer cilindro (22) se prevén agujeros de alivio de presión (25), alineados con los agujeros de alivio de presión (21) del cilindro (9) que conforma la cámara de combustión. También se representa en la figura 8 el cuarto anillo plano (37) en el borde superior del cilindro (22) .In figure 8 arrows are additionally represented corresponding to the air flows, thus, to the air injectors (14) enters air (18) coming from the air chamber under pressure (26) and by its lateral opening (14a) air flows in a substantially horizontal direction (2) and through its upper opening (14b) air flows in a substantially vertical direction (15). To the central air injector (16) air (18) enters from the pressurized air chamber (26) and air comes out in a substantially vertical direction (17). To the plurality of openings (16 ') provided around the central air injector (16) air (18) enters the pressurized air chamber (26), said air (31) first circulates vertically until it impinges on the first flat disc (13) and from there it continues in a substantially horizontal trajectory (31) and parallel to said flat disc (13), until it exits through the recesses of the crown shape of the vertical skirt (51). The lower end of the defined space (23) corresponds to a separation between the vertical skirt (51) that forms the pressurized air chamber (26) and the third cylinder (22) of the thermal insulation system and is also fed by air (18) coming from the pressurized air chamber (26) forming the air flow (24), this air flow (24) joins, in its path vertically upwards, with the air (31) flowing in substantially horizontal direction described above and together make up the air flow (32) flowing through the space (23) and directed towards the upper end of the cylinders (9 and 22), towards the outlet (33). Preferably, pressure relief holes (25) are provided in the third cylinder (22), aligned with the pressure relief holes (21) of the cylinder (9) forming the combustion chamber. Also shown in FIG. 8 is the fourth flat ring (37) at the upper edge of the cylinder (22).
También se representa en la figura 8 el espacio (34) de separación entre los cilindros (22 y 28) del sistema de aislamiento térmico, es alimentado también por aire (18) proveniente de la cámara de aire a presión (26) de modo tal que por dicho espacio (34) fluye un flujo de aire (35) que se dirige hacia el extremo superior de los cilindros (22 y 28), hacia una salida (36) . Preferentemente, en el cuarto cilindro (28) se prevén también agujeros de alivio de presión (27) alineados con los agujeros de alivio de presión (21 y 25) de los otros cilindros (9 y 22) .Also shown in figure 8 is the space (34) of separation between the cylinders (22 and 28) of the thermal insulation system, it is also fed by air (18) coming from the pressurized air chamber (26) in such a way that through said space (34) flows an air flow (35) that is directed towards the upper end of the cylinders (22 and 28), towards an outlet (36). Preferably, in the fourth cylinder (28) there are also provided pressure relief holes (27) aligned with the pressure relief holes (21 and 25) of the other cylinders (9 and 22).
También se representa en la figura 8 el quinto anillo plano (38), que se coloca en el borde superior del cuarto cilindro (28) y que posee en su borde exterior un aro (39) que, junto con el borde exterior del cuarto anillo plano (37) del borde superior del tercer cilindro (22) definen la salida (36) .Also shown in figure 8 is the fifth flat ring (38), which is placed on the upper edge of the fourth cylinder (28) and which has on its outer edge a ring (39) which, together with the outer edge of the fourth ring plane (37) of the upper edge of the third cylinder (22) define the outlet (36).
Preferentemente, el aparato de la invención cuenta con un sexto anillo plano (45) dispuesto sobre el extremo superior del cilindro (42) que conforma la cámara de aire a presión (26) . Además, en el sexto anillo plano (45) se apoya el cuarto cilindro (28), fijándose dicho anillo planoPreferably, the apparatus of the invention has a sixth flat ring (45) disposed on the upper end of the cylinder (42) forming the pressurized air chamber (26). Furthermore, in the sixth flat ring (45) the fourth cylinder (28) is supported, said flat ring being fixed
(45) al cuarto cilindro (28) por medios convencionales de sujeción. Esta configuración aporta una ventaja adicional para conseguir reducir las pérdidas de calor al medio, dado que el cuarto cilindro (28) queda desplazado hacia abajo respecto a la sección inferior (11) del cilindro (9) que conforma la cámara de combustión, es decir la zona en donde se produce la combustión y por lo tanto recibe menos calor, con lo que se logra obtener menores pérdidas de calor al medio.(45) to the fourth cylinder (28) by conventional fastening means. This configuration provides an additional advantage to reduce heat losses to the medium, since the fourth cylinder (28) is displaced downwards with respect to the lower section (11) of the cylinder (9) that forms the combustion chamber, ie the area where the combustion takes place and therefore receives less heat, with which it is possible to obtain less heat losses to the medium.
En la figura 11, donde también se representa la realización preferente, se representa cada inyector de aire (14) con una boquilla (47) para dirigir la salida del aire, en su apertura lateral (14a) .In figure 11, where the preferred embodiment is also represented, each air injector (14) is represented with a nozzle (47) to direct the air outlet, in its lateral opening (14a).
Preferentemente, y como se observa en las figuras 11, 14, 17, 18 y 19 los medios de sujeción están compuestos de sujetadores (48) auxiliados por clavijas (49), dispuestos de manera sustancialmente circular sobre el sexto anillo plano (45) . Además, la realización preferente contempla utilizar como medio de seguridad adicional un pasador (50), para asegurar la unión sujetador (48) y clavija (49) . Cabe destacar que los sujetadores (48) y las clavijas (49) descritas pueden reemplazarse por cualquier medio de fijación convencional sin que se altere la esencia de la invención. En las figuras 11, 14 y 20, se observa, también, que el inyector de aire central (16) se encuentra centrado y, siguiendo una trayectoria radial desde el centro y hacia el exterior, donde se encuentran primero los inyectores de combustible (19) distribuidos en un arreglo sustancialmente circular. Continuando con esta dirección radial, también con arreglo sustancialmente circular, se encuentran los inyectores de aire (14), los cuales están representados incorporando cada uno una boquilla (47) para salida de aire.Preferably, and as seen in figures 11, 14, 17, 18 and 19 the fastening means are composed of fasteners (48) aided by pins (49), arranged substantially circularly on the sixth flat ring (45). In addition, the preferred embodiment contemplates use as an additional safety means a pin (50), to secure the fastener union (48) and pin (49). It should be noted that the fasteners (48) and the pins (49) described can be replaced by any conventional fixing means without altering the essence of the invention. In figures 11, 14 and 20, it is also observed that the central air injector (16) is centered and, following a radial trajectory from the center and towards the outside, where the fuel injectors are located first (19). ) distributed in a substantially circular arrangement. Continuing with this radial direction, also in substantially circular arrangement, are the air injectors (14), which are represented by each incorporating a nozzle (47) for air outlet.
En las figuras 8, 9, 10 y 11 se ve claramente la junta o ranura de dilatación (54) .Figures 8, 9, 10 and 11 clearly show the expansion joint (54).
La ranura o junta de dilatación (54), sumado al hecho que los inyectores de aire (14) se apoyen sobre el primer anillo plano (43), hacen posible que tanto el segundo anillo plano (52) como el primero (43) puedan sufrir dilataciones debido a las altas temperaturas que se generan dentro de la cámara de combustión, sin pandear. Esto evitará que se rompan. En las figuras 12, 14, 15 y 16 se muestran realizaciones concretas para el caso en que el aparato solo admita combustible gaseoso o liquido sin plato de retención. Asi, las figuras enseñan que no existe la junta de dilatación (54) . Además, el segundo anillo plano (52) y el primer disco plano (13) de las realizaciones que admitían combustible en cualquier estado físico se reemplazan por un único disco plano (13') .The groove or expansion joint (54), added to the fact that the air injectors (14) rest on the first flat ring (43), make it possible for both the second flat ring (52) and the first (43) ring to be able to suffer dilatations due to the high temperatures that are generated inside the combustion chamber, without buckling. This will prevent them from breaking. Figures 12, 14, 15 and 16 show concrete embodiments for the case in which the apparatus only admits gaseous or liquid fuel without holding plate. Thus, the figures teach that there is no expansion joint (54). In addition, the second flat ring (52) and the first flat disk (13) of the embodiments that admitted fuel in any physical state are replaced by a single flat disk (13 ').
En las figuras 13, 17, 18 y 19 se muestran realizaciones concretas para el caso en que el aparato solo admita combustible sólido y aqui, en estas figuras, se muestra que tampoco existe la junta de dilatación (54) . Además, el segundo anillo plano (52) y el primer disco plano (13) de las realizaciones que admitían combustible en cualquier estado físico se reemplazan por un único disco plano (13'), mientras que el primer anillo plano (43) y el segundo disco plano (44) se reemplazan por un único disco plano (43' ) .Figures 13, 17, 18 and 19 show concrete embodiments for the case where the apparatus only admits solid fuel and here, in these figures, shows that there is no expansion joint (54). In addition, the second flat ring (52) and the first flat disk (13) of the embodiments that admitted fuel in any physical state are replaced by a single flat disk (13 '), while the first flat ring (43) and the second flat disk (44) are replaced by a single flat disk (43 ').
También en las figuras anteriores se ven el cuarto anillo plano (37) del borde superior del tercer cilindro (22) y el aro (39) que posee en su borde exterior el quinto anillo plano (38) que se coloca en el borde superior del cuarto cilindro (28) .Also in the previous figures are the fourth flat ring (37) of the upper edge of the third cylinder (22) and the ring (39) which has on its outer edge the fifth flat ring (38) which is placed on the upper edge of the fourth cylinder (28).
En la figura 15 se ejemplifica el movimiento de los flujos de aire (2) de los inyectores de aire (14) . Este esquema, si bien está dibujado para la realización concreta en que el aparato generador y transmisor de calor solo admite combustibles gaseosos o líquidos sin plato de retención, la representación de los flujos de aire es aplicable a cualquiera de las realizaciones posibles contempladas en la presente memoria. Asi los distintos inyectores de aire (14-1, 14-2, 14-3, 14-4, 14-5, 14-6, 14- 7, 14-8, 14-9 y 14-10) emiten los respectivos flujos de aire en dirección sustancialmente horizontal (2-1, 2-2, 2- 3, 2-4, 2-5, 2-6, 2-7, 2-8, 2-9 y 2-10), de tal manera que, por ejemplo, el flujo de aire 2-1 del inyector de aire 14-1 está orientado hacia una posición intermedia entre los inyectores de aire 14-5 y 14-6. De igual manera el flujo de aire 2-2 del inyector de aire 14-2 está orientado hacia una posición intermedia entre los inyectores 14-6 y 14-7, y asi sucesivamente con cada flujo de aire de cada inyector. Esta orientación de los flujos de aire es la que provoca el flujo de aire rotacional. Asimismo, como se trata de una realización concreta que contempla sólo la posibilidad de usar combustibles gaseosos o líquidos, sin plato de retención (53) , se ha dibujado la inyección de combustible gaseoso o líquido (5-1, 5-2 y 5-3) en dirección sustancialmente horizontal y contribuyendo al sentido rotacional de los flujos de aire. Se han indicado solamente las referencias numéricas de la inyección de combustible (5-1, 5-2 y 5-3) de tres de los inyectores de combustible para que la figura no pierda claridad, pero se entiende que de cada inyector de combustible emerge su inyección de combustible en dirección sustancialmente horizontal.In Figure 15 the movement of the air flows (2) of the air injectors (14) is exemplified. This scheme, although it is drawn for the specific embodiment in which the heat generating and transmitting apparatus only admits gaseous or liquid fuels without holding plate, the representation of the air flows is applicable to any of the possible embodiments contemplated herein memory. Thus, the different air injectors (14-1, 14-2, 14-3, 14-4, 14-5, 14-6, 14-7, 14-8, 14-9 and 14-10) emit the respective air flows in substantially horizontal direction (2-1, 2-2, 2-3, 2-4, 2-5, 2-6, 2-7, 2-8, 2-9 and 2-10), of such that, for example, the air flow 2-1 of the air injector 14-1 is oriented towards an intermediate position between the air injectors 14-5 and 14-6. In the same way, the air flow 2-2 of the air injector 14-2 is oriented towards an intermediate position between the injectors 14-6 and 14-7, and so on with each air flow of each injector. This orientation of the air flows is what causes the rotational air flow. Also, as it is a specific embodiment that contemplates only the possibility of using gaseous or liquid fuels, without holding plate (53), the fuel injection has been drawn gaseous or liquid (5-1, 5-2 and 5-3) in a substantially horizontal direction and contributing to the rotational sense of the air flows. Only the numerical references of the fuel injection (5-1, 5-2 and 5-3) of three of the fuel injectors have been indicated so that the figure does not lose clarity, but it is understood that each fuel injector emerges its fuel injection in a substantially horizontal direction.
En la figura 22 se muestra el esquema del conjunto de admisión de aire a la cámara de aire a presión (26) . En dicha figura se muestra tan solo un ventilador (63), no obstante, como ya se ha mencionado, la invención admite un número mayor de ventiladores.Figure 22 shows the diagram of the air intake assembly to the pressurized air chamber (26). In said figure only one fan (63) is shown, however, as already mentioned, the invention admits a larger number of fans.
La figura 23 representa una lámina deslizante (55) que se utiliza para cerrar y/o abrir la admisión de aire al ventilador, de esta manera se consigue una manera preferente de regular dicha admisión.Figure 23 shows a sliding sheet (55) which is used to close and / or open the air intake to the fan, in this way a preferred way of regulating said intake is achieved.
En la figura 21 se muestra una vista superior de la distribución de flujos de aire en la zona superior del aparato, es decir a la salida de la cámara de combustión. La figura representa una realización preferente, es decir aquella que conlleva el sistema de aislamiento térmico conformado por los dos cilindros concéntricos (22 y 28) con el cilindro (9) que conforma la cámara de combustión y dicha estructura es aplicable a combustible en cualquier estado físico. Así, en dicha figura se ve como desde la zona central de aire (6) del último disco de combustión (3) de la llama de combustión hacia el exterior se pueden definir cinco zonas que estarán a diferentes temperaturas. Las distintas zonas, desde el interior y hacia el exterior, es decir ordenadas según gradiente decreciente de temperaturas, son:Figure 21 shows a top view of the distribution of air flows in the upper area of the apparatus, ie at the outlet of the combustion chamber. The figure represents a preferred embodiment, that is to say the one that involves the thermal insulation system formed by the two concentric cylinders (22 and 28) with the cylinder (9) that forms the combustion chamber and said structure is applicable to fuel in any state physical. Thus, in said figure it can be seen that from the central air area (6) of the last combustion disk (3) of the combustion flame towards the exterior, five zones can be defined that will be at different temperatures. The different zones, from the inside and towards the outside, that is to say ordered according to decreasing temperature gradient, are:
- la zona central (6) de aire,- the central zone (6) of air,
- la zona del último disco de combustión (3) , - la zona del flujo de aire en dirección sustancialmente vertical (15) , emergente de los inyectores de aire (14 ) ,- the area of the last combustion disc (3), - the area of the air flow in substantially vertical direction (15), emerging from the air injectors (14),
- la zona del flujo de aire (32) que circula por el espacio de separación (23) entre el cilindro que conforma la cámara de combustión (9) y el tercer cilindro (22), y- the area of the air flow (32) circulating through the gap (23) between the cylinder forming the combustion chamber (9) and the third cylinder (22), and
- la zona del flujo de aire (35) que circula por el espacio de separación (34) entre el tercer cilindro (22) y el cuarto cilindro (28) . El aparato generador y transmisor de calor descrito por la presente invención, en cualquiera de sus realizaciones, prevé que se disponga un receptor de calor (41), sobre el mismo, a la salida de la cámara de combustión y separado por un espacio (40) . Además, se ha demostrado que el fondo del receptor de calor (41) debe ser preferentemente plano.- the area of the air flow (35) circulating through the gap (34) between the third cylinder (22) and the fourth cylinder (28). The heat generating and transmitting apparatus described by the present invention, in any of its embodiments, provides that a heat receiver (41) is disposed thereon, at the outlet of the combustion chamber and separated by a space (40). ). Furthermore, it has been shown that the bottom of the heat receiver (41) should preferably be flat.
Una realización preferente, independientemente del estado fisico del combustible a emplear contempla que se coloque un montículo (56) como el que se ilustra en la figura 17 entre los distintos cilindros concéntricos, para asegurar la concentricidad de los cilindros (9, 22 y 28) . Alternativamente, puede reemplazarse el montículo (56) por un doblado (57) de las paredes de los cilindros (9, 22 y 28) . También en dicha realización preferente se coloca un soporte (58) para el receptor de calor (41) . A preferred embodiment, regardless of the physical state of the fuel to be used, contemplates placing a mound (56) as illustrated in Figure 17 between the different concentric cylinders, to ensure the concentricity of the cylinders (9, 22 and 28) . Alternatively, the mound (56) can be replaced by a bending (57) of the walls of the cylinders (9, 22 and 28). Also in said preferred embodiment a support (58) for the heat receiver (41) is placed.

Claims

REIVINDICACIONES
1. Aparato generador y transmisor de calor que comprende al menos : una cámara de combustión cilindrica (9) dividida en una sección inferior (11) y una sección superior (12) de altura variable, una cámara de aire a presión (26) que se dispone debajo de la sección inferior (11) de la cámara de combustión (9), y una pluralidad de inyectores de aire (14), caracterizado porque: los inyectores de aire (14) se disponen apoyados sobre un anillo plano (43) que conforma la parte superior de la cámara de aire a presión (26) y encastrados en un segundo anillo plano (52) dispuesto en contacto con el extremo inferior del cilindro (9) que conforma la cámara de combustión; dicho primer anillo plano (43) posee orificios (59 y 60) de al menos dos diámetros diferentes en su superficie, y porque comprende además: un conjunto de piezas reemplazable (A) dispuesto en el centro libre de los anillos planos (43 y 52), en el extremo inferior de la sección inferior (11) de la cámara de combustión (9) y unido al segundo anillo plano (52) por medio de una junta de dilatación (54); dicho conjunto de piezas reemplazable (A) comprende al menos un inyector de aire central (16) dispuesto en el centro geométrico del conjunto de piezas (A) , siendo el resto de su configuración función del estado físico del combustible a emplear, y al menos un ventilador (63) .Heat generating and transmitting apparatus comprising at least: a cylindrical combustion chamber (9) divided into a lower section (11) and a upper section (12) of variable height, a pressurized air chamber (26) which it is arranged below the lower section (11) of the combustion chamber (9), and a plurality of air injectors (14), characterized in that: the air injectors (14) are disposed resting on a flat ring (43) forming the upper part of the pressurized air chamber (26) and embedded in a second flat ring (52) disposed in contact with the lower end of the cylinder (9) forming the combustion chamber; said first flat ring (43) has holes (59 and 60) of at least two different diameters on its surface, and because it also comprises: a replaceable set of parts (A) disposed in the free center of the flat rings (43 and 52) ), at the lower end of the lower section (11) of the combustion chamber (9) and joined to the second flat ring (52) by means of an expansion joint (54); said replaceable set of parts (A) comprises at least one central air injector (16) arranged in the geometric center of the set of pieces (A), the rest of its configuration being a function of the physical state of the fuel to be used, and at least a fan (63).
2. Aparato generador y transmisor de calor según la reivindicación 1, caracterizado porque la cámara de aire a presión (26) está constituida por un segundo cilindro (42) y provee aire a presión (18) a la pluralidad de inyectores de aire (14) y al inyector de aire central (16) comprendido en el conjunto de piezas (A) .2. Heat generating and transmitting apparatus according to claim 1, characterized in that the air chamber a pressure (26) is constituted by a second cylinder (42) and supplies pressurized air (18) to the plurality of air injectors (14) and to the central air injector (16) included in the assembly of parts (A).
3. Aparato generador y transmisor de calor según la reivindicación 1, caracterizado porque el anillo plano (43) que conforma la parte superior de la cámara de aire a presión (26) comprende además un faldón vertical (51) con acabado, en su parte superior, en forma de corona.3. Heat generating and transmitting apparatus according to claim 1, characterized in that the flat ring (43) forming the upper part of the pressurized air chamber (26) further comprises a vertical skirt (51) with finish, in its part superior, in the form of a crown.
4. Aparato generador y transmisor de calor según la reivindicación 1, caracterizado porque cada inyector de aire (14) posee una apertura lateral (14a) y una apertura superior (14b), de modo que la apertura lateral (14a) permita inyectar flujos de aire en dirección sustancialmente horizontal (2) y la apertura superior (14b) permita inyectar flujos de aire en dirección sustancialmente vertical (15), mientras que el inyector de aire central (16) inyecta un flujo de aire en dirección sustancialmente vertical (17), de tal manera que la acción combinada de todos los flujos de aire (2, 15 y 17) produzca un flujo de aire rotacional ascendente en el interior de la cámara de combustión.4. Heat generating and transmitting apparatus according to claim 1, characterized in that each air injector (14) has a lateral opening (14a) and an upper opening (14b), so that the lateral opening (14a) allows to inject flows of air in a substantially horizontal direction (2) and the upper opening (14b) allows injecting air flows in a substantially vertical direction (15), while the central air injector (16) injects an air flow in a substantially vertical direction (17) , in such a way that the combined action of all the air flows (2, 15 and 17) produces an ascending rotational air flow inside the combustion chamber.
5. Aparato generador y transmisor de calor según la reivindicación 4, caracterizado porque cada inyector de aire (14) posee, en su apertura lateral (14a), una boquilla (47) para salida de aire.5. Heat generating and transmitting apparatus according to claim 4, characterized in that each air injector (14) has, in its lateral opening (14a), a nozzle (47) for air outlet.
6. Aparato generador y transmisor de calor según la reivindicación 1, caracterizado porque las dos secciones (11 y 12) del cilindro (9) que conforma la cámara de combustión se forman mediante la interposición de un tercer anillo plano (10) divisor. 6. Heat generating and transmitting apparatus according to claim 1, characterized in that the two sections (11 and 12) of the cylinder (9) forming the combustion chamber are formed by the interposition of a third flat ring (10) divider.
7. Aparato generador y transmisor de calor según la reivindicación 1, caracterizado porque en la sección superior (12) del cilindro (9) se prevén agujeros de alivio de presión (21) .7. Heat generating and transmitting apparatus according to claim 1, characterized in that pressure relief holes (21) are provided in the upper section (12) of the cylinder (9).
8. Aparato generador y transmisor de calor según la reivindicación 1, caracterizado porque el segundo anillo plano (52) se fija mediante medios de fijación (46) del estilo de un perno, bulón o tornillo dispuestos de modo que estén intercalados entre los inyectores de aire (14) .8. Heat generating and transmitting apparatus according to claim 1, characterized in that the second flat ring (52) is fixed by fastening means (46) of the style of a bolt, bolt or screw arranged so that they are interposed between the injectors of air (14).
9. Aparato generador y transmisor de calor según la reivindicación 1, caracterizado porque el conjunto de piezas reemplazable (A) comprende además: un disco plano (13) unido al segundo anillo plano (52) por medio de la junta de dilatación (54), y un segundo disco plano (44), paralelo al anterior, apoyado en el anillo plano (43); de forma tal que el inyector de aire central (16) quede encastrado entre ambos discos planos (13 y 44), en su centro geométrico.9. Heat generating and transmitting apparatus according to claim 1, characterized in that the replaceable assembly (A) further comprises: a flat disc (13) joined to the second flat ring (52) by means of the expansion joint (54) , and a second flat disk (44), parallel to the previous one, resting on the flat ring (43); in such a way that the central air injector (16) is embedded between both flat discs (13 and 44), in its geometric center.
10. Aparato generador y transmisor de calor según la reivindicación 9, caracterizado porque en el centro geométrico del segundo disco plano (44), alrededor y en distribución circular concéntrica con el inyector de aire central (16), se prevé una pluralidad de aperturas (16') por donde ingresa aire a presión (18) proveniente de la cámara de aire a presión (26) que, al incidir contra el disco plano (13), contribuye con su enfriamiento y que, dado el acabado en forma de corona de la parte superior del faldón vertical (51), continúa con una trayectoria sustancialmente horizontal (31) hasta salir de la cámara de aire a presión (26) . 10. Heat generating and transmitting apparatus according to claim 9, characterized in that a plurality of openings are provided in the geometric center of the second flat disc (44), around and in circular distribution concentric with the central air injector (16). 16 ') through which pressurized air (18) comes from the pressurized air chamber (26), which, by striking against the flat disk (13), contributes to its cooling and, given the crown-shaped finish the upper part of the vertical skirt (51) continues with a substantially horizontal trajectory (31) until it leaves the pressurized air chamber (26).
11. Aparato generador y transmisor de calor según la reivindicación 10, caracterizado porque cuando el combustible a emplear es gaseoso o liquido, el conjunto de piezas reemplazable (A) comprende además una pluralidad inyectores de combustible (19) dispuestos apoyados sobre el segundo disco plano (44) y pasados a través del primer disco plano (13) por medio de orificios que se practican en dicho disco plano (13), - un distribuidor de combustible (30) cuya parte superior conforma el segundo disco plano (44), y un tubo de alimentación de combustible (29) al distribuidor .11. The heat generator and transmitter apparatus according to claim 10, characterized in that when the fuel to be used is gaseous or liquid, the replaceable part set (A) further comprises a plurality of fuel injectors (19) disposed resting on the second flat disc. (44) and passed through the first flat disc (13) by means of holes that are made in said flat disc (13), - a fuel distributor (30) whose upper part forms the second flat disc (44), and a fuel supply pipe (29) to the distributor.
12. Aparato generador y transmisor de calor según la reivindicación 11, caracterizado porque cuando el combustible a emplear es liquido, el conjunto de piezas reemplazable (A) comprende además un plato (53) de retención del combustible liquido y el distribuidor de combustible (30) varia su configuración de forma tal que la alimentación de combustible incluya un recorrido sustancialmente horizontal y paralelo (20' ) al primer disco plano (13) antes de llegar el combustible al inyector de combustible (19) .12. Heat generating and transmitting apparatus according to claim 11, characterized in that when the fuel to be used is liquid, the replaceable parts set (A) further comprises a liquid fuel retention plate (53) and the fuel distributor (30). ) varies its configuration in such a way that the fuel supply includes a substantially horizontal and parallel path (20 ') to the first flat disc (13) before the fuel reaches the fuel injector (19).
13. Aparato generador y transmisor de calor según las reivindicaciones 4, 11 o 12, caracterizado porque los inyectores de combustible (19) poseen una apertura lateral de forma tal que la inyección de combustible en estado gaseoso o liquido se realiza siguiendo una dirección sustancialmente horizontal (5), de manera de contribuir al sentido rotacional de los flujos de aire (2, 15 y 17), y los inyectores de combustible (19) son alimentados por su parte inferior (20) . 13. The heat generator and transmitter apparatus according to claim 4, 11 or 12, characterized in that the fuel injectors (19) have a lateral opening such that the injection of fuel in the gaseous or liquid state is carried out following a substantially horizontal direction (5), so as to contribute to the rotational sense of the air flows (2, 15 and 17), and the fuel injectors (19) are fed by its lower part (20).
14. Aparato generador y transmisor de calor según la reivindicación 1, caracterizado porque se prevé un tercer cilindro (22), concéntrico con el cilindro (9) que conforma la cámara de combustión, que se dispone separado de éste por un espacio (23) por cuyo extremo inferior fluye un flujo de aire (24) alimentado por el aire a presión (18) proveniente de la cámara de aire a presión (26) .14. Heat generating and transmitting apparatus according to claim 1, characterized in that a third cylinder (22) is provided, concentric with the cylinder (9) forming the combustion chamber, which is arranged separated from it by a space (23) at its lower end flows an air flow (24) fed by the pressurized air (18) coming from the pressurized air chamber (26).
15. Aparato generador y transmisor de calor según la reivindicaciones 10 y 14, caracterizado porque al flujo de aire (24) que circula por el extremo inferior del espacio15. Heat generating and transmitting apparatus according to claims 10 and 14, characterized in that the air flow (24) circulating through the lower end of the space
(23) de separación entre el cilindro (9) que conforma la cámara de combustión y el tercer cilindro (22) se le incorpora, además, el flujo de aire en dirección sustancialmente horizontal (31) , proveniente del faldón vertical (51) y juntos conforman un flujo de aire (32) que se dirige hacia el extremo superior de los cilindros (9 y(23) of separation between the cylinder (9) that forms the combustion chamber and the third cylinder (22) is incorporated, in addition, the air flow in substantially horizontal direction (31), coming from the vertical skirt (51) and together they form an air flow (32) that is directed towards the upper end of the cylinders (9 and
22), hacia una salida (33) .22), towards an exit (33).
16. Aparato generador y transmisor de calor de calor según la reivindicación 14, caracterizado porque en la sección superior (12) del cilindro (9) se prevén agujeros de alivio de presión (21) y en el tercer cilindro (22) se prevén agujeros de alivio de presión (25) alineados con los agujeros de alivio de presión (21) del cilindro (9) que conforma la cámara de combustión; además en el borde superior del tercer cilindro (22) se coloca un cuarto anillo plano (37) .16. Heat generating and heat transmitting apparatus according to claim 14, characterized in that in the upper section (12) of the cylinder (9) pressure relief holes (21) are provided and in the third cylinder (22) holes are provided pressure relief (25) aligned with the pressure relief holes (21) of the cylinder (9) that makes up the combustion chamber; furthermore, a fourth flat ring (37) is placed on the upper edge of the third cylinder (22).
17. Aparato generador y transmisor de calor según la reivindicación 14, caracterizado porque se prevé un cuarto cilindro (28), concéntrico con los cilindros anteriores (9 y 22), que se dispone separado de éste último por un espacio (34) por donde fluye un flujo de aire (35) alimentado por el aire a presión (18) de la cámara de aire a presión (26); dicho flujo de aire (35) se dirige hacia el extremo superior de los cilindros (22 y 28), hacia una segunda salida (36) .17. Heat generator and transmitter apparatus according to claim 14, characterized in that a fourth cylinder (28) is provided, concentric with the previous cylinders (9 and 22), which is arranged separately from the latter by a space (34) where a flow of air (35) flows through the pressurized air (18) of the air chamber under pressure (26); said air flow (35) is directed towards the upper end of the cylinders (22 and 28), towards a second outlet (36).
18. Aparato generador y transmisor de calor según la reivindicación 16, caracterizado porque en el cuarto cilindro (28) se prevén también agujeros de alivio de presión (27) alineados con los agujeros de alivio de presión (21 y 25) de los cilindros anteriores (9 y 22) y la segunda salida (36) de dicho cuarto cilindro (28) está definida por un quinto anillo plano (38) que se coloca en el borde superior del cuarto cilindro (28) y que posee en su borde exterior un aro (39) , junto con el borde exterior del cuarto anillo plano (37) del borde superior del tercer cilindro (22) .18. Heat generating and transmitting apparatus according to claim 16, characterized in that in the fourth cylinder (28) there are also provided pressure relief holes (27) aligned with the pressure relief holes (21 and 25) of the previous cylinders (9 and 22) and the second outlet (36) of said fourth cylinder (28) is defined by a fifth flat ring (38) which is placed on the upper edge of the fourth cylinder (28) and which has on its outer edge a ring (39), together with the outer edge of the fourth flat ring (37) of the upper edge of the third cylinder (22).
19. Aparato generador y transmisor de calor según una de las reivindicaciones 17 o 18, caracterizado porque se dispone, además un sexto anillo plano (45) sobre el extremo superior del cilindro (42) que conforma la cámara de aire a presión (26), en dicho anillo plano (45) se apoya el cuarto cilindro (28), fijándose el anillo plano (45) al cilindro (28) por medios convencionales de sujeción.Heat generator and transmitter apparatus according to one of claims 17 or 18, characterized in that a sixth flat ring (45) is also provided on the upper end of the cylinder (42) forming the pressurized air chamber (26) , in said flat ring (45) the fourth cylinder (28) is supported, the flat ring (45) being fixed to the cylinder (28) by conventional fastening means.
20. Aparato generador y transmisor de calor según la reivindicación 1, caracterizado porque el al menos un ventilador (63) comprende además una lámina deslizante de manera de abrir o cerrar la admisión de aire al ventilador20. Heat generating and transmitting apparatus according to claim 1, characterized in that the at least one fan (63) further comprises a sliding sheet so as to open or close the air intake to the fan
(63) .(63).
21. Aparato generador y transmisor de calor según una cualquiera de las reivindicaciones anteriores, caracterizado porque sobre él mismo, separado por un espacio (40), se coloca un receptor de calor (41) . 21. Heat generating and transmitting apparatus according to any one of the preceding claims, characterized in that a heat receiver (41) is placed on it, separated by a space (40).
22. Llama de combustión obtenida dentro del aparato generador y transmisor de calor según cualquiera de las reivindicaciones anteriores, caracterizada porque comprende una pluralidad de discos de combustión (3), formados por gases de combustión, separados por discos de aire (4) formados por los flujos de aire (2, 15 y 17) que se suministran para oxidación del combustible y el suministro de aire se realiza de manera tal que confiera rotación a la llama, de forma tal que ésta adopte la forma de un vórtice pulsante con zonas centrales de aire (6), secciones de continuidad (7) entre los discos de combustión (3) y terminaciones (8) .22. Flame of combustion obtained within the generating and heat transfer apparatus according to any of the preceding claims, characterized in that it comprises a plurality of combustion discs (3), formed by combustion gases, separated by air discs (4) formed by the air flows (2, 15 and 17) that are supplied for oxidation of the fuel and the supply of air is carried out in such a way that it confers rotation to the flame, in such a way that it takes the form of a pulsating vortex with central areas of air (6), continuity sections (7) between the combustion discs (3) and terminations (8).
23. Llama de combustión según la reivindicación 22, caracterizada porque cada uno de los disco de gases de combustión (3) tiene una su superficie exterior que define una superficie de oxidación, de manera tal que se define como superficie total de oxidación de la llama de combustión a la suma de todas las superficies de oxidación de cada uno de los discos de gases de combustión (3) presentes en dicha llama. 23. The combustion flame according to claim 22, characterized in that each of the combustion gas discs (3) has an outer surface that defines an oxidation surface, such that it is defined as the total surface of oxidation of the flame. of combustion to the sum of all the oxidation surfaces of each of the combustion gas disks (3) present in said flame.
PCT/SV2008/000003 2008-10-09 2008-10-09 Device for generating and transmitting heat capable of operating with fuel in any physical state and combustion flame WO2010042079A1 (en)

Priority Applications (10)

Application Number Priority Date Filing Date Title
MX2011003817A MX2011003817A (en) 2008-10-09 2008-10-09 Device for generating and transmitting heat capable of operating with fuel in any physical state and combustion flame.
BRPI0823153-2A BRPI0823153A2 (en) 2008-10-09 2008-10-09 Heat generating and transmitting device capable of operating on fuel in any physical state and combustion flame
CN200880132274.9A CN102245967B (en) 2008-10-09 2008-10-09 Device for generating and transmitting heat capable of operating with fuel in any physical state and combustion flame
PCT/SV2008/000003 WO2010042079A1 (en) 2008-10-09 2008-10-09 Device for generating and transmitting heat capable of operating with fuel in any physical state and combustion flame
EP08813763.3A EP2345842A4 (en) 2008-10-09 2008-10-09 Device for generating and transmitting heat capable of operating with fuel in any physical state and combustion flame
PA20098845101A PA8845101A1 (en) 2008-10-09 2009-10-08 HEAT GENERATING AND TRANSMITTER APPLIANCE TO OPERATE WITH FUEL IN ANY PHYSICAL STATE AND COMBUSTION FLAME
ARP090103900A AR076439A1 (en) 2008-10-09 2009-10-09 HEAT GENERATING AND TRANSMITTER APPLIANCE TO OPERATE WITH FUEL IN ANY PHYSICAL STATE AND COMBUSTION FLAME
UY0001032170A UY32170A (en) 2008-10-09 2009-10-09 HEAT GENERATING AND TRANSMITTER APPLIANCE TO OPERATE WITH FUEL IN ANY PHYSICAL STATE AND COMBUSTION FLAME
PE2009001182A PE20100614A1 (en) 2008-10-09 2009-10-12 HEAT GENERATOR AND TRANSMITTER APPLIANCE CAPABLE OF OPERATING WITH FUEL IN ANY PHYSICAL STATE AND COMBUSTION FLAME
US13/081,691 US20110239916A1 (en) 2008-10-09 2011-04-07 Device for generating and transmitting heat capable of operating with fuel in any physical state and combustion flame

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/SV2008/000003 WO2010042079A1 (en) 2008-10-09 2008-10-09 Device for generating and transmitting heat capable of operating with fuel in any physical state and combustion flame

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US13/081,691 Continuation US20110239916A1 (en) 2008-10-09 2011-04-07 Device for generating and transmitting heat capable of operating with fuel in any physical state and combustion flame

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CN (1) CN102245967B (en)
AR (1) AR076439A1 (en)
BR (1) BRPI0823153A2 (en)
MX (1) MX2011003817A (en)
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PE (1) PE20100614A1 (en)
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CN104848210A (en) * 2015-05-28 2015-08-19 苏州斯洛莱自动化设备有限公司 Boiler gas combustion device

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UY32170A (en) 2010-05-31
AR076439A1 (en) 2011-06-15
PA8845101A1 (en) 2010-05-26
PE20100614A1 (en) 2010-09-09
MX2011003817A (en) 2011-08-03
CN102245967A (en) 2011-11-16
EP2345842A1 (en) 2011-07-20
BRPI0823153A2 (en) 2015-06-16
CN102245967B (en) 2014-09-17
EP2345842A4 (en) 2014-06-25
US20110239916A1 (en) 2011-10-06

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