EP1364160B1 - Combustion device - Google Patents
Combustion device Download PDFInfo
- Publication number
- EP1364160B1 EP1364160B1 EP02700955A EP02700955A EP1364160B1 EP 1364160 B1 EP1364160 B1 EP 1364160B1 EP 02700955 A EP02700955 A EP 02700955A EP 02700955 A EP02700955 A EP 02700955A EP 1364160 B1 EP1364160 B1 EP 1364160B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- combustion
- air
- fuel
- supplied
- pipe
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired - Lifetime
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 78
- 239000000446 fuel Substances 0.000 claims abstract description 32
- 239000002245 particle Substances 0.000 claims description 9
- 239000002551 biofuel Substances 0.000 claims description 6
- -1 briquets Substances 0.000 claims description 2
- 239000008188 pellet Substances 0.000 claims description 2
- 239000002023 wood Substances 0.000 claims description 2
- 239000004449 solid propellant Substances 0.000 abstract 1
- 239000007789 gas Substances 0.000 description 13
- 229910052799 carbon Inorganic materials 0.000 description 11
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 10
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 4
- 230000008021 deposition Effects 0.000 description 3
- 238000000151 deposition Methods 0.000 description 3
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 3
- 238000006722 reduction reaction Methods 0.000 description 3
- 229910002092 carbon dioxide Inorganic materials 0.000 description 2
- 239000001569 carbon dioxide Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 239000006227 byproduct Substances 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 238000001311 chemical methods and process Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000002309 gasification Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 210000000056 organ Anatomy 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23L—SUPPLYING 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
- F23L1/00—Passages or apertures for delivering primary air for combustion
- F23L1/02—Passages or apertures for delivering primary air for combustion by discharging the air below the fire
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
- F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
- F23C6/045—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/02—Disposition of air supply not passing through burner
- F23C7/06—Disposition of air supply not passing through burner for heating the incoming air
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G7/00—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals
- F23G7/10—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of field or garden waste or biomasses
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23L—SUPPLYING 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
- F23L5/00—Blast-producing apparatus before the fire
- F23L5/02—Arrangements of fans or blowers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G2205/00—Waste feed arrangements
- F23G2205/12—Waste feed arrangements using conveyors
- F23G2205/121—Screw conveyor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G2205/00—Waste feed arrangements
- F23G2205/20—Waste feed arrangements using airblast or pneumatic feeding
Definitions
- This invention relates to an improved combustion device for burning relatively finely granulated biofuel, more specifically it relates to a combustion device that utilises preheated combustion air that is supplied to the combustion chamber in the combustion device.
- a combustion device according to the preamble of claim 1, is known from document FI-B-71408.
- the burning of gas intensive biofuels is associated with a plurality of problems.
- One specific problem in all biofuel combustions is to find combustion devices that allow for a high reduction speed for the carbon particles in the combustion zone. If a retort or a combustion chamber is used, the burning of the highly energetic fuels having a low degree of moisture content causes the fuels to gasify at a low effect output before they have reached the retort or the combusition chamber. High resistance in the throughput causes difficulties to direct a uniform blow-through of the fuel mass, which results in local burnings, where the main part of the airstream will flow through, while other parts of the fuel will be unaffected.
- a particular problem is that the melting point for ash often is easily reached. In connection to this, if a retort or an equivalent device is used, a deposition of slag and uncombusted fuel is easily created, which in turn disturbs the desired distribution of air and fuel.
- the present invention is intended to overcome these problems and simultaneously ensure an efficient combustion during all burning conditions. This and other advantages are obtained with the combustion device according to the present invention.
- Fig. 1 shows a cross-section of one embodiment of the present invention.
- the combustion device comprises a combustion chamber 1, which essentially consists of an excentric input part 2, a cylindrical middle part 3, and a conical output part 4.
- a number of apertures 12 for air-blasting are disposed in the input part 2, the middle part 3, and the output part 4 to supply preheated air on the one hand through the face of the fuel mass and on the other hand through the created gas volume, wherein the blowing is performed in marked zones of primary air, secondary ari and tertiary air, from the input part 2 to the output part 4.
- Primary air defines the fuel evaporation air
- secondary air defines the gas combustion air
- tertiary air is defined as the air in the final combustion of the rests.
- the combustion device is equipped with a fuel grating in the lower part of the conical shaped output part 4.
- a grating is here defined as a device that provides small evacuation paths out of the combustion chamber 1. The grating is provided to allow the combusted fuel particles to fall down through the grating and out of the combustion chamber, while the burned gases leave the combustion chamber through the apertures in the conically shaped output part 4.
- the fuel is fed horisontally into the combustion chamber 1 through a feeding pipe 7 by means of a feeding screw 6 disposed in the feeding pipe 7.
- a feeding screw 6 disposed in the feeding pipe 7.
- the combustion air is supplied around the feeding pipe 7 of the feeding screws 6, therebye cooling the fuel.
- the fuel is preferably ignited by means of an electrical ignition device 10 disposed in the end of the feeding pipe 7.
- the end of the feeding pipe is adjacent to the excentric input part 2.
- the combustion air continues towards the excentric input part 2 and cools this part.
- the combustion air then continues in a pipe 9, that surrounds the combustion chamber and a cylindrically shaped heat shield 8, which in turn surrounds a large part of the combustion chamber 1, preferably it surrounds the whole of the middle part and at least 2/3 of the conically shaped output part 4.
- the combustion air first encounters the conically shaped output part 4, and then shifts direction approximately 180°C and passes in under the heat shield 8. In this position the air is heated by the combustion chamber, but in the contact with the output part 4 heat is absorbed from the output part 4, which means that the air will be pre-heated at the same time as a cooling of the output part 4 is obtained.
- the combustion air enters the cylindrical middle part 3 as pre-heated primary air. Since the side channels have a divergent orientation with regard to the fuel input direction a loosening of the fuel mass as well as a smaller volume height is obtained, which gives an increased contact surface for the supplied primary air.
- the abovementioned heat shield have three functions.
- the first function is to shield the cylindrical pipe 9 from the heat that is radiated from the combustion chamber 1. Without this shielding the cylindrical pipe would implicitly influence the temperature in the combustion zones.
- the second purpose is to force the combustion air to cool the conical output part 4 in the combustion device, and therebye implicitly supply a lower temperature with the secondary air, which in turn reduces the creation of nitrogen oxides in the final stage of the combustion.
- the third purpose is to preheat the primary air that is to gasify the fuel under a sufficiently short time so that the creation of carbon monoxide radically decreases and so that the chemical process instead goes directly to carbon dioxide.
- the main part of the combustion takes place in the primary zone when the preheated air quickly gasifies the fuel.
- the combustion air is turbulent and directed against the feeding direction of the fuel.
- the rising burn gases might contain partially uncombusted parts that encounter the air supplied through the apertures in the upper part of the cylindrically shaped middle part 3, wherebye gases emanating from the fuel are trapped and mixed with fire flames from the front of the fuel. These gases are now forced, through the increase in volume, towards the conical output part 4 where they are mixed with air supplied from apartures in the conical part 4. This is where the final combustion of the remaining uncombusted gases takes place.
- the heat shield 8 that supports the preheating of the primary air also provides for a preheating of the moisture embedded in the fuel, which means that overheated vapour will be present in the process.
- the overheated vapour is heavier than the other gases and is transported out of the combustion chamber through the grating 5, where the overheated vapour encounters carbon particles which leads to a reduction reaction since carbon in combination with water creates carbon dioxide.
- the output aparture 4 is provided with a grating 5 in the lower part.
- the grating 5 prevents carbon particles larger than a certain size from leaving the combustion zone before they have been "prepared” with overheated vapour. The remains of the carbon that are still present after the combustion cannot leave the combustion zone since they are built by carbon crystals that are drawn to materials in the form of fluid or gas. They can be removed by treatment with overheated water vapour, which is a by-product in the combustion of biofuel.
- the grating in the lower part of the conically shaped output aperture is a way of overcoming the problem that the time required to burn the carbon particles completely cannot be achieved under normal conditions.
- the reason for this is partly the amount of fuel and the supply of air, but it also depends on the compositions that carbon particles bind on their surface without forming chemical bonds. If the uncombusted carbon particles did not fall down through the surface of the grating, the combustion zone would decrease in the same degree, whereby the increased volume of carbon particles would affect the combustion negatively, partly through increased volume-pressure relations, partly through a lower combustion temperature, something that in practice would mean shorter retention times and an increased output of uncombusted gases and indirectly a lower heating effect.
- Characteristic for all combustions of biofuels is that the gas generation and the reductions always reach an equilibrium that is directly linked to the reaction temperature.
- the combustion air is preheated in all combustion zones except the ash zone. It is always well calibrated in relation to the supplied amount of fuel in the combustion zone.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Environmental & Geological Engineering (AREA)
- Thermal Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Physics & Mathematics (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Solid-Fuel Combustion (AREA)
- Regulation And Control Of Combustion (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
Abstract
Description
- This invention relates to an improved combustion device for burning relatively finely granulated biofuel, more specifically it relates to a combustion device that utilises preheated combustion air that is supplied to the combustion chamber in the combustion device. Such a combustion device, according to the preamble of claim 1, is known from document FI-B-71408.
- The burning of gas intensive biofuels, such as pellets, briquets, wood chips and the like, is associated with a plurality of problems. One specific problem in all biofuel combustions is to find combustion devices that allow for a high reduction speed for the carbon particles in the combustion zone. If a retort or a combustion chamber is used, the burning of the highly energetic fuels having a low degree of moisture content causes the fuels to gasify at a low effect output before they have reached the retort or the combusition chamber. High resistance in the throughput causes difficulties to direct a uniform blow-through of the fuel mass, which results in local burnings, where the main part of the airstream will flow through, while other parts of the fuel will be unaffected.
- A particular problem is that the melting point for ash often is easily reached. In connection to this, if a retort or an equivalent device is used, a deposition of slag and uncombusted fuel is easily created, which in turn disturbs the desired distribution of air and fuel.
- Another problem in combustions is that salts condense in the temperature range of 600-1000 °C, as does certain gases within the fuel. This causes depositions to form on the outside surfaces of the combustion device. These depositions are hard to remove and may clog the air holes disposed in the combustion device.
- The present invention is intended to overcome these problems and simultaneously ensure an efficient combustion during all burning conditions. This and other advantages are obtained with the combustion device according to the present invention.
- Fig. 1 shows a cross-section of one embodiment of the present invention.
- As is clear from Fig.1, the combustion device according to the invention comprises a combustion chamber 1, which essentially consists of an
excentric input part 2, acylindrical middle part 3, and aconical output part 4. A number ofapertures 12 for air-blasting, in general marked with X in the figure, are disposed in theinput part 2, themiddle part 3, and theoutput part 4 to supply preheated air on the one hand through the face of the fuel mass and on the other hand through the created gas volume, wherein the blowing is performed in marked zones of primary air, secondary ari and tertiary air, from theinput part 2 to theoutput part 4. Primary air defines the fuel evaporation air, secondary air defines the gas combustion air, and tertiary air is defined as the air in the final combustion of the rests. In addition to the abovementioned parts the combustion device is equipped with a fuel grating in the lower part of the conicalshaped output part 4. A grating is here defined as a device that provides small evacuation paths out of the combustion chamber 1. The grating is provided to allow the combusted fuel particles to fall down through the grating and out of the combustion chamber, while the burned gases leave the combustion chamber through the apertures in the conicallyshaped output part 4. - During operation the fuel is fed horisontally into the combustion chamber 1 through a
feeding pipe 7 by means of afeeding screw 6 disposed in thefeeding pipe 7. With help from organs, such as a blower, the combustion air is supplied around thefeeding pipe 7 of thefeeding screws 6, therebye cooling the fuel. The fuel is preferably ignited by means of anelectrical ignition device 10 disposed in the end of thefeeding pipe 7. The end of the feeding pipe is adjacent to theexcentric input part 2. The combustion air continues towards theexcentric input part 2 and cools this part. The combustion air then continues in apipe 9, that surrounds the combustion chamber and a cylindrically shapedheat shield 8, which in turn surrounds a large part of the combustion chamber 1, preferably it surrounds the whole of the middle part and at least 2/3 of the conicallyshaped output part 4. After having travelled over theheat shield 8, the combustion air first encounters the conically shapedoutput part 4, and then shifts direction approximately 180°C and passes in under theheat shield 8. In this position the air is heated by the combustion chamber, but in the contact with theoutput part 4 heat is absorbed from theoutput part 4, which means that the air will be pre-heated at the same time as a cooling of theoutput part 4 is obtained. Finally, the combustion air enters thecylindrical middle part 3 as pre-heated primary air. Since the side channels have a divergent orientation with regard to the fuel input direction a loosening of the fuel mass as well as a smaller volume height is obtained, which gives an increased contact surface for the supplied primary air. - The abovementioned heat shield have three functions. The first function is to shield the
cylindrical pipe 9 from the heat that is radiated from the combustion chamber 1. Without this shielding the cylindrical pipe would implicitly influence the temperature in the combustion zones. The second purpose is to force the combustion air to cool theconical output part 4 in the combustion device, and therebye implicitly supply a lower temperature with the secondary air, which in turn reduces the creation of nitrogen oxides in the final stage of the combustion. The third purpose is to preheat the primary air that is to gasify the fuel under a sufficiently short time so that the creation of carbon monoxide radically decreases and so that the chemical process instead goes directly to carbon dioxide. - The main part of the combustion takes place in the primary zone when the preheated air quickly gasifies the fuel. Here, the combustion air is turbulent and directed against the feeding direction of the fuel. The rising burn gases might contain partially uncombusted parts that encounter the air supplied through the apertures in the upper part of the cylindrically
shaped middle part 3, wherebye gases emanating from the fuel are trapped and mixed with fire flames from the front of the fuel. These gases are now forced, through the increase in volume, towards theconical output part 4 where they are mixed with air supplied from apartures in theconical part 4. This is where the final combustion of the remaining uncombusted gases takes place. - During the gasification, the
heat shield 8 that supports the preheating of the primary air also provides for a preheating of the moisture embedded in the fuel, which means that overheated vapour will be present in the process. The overheated vapour is heavier than the other gases and is transported out of the combustion chamber through thegrating 5, where the overheated vapour encounters carbon particles which leads to a reduction reaction since carbon in combination with water creates carbon dioxide. - As mentioned above, the
output aparture 4 is provided with agrating 5 in the lower part. The grating 5 prevents carbon particles larger than a certain size from leaving the combustion zone before they have been "prepared" with overheated vapour. The remains of the carbon that are still present after the combustion cannot leave the combustion zone since they are built by carbon crystals that are drawn to materials in the form of fluid or gas. They can be removed by treatment with overheated water vapour, which is a by-product in the combustion of biofuel. - The grating in the lower part of the conically shaped output aperture is a way of overcoming the problem that the time required to burn the carbon particles completely cannot be achieved under normal conditions. The reason for this is partly the amount of fuel and the supply of air, but it also depends on the compositions that carbon particles bind on their surface without forming chemical bonds. If the uncombusted carbon particles did not fall down through the surface of the grating, the combustion zone would decrease in the same degree, whereby the increased volume of carbon particles would affect the combustion negatively, partly through increased volume-pressure relations, partly through a lower combustion temperature, something that in practice would mean shorter retention times and an increased output of uncombusted gases and indirectly a lower heating effect.
- Characteristic for all combustions of biofuels is that the gas generation and the reductions always reach an equilibrium that is directly linked to the reaction temperature. In a combustion device according to the present invention, the combustion air is preheated in all combustion zones except the ash zone. It is always well calibrated in relation to the supplied amount of fuel in the combustion zone.
Claims (7)
- A combustion device for burning biofuels, such as pellets, briquets, wood chips and the like, comprising a combustion chamber (1), wherein said combustion chamber comprises; an input part (2) for fuel with an input pipe (7), said input pipe (7) being equipped with a feeding screw (6) for the fuel; a middle part (3) and an output part (4); means for supplying combustion air; said middle part (3) having a cylindrical shape, said middle part (3) and input part (2) for fuel being equipped with a number of apertures to receive supplied air and to direct the supplied air into the surface of the fuel and into the gas volume that is created by the combustion of the fuel; further said middle part (3) and at least parts of said output part are surrounded by a heat shield (8); said combustion chamber (1) further comprising a pipe (9); said pipe (9) running from the input part (2) over said heat shield to the output part (4) so that combustion air supplied through the pipe cools the output part (4) and heat from the middle part (3) preheats the supplied combustion air before it reaches the middle part (3), characterized in that the pipe and the heat shield (8) are disposed so that part of the supplied air first enters the input part (2) through the air holes and the remains of the supplied air is fed through the pipe towards the output part (4) and back in under the heat shield (8), essentially parallel to the middle part (3), to finally enter through an aperture in middle part (3), whereby said output part (4) has a conical shape and is provided with air supply holes to receive part of the air supplied through the pipe (9), and in that the lower part of said conically shaped output part (4) is provided with a grating (5).
- Combustion device according to claim 1, further chararacterized in that it is provided with an electrical ignition device (10) in the end part of the input part (7) to ignite the forward-fed fuel.
- Combustion device according to claims 1-2, further characterized in that said heat shield (8) surrounds at least 2/3 of the conically shaped output part (4).
- Combustion device according to claims 1-3, characterized in that the air supply apertures are designed to create a turbulent air flow.
- Combustion device according to any of the above given claims where the apertures through which air is supplied are designed to direct the airflow essentially perpendicularly to the feeding direction of the fuel mass.
- Combustion device according to any of the claims 1-5, characterized in that part of the supplied air is supplied from under the grating (5), whereby the uncombusted particles are blown away.
- Combustion device according to any of the above given claims characterized in that said means (11) for supplying air is a blower.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE0100662A SE0100662D0 (en) | 2001-02-27 | 2001-02-27 | combustion device |
| SE0100662 | 2001-02-27 | ||
| PCT/SE2002/000339 WO2002068865A1 (en) | 2001-02-27 | 2002-02-27 | Combustion device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1364160A1 EP1364160A1 (en) | 2003-11-26 |
| EP1364160B1 true EP1364160B1 (en) | 2006-03-29 |
Family
ID=20283142
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP02700955A Expired - Lifetime EP1364160B1 (en) | 2001-02-27 | 2002-02-27 | Combustion device |
Country Status (7)
| Country | Link |
|---|---|
| EP (1) | EP1364160B1 (en) |
| AT (1) | ATE321977T1 (en) |
| DE (1) | DE60210252T2 (en) |
| DK (1) | DK1364160T3 (en) |
| ES (1) | ES2264720T3 (en) |
| SE (1) | SE0100662D0 (en) |
| WO (1) | WO2002068865A1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2907198A1 (en) * | 2006-10-12 | 2008-04-18 | S N E Ronot | BURNER WITH CEREALS |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FI71408C (en) * | 1982-06-24 | 1986-12-19 | Laempoetaltio Oy | BRAENNANORDNING |
| DE3368319D1 (en) * | 1982-12-22 | 1987-01-22 | Welger Geb | Furnace for straw or similar material |
| US5678494A (en) * | 1995-03-22 | 1997-10-21 | Ulrich; Gael | Biomass-fueled furnace |
-
2001
- 2001-02-27 SE SE0100662A patent/SE0100662D0/en unknown
-
2002
- 2002-02-27 AT AT02700955T patent/ATE321977T1/en not_active IP Right Cessation
- 2002-02-27 DE DE60210252T patent/DE60210252T2/en not_active Expired - Fee Related
- 2002-02-27 DK DK02700955T patent/DK1364160T3/en active
- 2002-02-27 ES ES02700955T patent/ES2264720T3/en not_active Expired - Lifetime
- 2002-02-27 EP EP02700955A patent/EP1364160B1/en not_active Expired - Lifetime
- 2002-02-27 WO PCT/SE2002/000339 patent/WO2002068865A1/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| WO2002068865A1 (en) | 2002-09-06 |
| DE60210252T2 (en) | 2006-12-14 |
| ES2264720T3 (en) | 2007-01-16 |
| EP1364160A1 (en) | 2003-11-26 |
| DE60210252D1 (en) | 2006-05-18 |
| DK1364160T3 (en) | 2006-07-31 |
| SE0100662D0 (en) | 2001-02-27 |
| ATE321977T1 (en) | 2006-04-15 |
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