EP0009182B1 - Brûleur à gazéification - Google Patents
Brûleur à gazéification Download PDFInfo
- Publication number
- EP0009182B1 EP0009182B1 EP79103322A EP79103322A EP0009182B1 EP 0009182 B1 EP0009182 B1 EP 0009182B1 EP 79103322 A EP79103322 A EP 79103322A EP 79103322 A EP79103322 A EP 79103322A EP 0009182 B1 EP0009182 B1 EP 0009182B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- chamber
- burner
- annular
- mixing
- primary air
- 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
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M27/00—Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sound waves, or the like
- F02M27/02—Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sound waves, or the like by catalysts
-
- 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
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details
- F23D11/44—Preheating devices; Vaporising devices
- F23D11/441—Vaporising devices incorporated with burners
- F23D11/448—Vaporising devices incorporated with burners heated by electrical means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/12—Radiant burners
- F23D14/18—Radiant burners using catalysis for flameless combustion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details
- F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
- F23D14/725—Protection against flame failure by using flame detection devices
Definitions
- the invention relates to a gasification burner with an antechamber for mixing an at least partially vaporized liquid fuel with primary air, with a catalytic device adjoining the antechamber for converting the steam-air mixture into a fuel gas, with a mixing chamber adjoining the catalyst device for mixing the fuel gas with secondary air, with an annular space concentrically surrounding the anteroom, the catalyst device and the mixing chamber and separated from the anteroom by an annular wall, with a conically expanding combustion chamber and a perforated burner plate made of porous material which closes off the combustion chamber and which from the mixing chamber releases the fuel gas-air Mixture can be supplied, with a front space located in front of the anteroom, which merges into an annular channel completely surrounding the antechamber and the annular space and the catalyst device at least over part of its length, with a heat source contained in the annular channel for evaporation of the fuel and a heat source contained in the annular space for preheating the primary air during the start-up process and for supporting changes in load,
- liquid fuel is burned in two stages, whereby in the first stage only a part of the total air used - as gasification air (primary air) - is mixed with the fuel and converted into a fuel gas by catalytic partial oxidation (substoichiometric combustion). In the second stage, the fuel gas is mixed with the remaining air (combustion air, secondary air) and burned on a burner plate.
- the fuel is sprayed with a nozzle and burned with all the air in a combustion chamber. Since the atomizing power of the nozzle can only be varied within narrow limits, such household burners cannot be regulated continuously down to low outputs. Rather, they are designed for maximum performance and are regulated with a two-point control when the heating requirement is low in burst operation. As a result, larger boilers are required as energy storage for the breaks in operation, furthermore the repeated starting of the burner causes a strong temperature change of the materials, an increased soot and pollutant load of the boiler, chimney and exhaust gases as well as an excessive energy requirement during electrical ignition.
- the gasification burner proposed in EP-B1-4055 only has to be started at the beginning of a heating period and can then be continuously reduced to very low outputs in accordance with the heating requirement, thereby avoiding the disadvantages mentioned. Furthermore, a substantial reduction in the emission of pollutants, for example unburned hydrocarbons and nitrogen oxides, is achieved in the course of the reaction during the combustion. The total air required can be limited to the air required for stoichiometric combustion, which means that high combustion temperatures can be achieved.
- FIG. 1 A preferred embodiment of the gasification burner proposed in EP-B1-4055 is shown in FIG. 1 and, as already mentioned, essentially consists of two stages, namely a gasification stage with a centrally arranged reactor chamber 2 (catalyst device) containing a catalyst and one Combustion part, which comprises a mixing chamber 3, an ignition chamber 7 and a flared combustion chamber 8 with a final porous, perforated burner plate 9.
- the catalyst device 2 is preceded by an antechamber 1 at the inlet 14 for mixing the fuel with primary air.
- the antechamber 1 is laterally delimited by an annular wall 5 and connected via radial channels 6 in this annular wall to an annular space 4, which concentrically surrounds the antechamber 1, the catalyst device 2 and the mixing space 3.
- the primary air is supplied to the antechamber 1 through the annular space 4.
- a front space 10 is connected upstream of the antechamber 1, which merges into an annular channel 11, which completely surrounds the antechamber 1 and the annular space 4 and the catalyst device 2 over at least part of its length.
- the fuel is at least partially evaporated at a first heat source 12 arranged in the annular duct 11 and mixed in the antechamber 1 with the primary air, which is preheated at a second heat source B arranged in the annular space 4, at a first homogenization device 13, for example a swirl orifice.
- the fuel gas generated in the catalyst device 2 is passed into the mixing chamber 3 and mixed there with secondary air supplied at a second homogenization device 24, for example a further swirl orifice.
- the reactor chamber 2 (catalyst device) has a catalytically inactive container A, in the end faces of inlet bores 14 and outlet bores 15 are arranged. Furthermore, a perforated disc 16 can be arranged between the mixing chamber 3 and the ignition chamber 7 as a kickback protection.
- the ignition chamber 7 can also be separated from the combustion chamber 8 by a perforated wall 17.
- a fuel connection piece 19 is provided for supplying the fuel to the annular channel 11 (evaporation chamber), a secondary air connection piece 23 for supplying the secondary air to the mixing chamber 3 and a primary air supply connection piece 26 for supplying the primary air to the annular space 4 (preheating chamber). Furthermore, a further connection piece 27 for an ignition device is fastened to the wall of the ignition chamber 7.
- a catalytically inactive lining C for example made of ceramic, can advantageously be provided in the mixing chamber 3.
- the housing of the proposed gasification burner is advantageously composed of several parts, for example a cylindrical first housing part 18 surrounding the first stage with a front cover 20, a cylindrical middle part 21 surrounding the mixing chamber 3 and a cylindrical end part 25 which has a conical surrounding the combustion chamber 8 Extension carries.
- These housing parts are advantageously made of metal, for example stainless steel.
- the wall 22 between the mixing space 3 and the annular space 4 is designed to be thermally conductive in order to preheat the primary air in the combustion part.
- the proposed gasification burner is susceptible to malfunctions in some cases. For example, if the fuel supply is temporarily suspended, there is no short-term combustion in the combustion part. The primary air supplied is then not preheated sufficiently so that cold air is flushed through the catalyst part and cooled. When the fuel supply is restarted, the catalyst device then does not work satisfactorily, so that the fuel is only incompletely converted into fuel gas and burner faults, in particular soot formation in the combustion part, occur. Furthermore, it is precisely the advantage of this burner that very high combustion temperatures can be achieved by stoichiometric air supply, but these high temperatures entail the risk that the materials used are destroyed.
- the burner plate 9 or the perforated wall 17 can jump and even the metal housing can be welded on.
- the burner is no longer safe to touch, since there is a considerable risk of injury when touching the burner housing.
- the heat losses occurring on the housing also mean a reduction in the efficiency of the burner.
- the object of the invention is to increase the operational safety of a gasification burner of the type mentioned, which has, inter alia, an annular space, a mixing space, an ignition chamber and a combustion space, as well as an annular wall provided with radial channels and a burner plate.
- annular space also surrounds the ignition chamber and the conically widening combustion chamber in an annular manner and extends up to the vicinity of the base plate, in that a primary air supply connection opens into the annular space and that guide walls are arranged in the annular space, which guide the primary air flow to be supplied from the primary air supply nozzle in a spiral or meandering flow path around the combustion chamber and the ignition chamber to the radial channels of the ring wall.
- FIGS. 2 and 3 a particularly preferred embodiment of the gasification burner according to the invention is shown.
- the improvements which the gasification burner according to the invention has - compared to the gasification burner according to EP-B1-4055 - relate to the combustion part of the burner, ie the mixing chamber 3, the ignition chamber 7, the combustion chamber 8 and the burner plate 9 and the associated housing parts (see. Fig. 1).
- 2 shows a longitudinal section through the combustion part of the gasification burner according to the invention, in FIG. 3 a cross section corresponding to line 111-111 in FIG. 2.
- the mixing chamber which is divided into two sub-rooms 3 'and 3 "by a homogenizing device (swirl orifice 24' with oblique slots 30).
- Fuel gas is supplied to the mixing chamber by the gasification section (arrow 31) which is mixed with secondary air (arrow 32)
- the mixture is passed through a non-return device 16 ', for example a perforated disk made of porous ceramic, into the ignition chamber 7', from where it flows through a perforated wall 17 ', which is advantageous as perforated ceramic plate is formed in the conically widening combustion chamber 8 'and through the burner plate 9'.
- the fundamental improvement is in the gasification burner according to the invention. achieved in that the annular space 4 ' also surrounds the ignition chamber 7' and the combustion chamber 8 'and extends into the vicinity of the burner plate 9'. There, the primary air supply nozzle 26 'is arranged so that the primary air in the immediate vicinity of the hot burner plate 9' comes into contact with the heated housing part 34 and cools the housing. Walls 35 are arranged in the annular space 4 ', which make the annular space a spiraling or meandering flow path around the combustion chamber 8' and the ignition chamber 7 '. This flow path can be realized in such a way that a thread-like groove is milled into the housing part 34 and a conical cover plate 36 is fastened on the housing part.
- the primary air flowing in through the connecting piece 26 ′ comes into intensive thermal contact with the housing part 34 on this tortuous flow path and cools it before it - according to FIG. 1 - enters the antechamber 1 through the radial channels 6 of the ring wall 5.
- This configuration of the burner according to the invention leads on the one hand to a better preheating of the primary air and on the other hand prevents overheating of the housing part 34, which can therefore be made of metal, for example stainless steel, without the risk of material softening at the high combustion temperatures.
- the ignition chamber 7 ' also widens conically in the flow direction, the outlet cross section of the ignition chamber being equal to the inlet cross section of the combustion chamber.
- the ignition chamber 7 ' is particularly advantageously separated from the combustion chamber 8' by the hole wall 17 'already mentioned, the perforated area of the burner plate 9' being larger than the perforated area of the hole wall 17 '. Since the flow cross section of the fuel gas / air mixture between the mixing chamber 3 'and the burner plate 9' is constantly expanding, the thermal load on the perforated wall is lower than in the gasification burner according to FIG. 1, and the risk of destruction of this perforated wall by thermal stresses is thus reduced .
- the perforated wall 17 ' is exposed to particularly high temperatures during burner operation, which can be recognized by a bright glow.
- the burner plate 9 'and possibly also the perforated wall 17' are composed of several plate parts 37, 38 which are held together by tongue and groove 39.
- the burner housing of the gasification burner according to the invention is preferably made of metal.
- the ignition chamber 7 'and the combustion chamber 8' can also wear a ceramic lining.
- This ceramic lining advantageously consists of individual ceramic rings 40, 41, which can also be held together by tongue and groove.
- the flame monitoring device can be optical in nature.
- one end of an observation tube 42 can be attached to an opening in the ignition chamber wall, the other end of which carries a photocell (not shown in FIG. 2) which emits a signal for trouble-free operation when the perforated wall 17 'is glowing and when it goes out the perforated wall 17 'a fault signal which can be used, for example, to switch off the fuel supply.
- a light guide can be provided between the observation tube 42 and the photocell in order to protect the photocell from the heat of the burner.
- the housing part 34 can also advantageously be provided with a wide flange 50 at the end adjoining the gasification part, that is to say at the level of the mixing chamber, which projects laterally beyond the other housing parts.
- This flange can be used Attach the burner to the wall of a boiler, an opening being provided in the boiler wall, into which the burner with the flow part behind the flange can be inserted and which is closed by the flange (threaded holes 43).
- the combustion part of the burner is then arranged inside the boiler, so that the thermal radiation from the burner part can also be used for heating purposes. Since the housing parts now inside the boiler are cooled by the primary air flow, there is no fear of overheating of these parts.
- the primary air supply takes place by means of at least one supply channel 45 which passes through the flange and leads to the primary air supply connection piece 26 '.
- the partial space of the annular space 4' located in the combustion part is connected via holes 48 to the part of the annular space located in front of it.
- the secondary air is supplied by means of at least one feed channel 46 which also extends through the flange and leads to the secondary air connection of the mixing chamber 3 '.
- openings 47 are provided in the flange 50 for the introduction of ignition electrodes, which are arranged on the ignition chamber wall, and optionally for flame monitoring.
- Mullite can be used as the material for the ceramic parts in the gasification burner according to the invention; Up to 50% by weight of bikorite (trademark) can advantageously be added to the mullite to increase the heat resistance.
- Aluminum oxide and alumina fireclay masses (for example so-called sieve core masses) are also suitable.
- other highly heat-resistant ceramics for example based on zirconium dioxide, or silicon carbide can also be used.
- the burner plates and the perforated wall advantageously consist of the same material as the ceramic linings.
- the primary air quantity is set to an air ratio of approximately 0.1 and the secondary air quantity to an air ratio of approximately 1.0, temperatures of approximately 1740 ° C. are reached. Despite these high temperatures, there is no fear of thermal damage to the burner components. In addition, the preheating of the primary air and the reduction in thermal radiation improve the efficiency of the burner.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Spray-Type Burners (AREA)
- Glass Compositions (AREA)
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT79103322T ATE1205T1 (de) | 1978-09-21 | 1979-09-06 | Vergasungsbrenner. |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2841105 | 1978-09-21 | ||
| DE2841105A DE2841105C2 (de) | 1978-09-21 | 1978-09-21 | Vergasungsbrenner |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0009182A1 EP0009182A1 (fr) | 1980-04-02 |
| EP0009182B1 true EP0009182B1 (fr) | 1982-06-16 |
Family
ID=6050052
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP79103322A Expired EP0009182B1 (fr) | 1978-09-21 | 1979-09-06 | Brûleur à gazéification |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US4421476A (fr) |
| EP (1) | EP0009182B1 (fr) |
| AT (1) | ATE1205T1 (fr) |
| CA (1) | CA1123333A (fr) |
| DE (1) | DE2841105C2 (fr) |
| DK (1) | DK149412C (fr) |
| NO (1) | NO152882C (fr) |
Families Citing this family (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3006048A1 (de) * | 1980-02-18 | 1981-08-20 | Siemens AG, 1000 Berlin und 8000 München | Verfahren zum betrieb einer heizkesselanlage und dafuer geeignete vorrichtung |
| DE3332572C2 (de) * | 1983-09-09 | 1986-10-30 | Insumma Projektgesellschaft mbH, 8500 Nürnberg | Brennwertgerät für Kohlenwasserstoffe |
| DE3339741A1 (de) * | 1983-09-09 | 1985-05-15 | Insumma Projektgesellschaft mbH, 8500 Nürnberg | Brennwertgeraet fuer kohlenwasserstoffe |
| US5059115A (en) * | 1985-06-13 | 1991-10-22 | British Gas Plc | Fuel fired burner |
| US4799879A (en) * | 1985-12-02 | 1989-01-24 | Solaronics Vaneecke | Radiant burners with a ceramic frame |
| US5766276A (en) * | 1989-06-27 | 1998-06-16 | Radiamon S.A. | Method for supplying natural gas to a catalytic burner and device for implementing said method |
| US5667374A (en) * | 1992-10-16 | 1997-09-16 | Process Combustion Corporation | Premix single stage low NOx burner |
| DE4440494A1 (de) * | 1994-11-12 | 1996-05-15 | Bosch Gmbh Robert | Wassererhitzer mit einem katalytischen Gasbrenner |
| US5997285A (en) * | 1996-08-19 | 1999-12-07 | Gas Research Institute | Burner housing and plenum configuration for gas-fired burners |
| US5857320A (en) * | 1996-11-12 | 1999-01-12 | Westinghouse Electric Corporation | Combustor with flashback arresting system |
| DE19813896B4 (de) * | 1998-03-28 | 2005-12-29 | Robert Bosch Gmbh | Gasbrenner |
| FR2791416B1 (fr) * | 1999-03-25 | 2001-06-15 | Sunkiss Aeronautique | Dispositif de combustion catalytique emettant un rayonnement infra-rouge |
| KR100662168B1 (ko) * | 1999-08-19 | 2006-12-27 | 마츠시타 덴끼 산교 가부시키가이샤 | 촉매연소장치 및 연료기화장치 |
| EP1510761A1 (fr) * | 2003-08-13 | 2005-03-02 | Siemens Aktiengesellschaft | Procédé de combustion d'un combustible fluide ainsi que brûleur, en particulier de turbine à gaz, pour la mise en oeuvre du procédé |
| DE102004049903B4 (de) * | 2004-10-13 | 2008-04-17 | Enerday Gmbh | Brennervorrichtung mit einem Porenkörper |
| DE602006010700D1 (de) * | 2006-09-06 | 2010-01-07 | Electrolux Home Prod Corp | Gasbrenner für Kochgeräte |
| US20080141584A1 (en) * | 2006-12-14 | 2008-06-19 | Texaco Inc. | Methods for Using a Catalyst Preburner in Fuel Processing Applications |
| RU2338121C1 (ru) * | 2007-02-21 | 2008-11-10 | Государственное образовательное учреждение высшего профессионального образования "Московский государственный горный университет" (МГГУ) | Устройство для сжигания взрывоопасных газовых смесей |
| CN101363624B (zh) * | 2007-08-06 | 2011-05-25 | 国际壳牌研究有限公司 | 燃烧器 |
| WO2010003904A1 (fr) * | 2008-07-08 | 2010-01-14 | Nv Bekaert Sa | Brûleur radiant amélioré |
| GB2474147B (en) * | 2008-07-25 | 2012-05-16 | Hatch Ltd | Apparatus for stabilization and deceleration of supersonic flow incorporating a diverging nozzle and perforated plate |
| DE102013220654B4 (de) * | 2013-10-14 | 2023-10-19 | Eberspächer Climate Control Systems GmbH | Brennkammerbaugruppe für einen Verdampferbrenner |
| DE102013220655B4 (de) * | 2013-10-14 | 2016-01-14 | Eberspächer Climate Control Systems GmbH & Co. KG | Bodenbaugruppe für eine Brennkammerbaugruppe eines Verdampferbrenners |
| US20160258619A1 (en) * | 2015-03-03 | 2016-09-08 | Willie H. Best | Multiple plenum gas burner |
| DE102016116687B4 (de) * | 2016-09-07 | 2019-12-05 | Eberspächer Climate Control Systems GmbH & Co. KG | Brennkammerbaugruppe für einen Verdampferbrenner |
| US11277090B1 (en) * | 2017-12-22 | 2022-03-15 | Jx Crystals Inc. | Multi fuel thermophotovoltaic generator incorporating an omega recuperator |
| CN111867717B (zh) | 2018-03-07 | 2021-07-06 | 沙伯环球技术有限公司 | 烃气热解转化的方法和反应器 |
| CN113195092B (zh) * | 2018-10-23 | 2022-04-29 | 沙伯环球技术有限公司 | 用于烃转化的方法和反应器 |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB893739A (en) * | 1959-05-04 | 1962-04-11 | Colt Ventilation Ltd | Improvements in heat generators |
| US3155142A (en) * | 1961-02-13 | 1964-11-03 | Minnesota Mining & Mfg | Radiant gas burner |
| DE1254279B (de) * | 1962-11-23 | 1967-11-16 | Erhard Schwarze | OElbrenner |
| GB1082823A (en) * | 1964-08-26 | 1967-09-13 | Minnesota Mining & Mfg | Radiant gas burner assembly |
| US3439996A (en) * | 1965-06-09 | 1969-04-22 | Solaronics Inc | Tile assembly for radiant gas burners |
| US3484189A (en) * | 1966-07-14 | 1969-12-16 | Universal Oil Prod Co | Method and means for thermal incineration of a contaminated air stream |
| DE1962839C3 (de) * | 1969-12-15 | 1974-04-18 | Universal Oil Products Co., Des Plaines, Ill. (V.St.A.) | Vorrichtung zur Verbrennung von Abgas |
| US3825913A (en) * | 1972-03-31 | 1974-07-23 | Electronics Corp America | Fuel burner supervisory system |
| DE2308753A1 (de) * | 1973-02-22 | 1974-09-05 | Volkswagenwerk Ag | Reaktionsvergaser fuer brennkraftmaschinen |
| DE2510091C2 (de) * | 1974-03-11 | 1983-11-24 | Mitsubishi Denki K.K., Tokyo | Verbrennungseinrichtung |
| DE2614673C3 (de) * | 1976-04-05 | 1981-06-25 | Siemens AG, 1000 Berlin und 8000 München | Startvorrichtung für einen Spaltgasgenerator |
| DE2811273C2 (de) * | 1978-03-15 | 1980-01-03 | Siemens Ag, 1000 Berlin Und 8000 Muenchen | Vergasungsbrenner |
-
1978
- 1978-09-21 DE DE2841105A patent/DE2841105C2/de not_active Expired
-
1979
- 1979-09-06 EP EP79103322A patent/EP0009182B1/fr not_active Expired
- 1979-09-06 AT AT79103322T patent/ATE1205T1/de not_active IP Right Cessation
- 1979-09-19 NO NO793004A patent/NO152882C/no unknown
- 1979-09-20 CA CA335,988A patent/CA1123333A/fr not_active Expired
- 1979-09-21 DK DK393679A patent/DK149412C/da not_active IP Right Cessation
-
1982
- 1982-05-10 US US06/376,569 patent/US4421476A/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CA1123333A (fr) | 1982-05-11 |
| DK393679A (da) | 1980-03-22 |
| NO793004L (no) | 1980-03-24 |
| DE2841105A1 (de) | 1980-04-10 |
| US4421476A (en) | 1983-12-20 |
| DE2841105C2 (de) | 1986-10-16 |
| NO152882C (no) | 1985-12-04 |
| DK149412C (da) | 1986-11-10 |
| ATE1205T1 (de) | 1982-07-15 |
| DK149412B (da) | 1986-06-02 |
| EP0009182A1 (fr) | 1980-04-02 |
| NO152882B (no) | 1985-08-26 |
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Legal Events
| Date | Code | Title | Description |
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