EP0605645B1 - Verfahren und vorrichtung zur verbrennung eines gasgemisches - Google Patents

Verfahren und vorrichtung zur verbrennung eines gasgemisches Download PDF

Info

Publication number
EP0605645B1
EP0605645B1 EP92921500A EP92921500A EP0605645B1 EP 0605645 B1 EP0605645 B1 EP 0605645B1 EP 92921500 A EP92921500 A EP 92921500A EP 92921500 A EP92921500 A EP 92921500A EP 0605645 B1 EP0605645 B1 EP 0605645B1
Authority
EP
European Patent Office
Prior art keywords
burner plate
gas
regions
flow resistance
plate
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
Application number
EP92921500A
Other languages
English (en)
French (fr)
Other versions
EP0605645A1 (de
Inventor
Paulus Jacobus Vloon
André IN HET VELD
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nefit Buderus BV
Original Assignee
Nefit Fasto BV
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 Nefit Fasto BV filed Critical Nefit Fasto BV
Publication of EP0605645A1 publication Critical patent/EP0605645A1/de
Application granted granted Critical
Publication of EP0605645B1 publication Critical patent/EP0605645B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/48Nozzles
    • F23D14/58Nozzles characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration
    • 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
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/72Safety devices, e.g. operative in case of failure of gas supply
    • F23D14/74Preventing flame lift-off

Definitions

  • the invention relates to a method and installation for the combustion of a combustible gas mixture containing a hydrocarbon or hydrogen gas, sufficient air for a complete combustion of the hydrocarbon or hydrogen gas, and an essentially non-combustible ballast gas, which gas mixture is supplied under pressure to a pressure space which is at least partially bounded by a burner plate with an inlet side in the pressure space and an outlet side lying opposite the inlet side for the gas mixture flowing through essentially in a direction at right angles to the plane of the burner plate.
  • a method and installation are known from EP-A-0 092 838.
  • a first principle is that heat is drawn from the flame by a surface which is placed in or near the flames, and which thereby begins to glow and transfers the heat drawn from the flame by means of radiation to an element to be heated, for example a heat exchanger.
  • an element to be heated for example a heat exchanger.
  • Only a limited output per unit surface area can be obtained in this way, and therefore a compact burner cannot be achieved.
  • the stability of the combustion is a problem during output modulation.
  • a second principle for obtaining a lower flame temperature is to increase the air factor to a value greater than 1, i.e. the combustible gas mixture contains more air than can react with the combustible component of the gas during complete combustion.
  • the use of high air factors in burners according to the prior art is not possible just like that.
  • air factors greater than 1.4 it is difficult to obtain a stable flame, due to the fact that the low flame temperature and low temperature of the burner surface resulting from the high air factor are insufficient to ignite the gas mixture stably, and the high gas velocity also resulting from the high air factor leads to blowing away of the flame.
  • the object of the invention is to provide a method and an installation which permit combustion of a combustible gas mixture containing an essentially non-combustible ballast gas, in particular a gas mixture with an air factor greater than 1.4 or a gas mixture to which through a process of recirculation exhaust gas is added, while retaining a high specific output and a stable, resonance-free combustion.
  • Another object of the invention is to provide the possibility of a great modulation of the output over a large range.
  • Such a burner plate is known in itself from EP-A-0 267 671, and is used in an atmospheric gas burner for a solid fuel effect gas fire. Quite surprisingly, experiments have shown that with such a burner plate, when used in a burner in which a combustible gas mixture containing an essentially non-combustible ballast gas is supplied under pressure to the burner plate, a stable and resonance-free combustion can be attained.
  • the burner plate is used in an installation comprising a pressure space to which the combustible gas mixture is supplied through a feed duct, and a combustion space in which the gas mixture is burned, both spaces being at least partially bounded by the burner plate, and compression means for generating a pressure in the pressure space which is higher than the pressure in the combustion space, the burner plate having an inlet side in the pressure space and an outlet side in the combustion space for the gas mixture flowing through essentially in a direction at right angles to the plane of the burner plate, and ignition means which are fitted at the outlet side of the burner plate in the combustion space.
  • regions with a significantly lower gas velocity than elsewhere in the flames are found between the flames and near the edges of the foot of the flames. These regions with low flow velocity remain intact up to a great distance from the burner plate and ensure a stable ignition along the edge of the flame. Such regions are absent in a burner in which the flames do fuse together, so that in such a burner other stabilisation means, e.g. glowing areas or separate glowing elements, are needed.
  • the regions with a large number of channels for the gas throughput have a low, but not negligible flow resistance.
  • This flow resistance causes a pressure drop in the gas flow, with the result that pressure fluctuations over the burner plate, which occur particularly in closed appliances, during combustion have less effect on the gas flow velocity and gas distribution through the burner plate, and flame resonances are thus suppressed.
  • An installation according to the invention therefore permits a stable combustion, and the output can be modulated over a large range.
  • the burner plate has a low surface temperature.
  • the burner plate can therefore have a long service life, and no strict standards as regards mechanical properties need to be met.
  • the ballast gas can be air, leading to an air factor of the combustible gas mixture of more than one, or part of the gas mixture after combustion thereof can be added to the combustible gas mixture to serve as a ballast gas.
  • the combustion space of the installation is connected to the feed duct for the combustible gas mixture.
  • Another suitable ballast gas is water, and for special burner applications other ballast gases may be used. It will be clear that a ballast gas may in itself be a mixture of different gases.
  • the narrow channels in the burner plate are labyrinth-shaped in the regions with a low flow resistance, i.e. the axis of a channel in general does not form a straight line, and channels can be interconnected.
  • These regions can be formed by a porous material, such as ceramic material.
  • the narrow channels in the burner plate are straight and run parallel to each other in a direction at right angles to the plane of the burner plate. In this way it is possible to make the channels by cutting with a laser beam or water jet or the like.
  • a hydraulic diameter of the channels which is smaller than 0.4 mm, and is preferably smaller than 0.2 mm, is envisaged.
  • the burner plate is preferably designed in such a way that the smallest cross-section of each region with a low flow resistance between the inlet and outlet side, viewed in the plane of the burner plate, is at least about 5 mm 2 , and the sum of these smallest cross-sections of all regions with low flow resistance is at most 70% of the burner plate surface area at the outlet side.
  • the burner plate is designed in such a way that the abovementioned sum of the smallest cross-sections is at least about 10% and at most about 50% of the burner plate surface area at the outlet side, and more particularly these lowest and highest percentages can be 20 and 40, respectively.
  • the regions in the burner plate with a low flow resistance advantageously have an essentially round cross-section, viewed in the plane of the burner plate, with the result that flames with a natural shape can develop.
  • the plate consists of a base plate of an essentially gastight material, which base plate is provided with holes of which the edges determine the boundaries of the regions with a low flow resistance, and also consists of a gas-permeable structure extending over at least the cross-section of the holes.
  • the gas-permeable structure can be made in the form of an essentially flat plate covering the abovementioned base plate.
  • the burner plate can be assembled in a particularly simple way from two plates.
  • Another possible embodiment comprises a gas-permeable plate which is locally densified in order to form the regions with a high flow resistance there. This again makes it possible to produce a thin burner plate, and in addition the plate forms one self-supporting entity.
  • the gas-permeable plate can be densified locally in a simple way by impregnating it with a filling material.
  • the densification can also be obtained by compressing the plate at the places where regions with a high flow resistance have to be formed.
  • the structure of the gas-permeable plate in this embodiment can be a foam structure, so that a simple manufacturing process is possible.
  • the gas-permeable plate can also be two foam structures with different degrees of gas permeability.
  • the regions with a low flow resistance can advantageously be made of metal fibres or aluminium oxide fibres, on account of the resistance of these materials to the prevailing temperatures.
  • Metal fibres can also be impregnated, which is advantageous, inter alia, in the abovementioned embodiment, in which the burner is one plate densified locally by impregnation.
  • Aluminium oxide fibres can be applied in an excellent way by spraying onto a carrier, which makes them very suitable for use in combination with a base plate according to an earlier described embodiment.
  • Fig. 1 shows a boiler 21, comprising an air inlet duct 22 and a gas inlet duct 23, which open out in a mixing chamber 24 for mixing the air and gas supplied to it.
  • the mixing chamber 24 is connected to a feed duct 25, in which a fan 26 which can pressurize the combustible gas/air mixture is situated.
  • the feed duct 25 ends in pressure space 27, which is bounded by a burner plate 6.
  • a combined igniter and temperature sensor 28 is situated in a combustion space 29.
  • a heat exchanger 30 Adjacent to this combustion space 29 is a heat exchanger 30, through which the hot combustion gases coming from separate flames can flow and transfer heat to another medium also flowing through the heat exchanger 30, following which the combustion gases can flow away through a discharge duct 31.
  • This boiler 21 can be used, for example, as a central heating boiler, and can then be fired by natural gas. To lower the flame temperature in the burner, excess air may be supplied to the mixing chamber 24, or a part of the exhaust gases may be recirculated by means of a recirculation duct 32 shown in dashed lines connecting the discharge duct 31 to the feed duct 25. In this way essentially non-combustible ballast gas is added to the combustible gas mixture in feed duct 25.
  • the recirculation duct 32 may comprise a control valve 33 for setting the flow in the duct 32.
  • a mixing chamber 24 strictly speaking is unnecessary, since the fan 26 can perform the same function.
  • a fan may be situated in the discharge duct 31 for generating the same gas flows in the boiler 21.
  • the recirculation duct 32 may, instead of being connected to the feed duct 25, be connected to the mixing chamber 24, the air inlet duct 22 or the gas inlet duct 23.
  • Fig. 2 shows a rectangular burner plate 1 with an inlet side 2 and an outlet side 3 for a gas mixture which can flow in the direction indicated by arrow A through the regions formed by narrow parallel, straight channels with a low flow resistance 4.
  • the reference number 5 indicates the regions with a high flow resistance.
  • the burner plate can be a metal plate in which the channels are made by laser cutting.
  • Fig. 3 shows a rectangular burner plate 6, again provided with an inlet side 7 and an outlet side 8, through which a gas mixture can flow in the direction indicated by an arrow B.
  • This burner plate is composed of a metal plate 9, which is perforated with square holes 10, and a porous plate 11 which forms a gas-permeable structure and is made of sprayed-on aluminium oxide fibres.
  • the gas flow direction can also be selected opposite to the direction of arrow B.
  • reference numeral 8 indicates the inlet side
  • reference numeral 7 indicates the outlet side.
  • Fig. 4 shows a rectangular burner plate 12, consisting of a perforated base plate 13 which is provided with a porous layer 14 covering the top and bottom side of the plate and filling up the perforations in the base plate.
  • Fig. 5 shows a burner plate 15 similar to the burner plate 6 of Fig. 3, and differing from it in that round conical holes 17 are provided in the metal plate 16.
  • Fig. 6 shows a burner plate 18 which consists of a metal fibre mat which is densified to form regions with high flow resistance 19, which bound regions with low flow resistance 20.
  • a burner plate made up of a metal plate perforated with round holes and covered with a porous plate was tested.
  • the configuration of this plate and the test conditions are given in Table 1, in which the emission of harmful substances is also stated, for an output which is held constant, and as a function of the air factor. It can be seen clearly that a considerable reduction of this emission can be achieved compared with known combustion methods, where the air factor generally was lower and never more than 1.4.
  • Table 2 further shows the influence of the output on the harmful emission, for a combustion method according to the invention. It can be seen from this that the output can be varied over a large range, while the harmful emission remains low and virtually constant.
  • the burner plates shown in the drawing are all made flat. Of course, the plates can also be a different shape, such as a curved, ribbed or bent shape. It is, however, essential that the burner plates according to the invention should be designed in such a way that during use in a burner flames which are at least almost completely separate from each other occur at the outlet side of the burner plate.
  • Table 1 Test results with a burner plate made up of a metal plate perforated with round holes and covered with a porous plate, the air factor being varied. No recirculation of exhaust gases. configuration width of metal plate 160 mm length of metal plate 200 mm thickness of metal plate 2 mm number of holes 150 hole diameter 8 mm surf.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)

Claims (17)

  1. Verfahren zum Verbrennen eines brennbaren Gasgemisches mit Hilfe einer Brennerplatte (1; 6; 12; 15; 18) mit einer Einlaßseite (2; 7) und einer der Einlaßseite gegenüberliegenden Auslaßseite (3; 8) für das durch im wesentlichen in einer Richtung rechtwinklig zur Ebene der Brennerplatte hindurchströmende Gasgemisch, wobei in der Brennerplatte zwischen der Einlaßseite und der Auslaßseite ein oder mehrere Bereiche (4; 20) ausgebildet sind, die eine große Anzahl von schmalen Kanälen für den Gasdurchfluß enthalten, die einen vorbestimmten geringen Durchflußwiderstand, von der Einlaßseite zur Auslaßseite der Brennerplatte gesehen, besitzen, und die durch Bereiche (5; 19) mit einem hohen Durchflußwiderstand begrenzt sind, wobei die Bereiche mit einem geringen Durchflußwiderstand mindestens in einem solchen Abstand voneinander angeordnet sind, daß bei einer Verbrennung des Gasgemisches an der Auslaßseite der Brennerplatte von jedem Bereich mit einem geringen Durchflußwiderstand eine Flamme auftritt, die mindestens nahezu vollständig von den Flammen der anderen Bereiche mit geringem Durchflußwiderstand getrennt sind,
    dadurch gekennzeichnet, daß das Gasgemisch, das ein Kohlenwasserstoff- oder Wasserstoff-Gas, ausreichend Luft für eine vollständige Verbrennung des Kohlenwasserstoff- oder Wasserstoff-Gases und ein im wesentlichen nicht brennbares Ballast-Gas enthält, unter Druck in einen Druckraum (27) eingespeist wird, der mindestens teilweise durch die Einlaßseite (2; 7) der Brennerplatte (1; 6; 12; 15; 18) begrenzt ist.
  2. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß das Ballast-Gas Luft ist.
  3. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß ein Teil des Gasgemisches nach der Verbrennung dem brennbaren Gasgemisch hinzugefügt wird, damit es als Ballast-Gas dient.
  4. Anlage zum Verbrennen eines brennbaren Gasgemisches, das ein Kohlenwasserstoff- oder Wasserstoff-Gas, ausreichend Luft für eine vollständige Verbrennung des Kohlenwasserstoff- oder Wasserstoff-Gases und ein im wesentlichen nicht brennbares Ballast-Gases enthält, mit
    einem Druckraum (27), dem das brennbare Gasgemisch über eine Zuführleitung (25) zugeführt wird, und einem Verbrennungsraum (29), in dem das Gasgemisch verbrannt wird, wobei beide Räume mindestens teilweise durch eine Brennerplatte (1; 6; 12; 15; 18) begrenzt sind, und einer Kompressionsvorrichtung (26) zum Erzeugen eines Druckes im Druckraum (27), der höher ist als der Druck im Verbrennungsraum (29), wobei die Brennerplatte eine Einlaßseite im Druckraum (27) und eine Auslaßseite im Verbrennungsraum (29) für das durch im wesentlichen in einer Richtung rechtwinklig zur Ebene der Brennerplatte hindurchströmende Gasgemisch, und eine Zündvorrichtung (28), die an der Auslaßseite der Brennerplatte im Verbrennungsraum (29) angeordnet ist, aufweist,
    dadurch gekennzeichnet, daß zwischen der Einlaßseite (2; 7) und der Auslaßseite (3; 8) der Brennerplatte (1; 6; 12; 15; 18) ein oder mehrere Bereiche gebildet werden, die eine große Anzahl von schmalen Kanälen für den Gasdurchfluß enthalten, daß die Bereiche (4; 20) einen vorbestimmen geringen Durchflußwiderstand, betrachtet von der Einlaßseite zur Auslaßseite der Brennerplatte, aufweisen, und daß sie durch Bereiche (5; 19) begrenzt sind, die einen hohen Durchflußwiderstand besitzen, wobei die Bereiche mit geringem Durchflußwiderstand mindestens in einem solchen Abstand voneinander angeordnet sind, daß bei einer Verbrennung des Gasgemisches an der Auslaßseite der Brennerplatte aus jedem Bereich mit geringem Durchflußwiderstand eine Flamme auftritt, die mindestens nahezu vollständig von den Flammen der anderen Bereiche mit geringem Durchflußwiderstand getrennt sind.
  5. Anlage nach Anspruch 4, dadurch gekennzeichnet, daß der Verbrennungsraum (29) mit der Zuführleitung (25) verbunden ist, um einen Teil des Gasgemisches nach dessen Verbrennung dem brennbaren Gasgemisch hinzuzufügen, damit es als Ballast-Gas wirkt.
  6. Anlage nach Anspruch 4 oder 5, dadurch gekennzeichnet, daß die schmalen Kanäle in der Brennerplatte ein Labyrinth ausbilden.
  7. Anlage nach Anspruch 4 oder 5, dadurch gekennzeichnet, daß die schmalen Kanäle in der Brennerplatte (1) geradlinig ausgebildet sind und parallel zueinander in einer Richtung rechtwinklig zur Ebene der Brennerplatte verlaufen.
  8. Anlage nach einem der Ansprüche 4 - 7, dadurch gekennzeichnet, daß der kleinste Querschnitt eines jeden Bereiches (4; 20) in der Brennerplatte (1; 6; 12; 15; 18) mit einem geringen Durchflußwiderstand zwischen der Einlaßseite (2; 7) und der Auslaßseite (3; 8), in der Ebene der Brennerplatte gesehen, mindestens etwa 5 mm2 beträgt, und daß die Summe dieser kleinsten Querschnitte aller Bereiche mit geringem Durchflußwiderstand höchstens etwa 70% der Oberfläche der Brennerplatte an der Auslaßseite, insbesondere mindestens etwa 10% und höchstens etwa 50% der Oberfläche der Brennerplatte an der Auslaßseite oder noch spezieller mindestens etwa 20% und höchstens 40% der Oberfläche der Brennerplatte an der Auslaßseite beträgt.
  9. Anlage nach einem der Ansprüche 4 - 8, dadurch gekennzeichnet, daß die Bereiche (4; 20) in der Brennerplatte (1; 6; 12; 15; 18) mit einem geringen Durchflußwiderstand einen im wesentlichen runden Querschnitt, in der Ebene der Brennerplatte gesehen, aufweisen.
  10. Anlage nach einem der Ansprüche 4 - 9, dadurch gekennzeichnet, daß die Brennerplatte aus einer Basisplatte (9; 13; 16) aus im wesentlichen gasdichtem Material besteht, daß die Basisplatte mit Löchern (10; 17) versehen ist, deren Ränder die Begrenzungen der Bereiche (4; 20) mit geringem Durchflußwiderstand festlegen, und daß die Basisplatte aus einem gasdurchlässigen Gefüge (11; 14) besteht, das sich über mindestens den Querschnitt der Löcher erstreckt.
  11. Anlage nach Anspruch 10, dadurch gekennzeichnet, daß das gasdurchlässige Anordnung (11, 14) die Form einer im wesentlichen flachen, die Basisplatte überdeckenden Platte hat.
  12. Anlage nach Anspruch 10 oder 11, dadurch gekennzeichnet, daß die Löcher (10; 17) in der Basisplatte (9; 13; 16) mindestens teilweise mit dem gasdurchlässigen Gefüge (11; 14) gefüllt sind.
  13. Anlage nach einem der Ansprüche 10 - 12, dadurch gekennzeichnet, daß die Basisplatte (9; 13; 16) eine perforierte Metallplatte ist.
  14. Anlage nach einem der Ansprüche 4 - 9, dadurch gekennzeichnet, daß die Brennerplatte (18) eine gasdurchlässige Platte ist, die örtlich verdichtet ist.
  15. Anlage nach Anspruch 14, dadurch gekennzeichnet, daß die Brennerplatte örtlich durch Imprägnieren mit einem Füllmaterial oder durch teilweises Komprimieren der Platte verdichtet ist.
  16. Anlage nach Anspruch 14 oder 15, dadurch gekennzeichnet, daß die Brennerplatte (18) ein Schaumgefüge hat oder aus zwei Schaumgefügen mit unterschiedlichen Gasdurchlässigkeiten besteht.
  17. Anlage nach einem der Ansprüche 4 - 15, dadurch gekennzeichnet, daß die Bereiche (4; 20) in der Brennerplatte mit geringem Durchflußwiderstand aus Metallfasern oder Aluminiumoxidfasern bestehen.
EP92921500A 1991-10-03 1992-10-02 Verfahren und vorrichtung zur verbrennung eines gasgemisches Expired - Lifetime EP0605645B1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
NL9101668A NL9101668A (nl) 1991-10-03 1991-10-03 Branderplaat en brander voor een gasmengsel met een hoge luchtfactor.
NL9101668 1991-10-03
PCT/NL1992/000172 WO1993007420A1 (en) 1991-10-03 1992-10-02 Method and installation for the combustion of a gas mixture

Publications (2)

Publication Number Publication Date
EP0605645A1 EP0605645A1 (de) 1994-07-13
EP0605645B1 true EP0605645B1 (de) 1997-02-12

Family

ID=19859773

Family Applications (1)

Application Number Title Priority Date Filing Date
EP92921500A Expired - Lifetime EP0605645B1 (de) 1991-10-03 1992-10-02 Verfahren und vorrichtung zur verbrennung eines gasgemisches

Country Status (4)

Country Link
EP (1) EP0605645B1 (de)
DE (1) DE69217500T2 (de)
NL (1) NL9101668A (de)
WO (1) WO1993007420A1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4088064A1 (de) * 2020-01-08 2022-11-16 Bekaert Combustion Technology B.V. Gasbrenner und heizgerät

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL9400280A (nl) * 1994-02-23 1995-10-02 Stichting Energie Werkwijze voor de verbranding van hoogreaktieve gasvormige lucht/brandstof-mengsels en branderinrichting voor het uitvoeren van deze werkwijze.
JP3695201B2 (ja) * 1998-04-08 2005-09-14 リンナイ株式会社 燃焼用バーナプレート
GB2394275B (en) 2002-08-14 2005-09-21 Hamworthy Combustion Eng Ltd Burner and method of burning gas in a furnace
DE10251548A1 (de) * 2002-11-05 2004-05-19 Cramer Sr, S.R.O. Leistungsoptimierter Strahlungsbrenner
DE102014206372A1 (de) * 2014-04-03 2015-10-08 Vaillant Gmbh Kraft-Wärme-Kopplungssystem
NL2024623B1 (en) * 2020-01-08 2021-09-07 Bekaert Combustion Tech Bv Gas burner and heating appliance
DE102021103800B4 (de) * 2021-02-18 2024-10-17 Viessmann Climate Solutions Se Verfahren zum Betrieb eines Gasbrenners

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3371118D1 (en) 1982-04-28 1987-05-27 Ruhrgas Ag Gas-fired water heating apparatus
US4673349A (en) * 1984-12-20 1987-06-16 Ngk Insulators, Ltd. High temperature surface combustion burner
AU583674B2 (en) * 1985-10-25 1989-05-04 Rinnai Corporation Combustion heater
GB8620228D0 (en) * 1986-08-20 1986-10-01 Valor Heating Ltd Gas burner

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4088064A1 (de) * 2020-01-08 2022-11-16 Bekaert Combustion Technology B.V. Gasbrenner und heizgerät

Also Published As

Publication number Publication date
DE69217500D1 (de) 1997-03-27
EP0605645A1 (de) 1994-07-13
DE69217500T2 (de) 1997-05-28
NL9101668A (nl) 1993-05-03
WO1993007420A1 (en) 1993-04-15

Similar Documents

Publication Publication Date Title
EP0157432B1 (de) Brenner zur Strahlungsoberflächenverbrennung
US4608012A (en) Gas burner
EP0705409B1 (de) Brenner mit mehreren brenngeschwindigkeitszonen und verfahren dazu
US5848887A (en) Low emission combustion system
US4643667A (en) Non-catalytic porous-phase combustor
US7631640B2 (en) Radiant burner
US5511974A (en) Ceramic foam low emissions burner for natural gas-fired residential appliances
US4919609A (en) Ceramic tile burner
US4900245A (en) Infrared heater for fluid immersion apparatus
EP0681143A2 (de) Strahlungsbrenner mit niedrigem NOx-Ausstoss und hoher Intensität
US6129545A (en) Gas burner with pollution-reducing features
US5431557A (en) Low NOX gas combustion systems
US4318392A (en) Catalytic gas-fired furnace system and method
US4904179A (en) Low NOx primary zone radiant screen device
EP0605645B1 (de) Verfahren und vorrichtung zur verbrennung eines gasgemisches
CA1292650C (en) Advanced heater
US6435861B1 (en) Gas burner assembly and method of making
EP3170564B1 (de) Hochdruckreiniger mit infrarotbrenner
US20050069830A1 (en) Infrared radiator embodied as a surface radiator
US7537447B2 (en) Atmospheric gas burner made of biosoluble and gel-cast ceramic fibers
US3923447A (en) Burner of use with fluid fuels
US4412523A (en) Catalytic gas-fired furnace system and method
DE19545504A1 (de) Gasstrahlungsbrenner mit einer Brennerplatte aus Fasermaterial und reduzierter Geräuschentwicklung
RU2094703C1 (ru) Радиационная газовая горелка
JP3488634B2 (ja) 水素表面燃焼バーナ

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19940315

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE FR GB IT NL

17Q First examination report despatched

Effective date: 19951114

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB IT NL

ITF It: translation for a ep patent filed
ET Fr: translation filed
REF Corresponds to:

Ref document number: 69217500

Country of ref document: DE

Date of ref document: 19970327

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 19980922

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 19980925

Year of fee payment: 7

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 19991002

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 19991002

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20000630

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

NLT1 Nl: modifications of names registered in virtue of documents presented to the patent office pursuant to art. 16 a, paragraph 1

Owner name: NEFIT BUDERUS B.V.

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20051002

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20101022

Year of fee payment: 19

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 20111102

Year of fee payment: 20

REG Reference to a national code

Ref country code: DE

Ref legal event code: R071

Ref document number: 69217500

Country of ref document: DE

REG Reference to a national code

Ref country code: DE

Ref legal event code: R071

Ref document number: 69217500

Country of ref document: DE

REG Reference to a national code

Ref country code: NL

Ref legal event code: V4

Effective date: 20121002