DE4433184C1 - Combustion bar for atmospheric gas burner - Google Patents
Combustion bar for atmospheric gas burnerInfo
- Publication number
- DE4433184C1 DE4433184C1 DE19944433184 DE4433184A DE4433184C1 DE 4433184 C1 DE4433184 C1 DE 4433184C1 DE 19944433184 DE19944433184 DE 19944433184 DE 4433184 A DE4433184 A DE 4433184A DE 4433184 C1 DE4433184 C1 DE 4433184C1
- Authority
- DE
- Germany
- Prior art keywords
- coating
- fuel rod
- burner
- outlet openings
- atmospheric gas
- 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 - Fee Related
Links
- 238000002485 combustion reaction Methods 0.000 title abstract description 3
- 239000011248 coating agent Substances 0.000 claims abstract description 25
- 238000000576 coating method Methods 0.000 claims abstract description 25
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 5
- 239000004020 conductor Substances 0.000 claims abstract description 5
- 239000010959 steel Substances 0.000 claims abstract description 5
- 239000000919 ceramic Substances 0.000 claims abstract description 4
- 239000011148 porous material Substances 0.000 claims abstract description 4
- 239000000446 fuel Substances 0.000 claims description 20
- 239000000203 mixture Substances 0.000 claims description 12
- 239000007789 gas Substances 0.000 description 13
- 239000012876 carrier material Substances 0.000 description 3
- 238000013021 overheating Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
Classifications
-
- 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
- F23D14/02—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
- F23D14/04—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner
- F23D14/10—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner with elongated tubular burner head
- F23D14/105—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner with elongated tubular burner head with injector axis parallel to the burner head axis
-
- 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, e.g. noise reduction 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
- F23D14/46—Details, e.g. noise reduction means
- F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
- F23D14/76—Protecting flame and burner parts
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
Abstract
Description
Die Erfindung betrifft einen Brennstab für einen atmosphärischen Gasbrenner nach dem Oberbegriff des Anspruches 1.The invention relates to a fuel rod for an atmospheric gas burner according to the preamble of claim 1.
Ein derartiger Brennstab für einen atmosphärischen Gasbrenner ist bekannt aus der DE 41 18 861 A1. Bei diesem Brenner mit einem oder mehreren nebeneinan der angeordneten Brennstäben besitzt jeder Brennstab ein Mischrohr, das von einem Gasstrahl aus einer Gasdüse angeströmt wird. Dabei wird Verbrennungs luft mittels Hilfsgebläse angesaugt und im Brennstab mit dem Gas gemischt. An der gelochten Oberfläche des Brennstabmantels aus Stahlblech tritt das Gemisch aus und verbrennt.Such a fuel rod for an atmospheric gas burner is known from DE 41 18 861 A1. With this burner with one or more next to each other of the arranged fuel rods, each fuel rod has a mixing tube which a gas jet flows from a gas nozzle. This will burn air is drawn in by means of an auxiliary fan and mixed with the gas in the fuel rod. At The mixture enters the perforated surface of the steel sheet fuel rod jacket out and burns.
Die Flammenform ist unter anderem von der Lochgeometrie der Ge mischaustrittsöffnungen, dem Gasdruck sowie der Luftmenge abhängig. Günstig ist es, wenn die Flamme in einem gewissen Abstand von der Brenneroberfläche brennt, da diese nur begrenzt thermisch belastbar ist. Durch Ungeregelmäßig keiten im Betrieb oder durch Gasqualitätsschwankungen kann es vorkommen, daß die Flamme am Brennstab aufsitzt und Überhitzungsschäden eintreten. The flame shape is, among other things, from the hole geometry of the Ge mixing outlet openings, the gas pressure and the amount of air. Cheap it is when the flame is some distance from the burner surface burns because it can only withstand thermal loads to a limited extent. By irregular in operation or due to fluctuations in gas quality, that the flame sits on the fuel rod and damage caused by overheating occurs.
Weiterhin ist ein von einem Brenngas-Luft-Gemisch durchströmter rohrförmiger Brenner bekannt, dessen Mantel außenseitig mehrere Schichten porösen Materials aufweisen kann (DE-OS 22 11 297). Hierdurch wird einem Flammen rückschlag vorgebeugt und ein Kühleffekt erreicht. Das poröse Material bildet dabei die Brenneroberfläche mit einer großen Anzahl feinster Gemischaustritts öffnungen. Es handelt sich nicht um einen Gasbrenner aus Stahlblech mit einer gelochten Oberfläche, bei dem durch Unregelmäßigkeiten im Betrieb oder durch Gasqualitätsschwankungen Überhitzungsschäden am Mantel aus Stahlblech auftreten können.Furthermore, a tubular gas flows through a mixture of fuel gas and air Burner known, the outer surface of which has several layers of porous May have materials (DE-OS 22 11 297). This will make a flame setback prevented and a cooling effect achieved. The porous material forms the burner surface with a large number of the finest mixture outlet openings. It is not a gas burner made of sheet steel with a perforated surface, due to irregularities in operation or through Fluctuations in gas quality Overheating damage to the sheet steel jacket may occur.
Der Erfindung liegt die Aufgabe zugrunde, einen gattungsgemäßen Brennstab zu schaffen, bei dem Überhitzungsschäden vermieden werden.The invention has for its object a generic fuel rod to create, in which overheating damage is avoided.
Der erfindungsgemäße Brennstab besitzt die im Patentanspruch 1 genannten Merkmale.The fuel rod according to the invention has those mentioned in claim 1 Features.
Die auf dem rohrförmigen Brennstabmantel angebrachte Beschichtung, z. B. auf keramischer Basis, kann einerseits aus einem schlecht wärmeleitenden Material zur Abschirmung bestehen. Andererseits kann das Material auch gut wärmelei tend und mit Lufteinschlüssen versehen sein, welche unterhalb der Beschich tung den Wärmeübergang in das Trägermaterial vermindern und das Abführen der Wärme innerhalb der Beschichtung in kältere Bereiche begünstigen. The coating applied to the tubular fuel rod jacket, e.g. B. on ceramic base, can be made of a poorly heat-conducting material exist for shielding. On the other hand, the material can also heat well tend and be provided with air pockets, which underneath the coating tion reduce the heat transfer into the carrier material and the dissipation favor the heat within the coating in colder areas.
Bei den Ausführungsformen nach den Unteransprüchen 2 und 3 besteht die Möglichkeit, daß sich die Lochung der Gemischaustrittsöffnungen durchgehend durch die Beschichtung fortsetzt oder daß die Beschichtung aus einem porösen Material besteht und die Gemischaustrittsöffnungen im Trägermaterial über deckt. Durch die Überdeckung ändert sich das Flammenbild gegenüber durchge hender Lochung und es wird ein Rückschlagen der Flamme in den Brennstab verhindert. Mit der Körnung sowie dem Aufbau der Beschichtung läßt sich das Flammenbild beeinflussen. Im Bereich der Beschichtung wird der Brennstab vor Korrosion geschützt.In the embodiments according to subclaims 2 and 3 there is Possibility that the holes in the mixture outlet openings are continuous continues through the coating or that the coating consists of a porous Material exists and the mixture outlet openings in the carrier material over covers. Due to the overlap, the flame pattern changes throughout holes and there will be a backlash of the flame in the fuel rod prevented. This can be done with the grain and the structure of the coating Influence flame pattern. The fuel rod is in front of the coating Corrosion protected.
Die Zeichnung stellt ein Ausführungsbeispiel der Erfindung dar. Es zeigtThe drawing shows an embodiment of the invention. It shows
Fig. 1 einen Längsschnitt durch einen Brennstab, Fig. 1 shows a longitudinal section through a fuel rod,
Fig. 2 einen vergrößerten Längsschnitt durch die Brenneroberfläche mit einer schlecht wärmeleitenden Beschichtung und Fig. 2 is an enlarged longitudinal section through the burner surface with a poorly heat-conducting coating and
Fig. 3 einen vergrößerten Längsschnitt durch die Brenneroberfläche mit einer gut wärmeleitenden Beschichtung mit Lufteinschlüssen. Fig. 3 is an enlarged longitudinal section through the burner surface with a good heat-conducting coating with air pockets.
Der Brennstab in Fig. 1 besitzt ein Venturirohr 2, das von einem Gasstrahl aus einer Gasdüse 3 angeströmt wird. Dabei wird Verbrennungsluft angesaugt und im Brennstab mit dem Gas gemischt. An der gelochten Oberfläche des Mantels 1 tritt das Gemisch aus und verbrennt. The fuel rod in Fig. 1 has a Venturi tube 2 , which is blown by a gas jet from a gas nozzle 3 . Combustion air is drawn in and mixed with the gas in the fuel rod. The mixture emerges from the perforated surface of the casing 1 and burns.
Fig. 2 zeigt einen Brennstab mit einer schlecht wärmeleitenden Beschichtung 4, z. B. auf keramischer Basis, auf dem Mantel 1. Die als Bohrungen ausgebildeten Gemischaustrittsöffnungen 5 können von der Beschichtung 4 überdeckt sein oder in der Beschichtung 4 korrespondierende Bohrungen 6 besitzen. Fig. 2 shows a fuel rod with a poorly heat-conducting coating 4 , for. B. on a ceramic basis, on the jacket 1 . The mixture outlet openings 5 designed as bores can be covered by the coating 4 or have corresponding bores 6 in the coating 4 .
Ein Brennstab mit einer gut wärmeleitenden Beschichtung 7, z. B. auf kerami scher Basis, auf dem Mantel 1 ist in Fig. 3 dargestellt. An der Unterseite der Be schichtung 7 sind Lufteinschlüsse 8 angeordnet, die den Wärmeübergang in das Trägermaterial vermindern und das Abführen der Wärme innerhalb der Be schichtung 7 in kältere Bereiche begünstigen. Die Gemischaustrittsöffnungen 5 können von der Beschichtung 7 überdeckt sein oder in der Beschichtung 7 korrespondierende Bohrungen 6 besitzen.A fuel rod with a good heat-conducting coating 7 , for. B. based on kerami shear, on the jacket 1 is shown in Fig. 3. At the bottom of the loading coating 7 , air pockets 8 are arranged, which reduce the heat transfer into the carrier material and favor the dissipation of the heat within the loading coating 7 into colder areas. The mixture outlet openings 5 can be covered by the coating 7 or have corresponding holes 6 in the coating 7 .
Claims (3)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19944433184 DE4433184C1 (en) | 1994-09-17 | 1994-09-17 | Combustion bar for atmospheric gas burner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19944433184 DE4433184C1 (en) | 1994-09-17 | 1994-09-17 | Combustion bar for atmospheric gas burner |
Publications (1)
Publication Number | Publication Date |
---|---|
DE4433184C1 true DE4433184C1 (en) | 1996-03-07 |
Family
ID=6528490
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19944433184 Expired - Fee Related DE4433184C1 (en) | 1994-09-17 | 1994-09-17 | Combustion bar for atmospheric gas burner |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE4433184C1 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0795721A2 (en) * | 1996-03-16 | 1997-09-17 | Furigas Assen B.V. | Burner for gas fired heating device |
EP0809071A1 (en) * | 1995-05-05 | 1997-11-26 | Burner Systems International, Inc. | Premixed gas burner |
WO1998049495A1 (en) * | 1997-04-28 | 1998-11-05 | Worgas Bruciatori S.R.L. | Burner for gaseous fuels |
WO2001057438A1 (en) * | 2000-02-02 | 2001-08-09 | Worgas Bruciatori S.R.L. | Burner provided with means against the overheating of the burner head |
FR2835042A1 (en) * | 2002-01-22 | 2003-07-25 | Mer Joseph Le | GAS BURNER, FACING BIPARTITE COMBUSTION AND BOILER EQUIPPED WITH SUCH A BURNER |
GB2606769A (en) * | 2021-05-20 | 2022-11-23 | Beckett Thermal Solutions Ltd | Gas burner membrane |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3275497A (en) * | 1962-01-17 | 1966-09-27 | American Thermocatalytic Corp | Method of molding a combustion element of ceramic fibers on a porous support |
US3383159A (en) * | 1966-02-03 | 1968-05-14 | American Thermocatalytic Corp | Combustion elements |
DE2211297A1 (en) * | 1971-04-26 | 1972-11-16 | CA. Sundberg AB, Kallhäll (Schweden) | Gaseous fuel burners |
US4746287A (en) * | 1986-01-17 | 1988-05-24 | Gas Research Institute | Fiber matrix burner composition with aluminum alloys and method of formulation |
DE4118861A1 (en) * | 1991-06-07 | 1992-12-10 | Buderus Heiztechnik Gmbh | Premixing gas burner - has axial or radial flow fan housed inside burner bar with end inlet |
US5326631A (en) * | 1993-06-07 | 1994-07-05 | Alzeta Corporation | Unsintered fiber burner made with metal fibers, ceramic fibers and binding agent |
-
1994
- 1994-09-17 DE DE19944433184 patent/DE4433184C1/en not_active Expired - Fee Related
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3275497A (en) * | 1962-01-17 | 1966-09-27 | American Thermocatalytic Corp | Method of molding a combustion element of ceramic fibers on a porous support |
US3383159A (en) * | 1966-02-03 | 1968-05-14 | American Thermocatalytic Corp | Combustion elements |
DE2211297A1 (en) * | 1971-04-26 | 1972-11-16 | CA. Sundberg AB, Kallhäll (Schweden) | Gaseous fuel burners |
US4746287A (en) * | 1986-01-17 | 1988-05-24 | Gas Research Institute | Fiber matrix burner composition with aluminum alloys and method of formulation |
DE4118861A1 (en) * | 1991-06-07 | 1992-12-10 | Buderus Heiztechnik Gmbh | Premixing gas burner - has axial or radial flow fan housed inside burner bar with end inlet |
US5326631A (en) * | 1993-06-07 | 1994-07-05 | Alzeta Corporation | Unsintered fiber burner made with metal fibers, ceramic fibers and binding agent |
DE4417645A1 (en) * | 1993-06-07 | 1994-12-08 | Alzeta Corp | fiber burner |
Non-Patent Citations (1)
Title |
---|
Dreizler, U. u.a.: High-Tech Gasgebläsebrenner mitMagma-Infrarotverbrennung, in: Heizungs-Journal Heft 1, Febr./März 1993 * |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0809071A1 (en) * | 1995-05-05 | 1997-11-26 | Burner Systems International, Inc. | Premixed gas burner |
EP0795721A2 (en) * | 1996-03-16 | 1997-09-17 | Furigas Assen B.V. | Burner for gas fired heating device |
EP0795721A3 (en) * | 1996-03-16 | 1998-10-28 | Furigas Assen B.V. | Burner for gas fired heating device |
WO1998049495A1 (en) * | 1997-04-28 | 1998-11-05 | Worgas Bruciatori S.R.L. | Burner for gaseous fuels |
WO2001057438A1 (en) * | 2000-02-02 | 2001-08-09 | Worgas Bruciatori S.R.L. | Burner provided with means against the overheating of the burner head |
FR2835042A1 (en) * | 2002-01-22 | 2003-07-25 | Mer Joseph Le | GAS BURNER, FACING BIPARTITE COMBUSTION AND BOILER EQUIPPED WITH SUCH A BURNER |
WO2003062705A1 (en) * | 2002-01-22 | 2003-07-31 | Societe D'etude Et De Realisation Mecaniques Engeneering En Technologies Avancees | Gas burner comprising a two-part combustion surface and a boiler equipped with one such burner |
GB2606769A (en) * | 2021-05-20 | 2022-11-23 | Beckett Thermal Solutions Ltd | Gas burner membrane |
EP4092322A1 (en) * | 2021-05-20 | 2022-11-23 | Beckett Thermal Solutions Ltd. | Gas burner membrane |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8100 | Publication of the examined application without publication of unexamined application | ||
D1 | Grant (no unexamined application published) patent law 81 | ||
8363 | Opposition against the patent | ||
8368 | Opposition refused due to inadmissibility | ||
8339 | Ceased/non-payment of the annual fee |