EP2510281B1 - Burner with low porosity burner deck - Google Patents
Burner with low porosity burner deck Download PDFInfo
- Publication number
- EP2510281B1 EP2510281B1 EP10782307.2A EP10782307A EP2510281B1 EP 2510281 B1 EP2510281 B1 EP 2510281B1 EP 10782307 A EP10782307 A EP 10782307A EP 2510281 B1 EP2510281 B1 EP 2510281B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- burner
- deck
- gas
- porosity
- metal 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.)
- Active
Links
- 239000002184 metal Substances 0.000 claims description 26
- 239000007789 gas Substances 0.000 description 29
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 6
- 230000003247 decreasing effect Effects 0.000 description 5
- 239000011295 pitch Substances 0.000 description 4
- POIUWJQBRNEFGX-XAMSXPGMSA-N cathelicidin Chemical compound C([C@@H](C(=O)N[C@@H](CCCNC(N)=N)C(=O)N[C@@H](CCCCN)C(=O)N[C@@H](CO)C(=O)N[C@@H](CCCCN)C(=O)N[C@@H](CCC(O)=O)C(=O)N[C@@H](CCCCN)C(=O)N[C@@H]([C@@H](C)CC)C(=O)NCC(=O)N[C@@H](CCCCN)C(=O)N[C@@H](CCC(O)=O)C(=O)N[C@@H](CC=1C=CC=CC=1)C(=O)N[C@@H](CCCCN)C(=O)N[C@@H](CCCNC(N)=N)C(=O)N[C@@H]([C@@H](C)CC)C(=O)N[C@@H](C(C)C)C(=O)N[C@@H](CCC(N)=O)C(=O)N[C@@H](CCCNC(N)=N)C(=O)N[C@@H]([C@@H](C)CC)C(=O)N[C@@H](CCCCN)C(=O)N[C@@H](CC(O)=O)C(=O)N[C@@H](CC=1C=CC=CC=1)C(=O)N[C@@H](CC(C)C)C(=O)N[C@@H](CCCNC(N)=N)C(=O)N[C@@H](CC(N)=O)C(=O)N[C@@H](CC(C)C)C(=O)N[C@@H](C(C)C)C(=O)N1[C@@H](CCC1)C(=O)N[C@@H](CCCNC(N)=N)C(=O)N[C@@H]([C@@H](C)O)C(=O)N[C@@H](CCC(O)=O)C(=O)N[C@@H](CO)C(O)=O)NC(=O)[C@H](CC=1C=CC=CC=1)NC(=O)[C@H](CC(O)=O)NC(=O)CNC(=O)[C@H](CC(C)C)NC(=O)[C@@H](N)CC(C)C)C1=CC=CC=C1 POIUWJQBRNEFGX-XAMSXPGMSA-N 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 description 2
- QQONPFPTGQHPMA-UHFFFAOYSA-N Propene Chemical compound CC=C QQONPFPTGQHPMA-UHFFFAOYSA-N 0.000 description 2
- 238000012217 deletion Methods 0.000 description 2
- 230000037430 deletion Effects 0.000 description 2
- 239000002737 fuel gas Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000003345 natural gas Substances 0.000 description 2
- VXNZUUAINFGPBY-UHFFFAOYSA-N 1-Butene Chemical compound CCC=C VXNZUUAINFGPBY-UHFFFAOYSA-N 0.000 description 1
- OTMSDBZUPAUEDD-UHFFFAOYSA-N Ethane Chemical compound CC OTMSDBZUPAUEDD-UHFFFAOYSA-N 0.000 description 1
- VGGSQFUCUMXWEO-UHFFFAOYSA-N Ethene Chemical compound C=C VGGSQFUCUMXWEO-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 description 1
- 239000001273 butane Substances 0.000 description 1
- IAQRGUVFOMOMEM-UHFFFAOYSA-N butene Natural products CC=CC IAQRGUVFOMOMEM-UHFFFAOYSA-N 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- IJDNQMDRQITEOD-UHFFFAOYSA-N n-butane Chemical compound CCCC IJDNQMDRQITEOD-UHFFFAOYSA-N 0.000 description 1
- OFBQJSOFQDEBGM-UHFFFAOYSA-N n-pentane Natural products CCCCC OFBQJSOFQDEBGM-UHFFFAOYSA-N 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 239000001294 propane Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
Images
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
- F23D14/02—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
-
- 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
- F23D14/26—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid with provision for a retention flame
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2203/00—Gaseous fuel burners
- F23D2203/10—Flame diffusing means
- F23D2203/101—Flame diffusing means characterised by surface shape
- F23D2203/1012—Flame diffusing means characterised by surface shape tubular
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2203/00—Gaseous fuel burners
- F23D2203/10—Flame diffusing means
- F23D2203/102—Flame diffusing means using perforated plates
- F23D2203/1023—Flame diffusing means using perforated plates with specific free passage areas
Definitions
- the present invention relates to a premix burner, more in particular a burner having a flameholder made of perforated metal plate material.
- the burner is a tubular burner having a cylindrical shape. These burners are especially suitable for use in combustion boilers.
- premix burner consist of one or more of the following components: a) an end cap located at the top of the burner, b) a burner deck, the burner deck consists of a blind piece at the bottom, a perforated piece, with a regular (circular) pattern, with sometimes locally an additional modification for ignition purposes, in the centre part and a blind piece at the top.
- the pattern is mostly circumferential, and mostly repeating itself in height after a pitch of 1-10 mm; c) a distributor, having a blind piece at the bottom, a perforated part in the centre and a blind piece at the top; d) a distributor end cap; e) a flange; f) an anti noise tube which is a device located in or nearby the flange to adjust the pressure distribution.
- a distributor having a blind piece at the bottom, a perforated part in the centre and a blind piece at the top
- d) a distributor end cap e) a flange; f) an anti noise tube which is a device located in or nearby the flange to adjust the pressure distribution.
- Such premix burners are described in e.g. EP 1337789 , EP2037175 , WO2009/077333 , WO2009/065733 , WO2009/059933 .
- these burners are provided with devices in the mixing chamber, such as e.g
- an inner liner also called distributor and/or anti-noise tube or other devices such as swirls or perforated disks in or nearby the flange.
- distributor and/or anti-noise tube or other devices such as swirls or perforated disks in or nearby the flange.
- the object of the present invention is to obviate the drawbacks mentioned above.
- An object of the present invention is to provide a premix burner which does not need such devices in the mixing chamber of the burner to obtain a good stability of the flames and to reduce or even eliminate noise problems.
- a further object of the present invention is to provide a premix burner with a good stability over the full operating range of high to low CO 2 , and for the full band of customary or natural gas qualities.
- This full band of customary and natural gas qualities covers all gases selected from hydrocarbons such as methane, ethane, propane, butane, ethene, propene, butene, acetylene, and the like.
- hydrocarbons such as methane, ethane, propane, butane, ethene, propene, butene, acetylene, and the like.
- the present invention does not relate specifically to high reactive fuel gases, which are a mixture of hydrogen and customary fuel gases.
- a further object of the present invention is to provide a premix burner producing low NOx levels.
- An aspect of the claimed invention provides a gas burner as described in claim 1.
- the present invention provides a gas burner as described above wherein the burner further comprises an end cap connected to the perforated metal plate substantially opposite to said gas inlet port.
- the present invention provides a gas burner as described in paragraph 8, wherein the end cap is also provided with perforations. These perforations thereby enlarge and are part of the burner deck.
- the end cap is made of metal plate material.
- the perforation patterns in the end cap and in the perforated metal plate are equal.
- the perforation patterns in the end cap and in the perforated metal plate are different.
- the perforations, such as e.g. slots and holes, in the end cap and in the perforated metal plate are equal.
- the perforations in the end cap and in the perforated metal plate are different.
- the burner of claim 1 has a burner deck wherein more than 50% of the burner deck has a porosity being equal to or lower than 9% and wherein upto 50% of the burner deck has a porosity being higher than 11 % and with an overall porosity which is equal to or lower than 11 %.
- This modification of the perforation pattern of the burner deck provided a burner which, next to the effect of the deletion of the diffuser and the removal of the humming noise, also had a more stable response on the second and higher Helmholtz or instable acoustic resonances of the heat exchanger, which therefore made that the boiler, with this build in burner did not provoke a whistling sound anymore.
- Another aspect of the claimed invention provides a gas burner as described in [0007], [0008], [0009] or [0011] wherein the burner deck has different patterns of perforations. Adding more patterns with different pitches showed an increased stability for a broader range of gas qualities and induced less NOx-emissions.
- the burner is provided with an abrupt and stepwise variation of the perforation pattern in the burner deck.
- the present invention provides a burner with gradually increasing or decreasing perforation pattern or gradually increasing or decreasing pitches in between the perforation pattern of the burner deck.
- This grading can go in axial or circumferential direction.
- Gradually increasing or decreasing the perforation of the decks allows an almost step less variety of the perforation, and thus creating a varying perforation of the surface of the deck.
- the burner has a completely random deck with no repeatability over the full height or circumference of the burner deck which provides a stabilized deck without the additional devices as mentioned above.
- the part with a porosity higher than 11 % is closest to the gas inlet.
- the part with a porosity equal to or lower than 9% is most remote, i.e. downstream, from the gas inlet.
- burner deck is to be understood, in the light of this invention, to be that part of the burner where the totality of perforations are present. In case two or more distinct regions of perforations can be detected on the burner surface, the burner deck is defined as being the surface spanning of all regions with perforations.
- all porosity of the burner deck is to be understood, in the light of this invention, as ratio of the surface of the holes, slots or other openings divided by the surface of the burner over which the perforated part(s) is(are) located.
- perforation pattern is to be understood, in the light of this invention, to be a recurring scheme of perforations.
- FIG. 1 shows a gas burner 10, preferably a premix burner, comprising a support or flange 12 which has a central gas inlet port 14 for supply of gas into a gas supply or mixing chamber 16.
- the gas supply chamber 16 is enclosed by a perforated metal plate 22.
- the perforated metal plate 22 is connected at the bottom to the support or flange 12 through a base section.
- the perforations 24 in the perforated metal plate 22 provide the burner deck 20.
- the burner deck 20 has an overall porosity which is equal to or lower than 11 %, preferably lower than 10%, even more preferably lower than 9%.
- Figure 2A shows a perspective view of a burner.
- Figure 2B shows a cross sectional view taken along the line II-II' in Figure 2A.
- Figures 2A and 2B shows a gas burner 10, preferably a premix burner, comprising a support or flange 12 which has a central gas inlet port 14 for supply of gas into a gas supply or mixing chamber 16.
- the gas supply chamber 16 is enclosed by a perforated metal plate 22 and an end cap 18 substantially opposite to said gas inlet port 14.
- the perforations 24 in the perforated metal plate 22 provide the burner deck 20.
- the end cap 18 is connected to the top of the perforated metal plate 22 and the perforated metal plate 22 is connected at the bottom to the support or flange 18 through a base section.
- the burner deck 20 has an overall porosity which is equal to or lower than 11%, preferably lower than 10%, even more preferably lower than 9%.
- a burner 10 with a perforation pattern as shown in figure 2C has a length of 102,4mm and diameter of 70,4mm.
- the burner deck has a length of 81,2 mm and has a porosity of 7,7%.
- the perforation pattern in the perforated plate is a combination of slits and round holes. For a thickness of the perforated plate of 0,6 mm, the slits being 4,0x0,5mm, the holes having a diameter of 0,8mm.
- the perforations are grouped in a pattern of 4,8 mm and this pattern is repeated over the burner deck in an equal division. As explained above, this burner still needed an anti-noise device, but no pressure divider or distributor anymore.
- An aspect of the present invention provides a burner 10 wherein the end cap 18 is also provided with perforations.
- Figure 3 shows an exemplary burner wherein the end cap is provided with perforations 30.
- the burner deck of this burner is as shown by reference number 20.
- the present invention provides a burner 10 with a burner deck wherein more than 50% of the burner deck has a porosity being equal to or lower than 9% and wherein 10 to 50% of the burner deck has a porosity being higher than 11 %.
- the burner deck has an overall porosity which is equal to or lower than 11%.
- a burner 10 as shown in figure 4 has a length of 94,8mm and diameter of 70,4mm.
- the burner deck 20 has a length of 93,6mm.
- the perforation pattern in the perforated plate 22 is a combination of slits and round holes.
- the thickness of the perforated plate 22 is 0,6 mm, the slits being 4,0x0,5mm, the holes having a diameter of 0,8mm.
- the perforations are grouped in a pattern as shown in fig. 4 , wherein the first 11,8mm of the burner deck length has a porosity of 15%, thereafter is a zone of 46,8mm of the burner deck length with a porosity of 7,3% and the last zone with a length of 5.8mm of the burner deck length having a porosity of 16,5%.
- This pattern is repeated over the burner deck on the circumference of the burner. This provides a burner deck which has an overall porosity of 9,8%.
- This modification of the perforation pattern of the burner deck provided a burner which, next to the effect of the deletion of the diffuser and the removal of the humming noise, also had a more stable response on the second and higher Helmholtz or instable acoustic resonances of the heat exchanger, which therefore made that the burner did not provoke a whistling sound anymore.
- the humming sound was eliminated and therefore the use of anti-noise devices in the mixing chamber of the burner could be omitted.
- the use of the relatively high porosity at the beginning and end of the burner deck 20 provide an even more stable flame pattern of the burner.
- An example embodiment according to a further aspect of the claimed invention provides a gas burner with a perforated metal plate 22 with a perforation pattern as shown in fig. 5 .
- the shown perforation pattern is repeated over the circumference of the burner.
- the burner deck 20 has different patterns of perforations. Adding more patterns with different pitches showed an increased stability for a broader range of gas qualities and induced less NOx-emissions.
- the exemplary perforation pattern of fig. 5 is an abrupt and stepwise variation of the perforation pattern in the burner deck 20.
- Figure 6 shows another example of a perforation pattern of burner deck 20 according to a preferred aspect of the present invention, wherein the porosity of the burner deck 20 decreases stepwise in downstream direction.
- the shown perforation pattern is repeated in the perforated metal plate 22 over the circumference of the burner.
- Figure 7 shows an example of a perforation pattern of burner deck 20 according to a preferred aspect of the present invention, wherein the porosity is gradually increasing. This perforation pattern is repeated in the perforated metal plate 22 over the circumference of the burner.
- Figure 8 shows an exemplary perforation pattern of the burner deck 20, which is repeated lengthwise over the perforated metal plate 22.
- Figure 9 shows a further exemplary perforation pattern which is repeated on the circumference of a burner.
- the perforation pattern is such that no repeat of pattern is occurring along the length of the burner deck 20.
- An exemplary burner with a length of 91,2mm and diameter of 70,4mm.
- the burner deck has a length of 70,4mm.
- the perforation pattern in the perforated plate 22 is a combination of slits and round holes as shown in figure 9 .
- this burner deck has an overall porosity of 7.5%.
- any perforation pattern or set of perforation patterns can be repeated lengthwise or over the circumference to obtain the burner according to the present invention.
- FIG. 10 Another preferred embodiment of the present invention is shown in figure 10 .
- the burner 10 made out of perforated metal plate 22 has a completely random perforated burner deck 20 with no repeatability over the full height or circumference of the burner deck which provides a stabilized deck without the additional devices as mentioned above.
- FIG 11 shows another exemplary embodiment of the present invention.
- This burner has a perforated end cap 24 with different perforation pattern than the perforated metal plate 22.
- the perforations 30 together with the perforations 24 provide the burner deck 20.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
Description
- The present invention relates to a premix burner, more in particular a burner having a flameholder made of perforated metal plate material. Preferably, the burner is a tubular burner having a cylindrical shape. These burners are especially suitable for use in combustion boilers.
- One known type of premix burner consist of one or more of the following components: a) an end cap located at the top of the burner, b) a burner deck, the burner deck consists of a blind piece at the bottom, a perforated piece, with a regular (circular) pattern, with sometimes locally an additional modification for ignition purposes, in the centre part and a blind piece at the top. The pattern is mostly circumferential, and mostly repeating itself in height after a pitch of 1-10 mm; c) a distributor, having a blind piece at the bottom, a perforated part in the centre and a blind piece at the top; d) a distributor end cap; e) a flange; f) an anti noise tube which is a device located in or nearby the flange to adjust the pressure distribution. Such premix burners are described in e.g.
EP 1337789 ,EP2037175 ,WO2009/077333 ,WO2009/065733 ,WO2009/059933 . As can be seen in most of above referenced documents, these burners are provided with devices in the mixing chamber, such as e.g. an inner liner, also called distributor and/or anti-noise tube or other devices such as swirls or perforated disks in or nearby the flange. These devices are needed for stabilization of flames on these burners, which has an effect on noise and emissions. The need of using these devices implies a considerable complication for making the burner and for the assemblage and implies a considerable cost. - The object of the present invention is to obviate the drawbacks mentioned above.
- An object of the present invention is to provide a premix burner which does not need such devices in the mixing chamber of the burner to obtain a good stability of the flames and to reduce or even eliminate noise problems.
- A further object of the present invention is to provide a premix burner with a good stability over the full operating range of high to low CO2, and for the full band of customary or natural gas qualities.
- This full band of customary and natural gas qualities covers all gases selected from hydrocarbons such as methane, ethane, propane, butane, ethene, propene, butene, acetylene, and the like. In contrast with
WO 95/23315 - A further object of the present invention is to provide a premix burner producing low NOx levels.
- An aspect of the claimed invention provides a gas burner as described in claim 1.
- In a further aspect, the present invention provides a gas burner as described above wherein the burner further comprises an end cap connected to the perforated metal plate substantially opposite to said gas inlet port.
- In a preferred aspect, the present invention provides a gas burner as described in paragraph 8, wherein the end cap is also provided with perforations. These perforations thereby enlarge and are part of the burner deck. In a preferred aspect, the end cap is made of metal plate material. In a further preferred aspect, the perforation patterns in the end cap and in the perforated metal plate are equal. In an alternative further aspect, the perforation patterns in the end cap and in the perforated metal plate are different. In a further preferred aspect, the perforations, such as e.g. slots and holes, in the end cap and in the perforated metal plate are equal. In an alternative further aspect, the perforations in the end cap and in the perforated metal plate are different.
- Conventional premix burners have a porosity in the range of 14 to 18%. It was surprisingly found that lowering the porosity of the burner deck decreased acoustic time-lag of the flames formed on the burner deck, which enabled us to make a burner which did not need a diffuser anymore. It was also surprisingly found that this burner had an unstable burning when this burner was operated in open air, but when applied inside a heat exchanger, this burner had a stable flame and burning pattern. This burner also had a more stable response on the first Helmholtz resonance of the heat exchanger and its peripheral parts, which therefore made that the burner did not provoke low frequency thermo-acoustic instabilities, often referred to as humming. However, during start sequences under cold conditions with this burner build in, the boiler sometimes suffered a humming sound which sometimes makes the burner still needing an anti-noise device in its mixing chamber. The use of the anti-noise device in this burner also has a positive effect on the CO emission. Also it was found that lowering the porosity did not dampen thermo-acoustic instabilities with a higher frequency than the first Helmholtz resonance of the boiler, often referred to as whistling or howling. To cancel these frequencies, the anti-noise device was necessary again.
- The burner of claim 1 has a burner deck wherein more than 50% of the burner deck has a porosity being equal to or lower than 9% and wherein upto 50% of the burner deck has a porosity being higher than 11 % and with an overall porosity which is equal to or lower than 11 %. This modification of the perforation pattern of the burner deck provided a burner which, next to the effect of the deletion of the diffuser and the removal of the humming noise, also had a more stable response on the second and higher Helmholtz or instable acoustic resonances of the heat exchanger, which therefore made that the boiler, with this build in burner did not provoke a whistling sound anymore. Next to that, during start sequences under cold conditions, the humming sound was eliminated and therefore the use of anti-noise devices in the mixing chamber of the burner could be omitted. Furthermore, this provided a stabilized deck over the full operating range of high to low CO2, and for a broad range of gas qualities.
- Another aspect of the claimed invention provides a gas burner as described in [0007], [0008], [0009] or [0011] wherein the burner deck has different patterns of perforations. Adding more patterns with different pitches showed an increased stability for a broader range of gas qualities and induced less NOx-emissions. In a preferred aspect, the burner is provided with an abrupt and stepwise variation of the perforation pattern in the burner deck.
- In a preferred aspect, the present invention provides a burner with gradually increasing or decreasing perforation pattern or gradually increasing or decreasing pitches in between the perforation pattern of the burner deck. This grading can go in axial or circumferential direction. Gradually increasing or decreasing the perforation of the decks allows an almost step less variety of the perforation, and thus creating a varying perforation of the surface of the deck. In another preferred embodiment of the present invention, the burner has a completely random deck with no repeatability over the full height or circumference of the burner deck which provides a stabilized deck without the additional devices as mentioned above.
- Most preferably, in order to improve flame stability, there is a decreased porosity when going downstream. In an embodiment, the part with a porosity higher than 11 % is closest to the gas inlet. The part with a porosity equal to or lower than 9% is most remote, i.e. downstream, from the gas inlet.
- The term "burner deck" is to be understood, in the light of this invention, to be that part of the burner where the totality of perforations are present. In case two or more distinct regions of perforations can be detected on the burner surface, the burner deck is defined as being the surface spanning of all regions with perforations.
- The term "overall porosity of the burner deck" is to be understood, in the light of this invention, as ratio of the surface of the holes, slots or other openings divided by the surface of the burner over which the perforated part(s) is(are) located.
- The term "perforation pattern" is to be understood, in the light of this invention, to be a recurring scheme of perforations.
-
-
Figure 1 shows an example of a gas burner. -
Figures 2A and 2B show an example of a gas burner.Figure 2C shows an example perforation pattern according to an aspect of the present invention. -
Figure 3 shows an example embodiment according to an aspect of the present invention. -
Figure 4 shows an example embodiment according to the present invention. -
Figure 5 shows an example embodiment according to a further aspect of the present invention. -
Figure 6 shows an example embodiment according to a further aspect of the present invention. -
Figure 7 shows an example embodiment according to a further aspect of the present invention. -
Figure 8 shows an example embodiment according to a further aspect of the present invention. -
Figure 9 shows an example embodiment according to a further aspect of the present invention. -
Figure 10 shows a further example embodiment according to an aspect of the present invention. -
Figure 11 shows a further example embodiment according to an aspect of the present invention. -
- 10
- gas burner
- 12
- support or flange
- 14
- central gas inlet port
- 16
- gas supply or mixing chamber
- 18
- end cap
- 20
- burner deck
- 22
- perforated metal plate
- 24
- perforation
- 30
- perforation
-
Figure 1 shows agas burner 10, preferably a premix burner, comprising a support orflange 12 which has a centralgas inlet port 14 for supply of gas into a gas supply or mixingchamber 16. Thegas supply chamber 16 is enclosed by aperforated metal plate 22. Theperforated metal plate 22 is connected at the bottom to the support orflange 12 through a base section. Theperforations 24 in theperforated metal plate 22 provide theburner deck 20. Theburner deck 20 has an overall porosity which is equal to or lower than 11 %, preferably lower than 10%, even more preferably lower than 9%. -
Figure 2A shows a perspective view of a burner.Figure 2B shows a cross sectional view taken along the line II-II' inFigure 2A. Figures 2A and 2B shows agas burner 10, preferably a premix burner, comprising a support orflange 12 which has a centralgas inlet port 14 for supply of gas into a gas supply or mixingchamber 16. Thegas supply chamber 16 is enclosed by aperforated metal plate 22 and anend cap 18 substantially opposite to saidgas inlet port 14. Theperforations 24 in theperforated metal plate 22 provide theburner deck 20. Theend cap 18 is connected to the top of theperforated metal plate 22 and theperforated metal plate 22 is connected at the bottom to the support orflange 18 through a base section. Theburner deck 20 has an overall porosity which is equal to or lower than 11%, preferably lower than 10%, even more preferably lower than 9%. In an exemplary embodiment, aburner 10, with a perforation pattern as shown infigure 2C , has a length of 102,4mm and diameter of 70,4mm. The burner deck has a length of 81,2 mm and has a porosity of 7,7%. The perforation pattern in the perforated plate is a combination of slits and round holes. For a thickness of the perforated plate of 0,6 mm, the slits being 4,0x0,5mm, the holes having a diameter of 0,8mm. The perforations are grouped in a pattern of 4,8 mm and this pattern is repeated over the burner deck in an equal division. As explained above, this burner still needed an anti-noise device, but no pressure divider or distributor anymore. - An aspect of the present invention provides a
burner 10 wherein theend cap 18 is also provided with perforations.Figure 3 shows an exemplary burner wherein the end cap is provided withperforations 30. The burner deck of this burner is as shown byreference number 20. - The present invention provides a
burner 10 with a burner deck wherein more than 50% of the burner deck has a porosity being equal to or lower than 9% and wherein 10 to 50% of the burner deck has a porosity being higher than 11 %. The burner deck has an overall porosity which is equal to or lower than 11%. In an exemplary embodiment, aburner 10 as shown infigure 4 has a length of 94,8mm and diameter of 70,4mm. Theburner deck 20 has a length of 93,6mm. The perforation pattern in theperforated plate 22 is a combination of slits and round holes. The thickness of theperforated plate 22 is 0,6 mm, the slits being 4,0x0,5mm, the holes having a diameter of 0,8mm. The perforations are grouped in a pattern as shown infig. 4 , wherein the first 11,8mm of the burner deck length has a porosity of 15%, thereafter is a zone of 46,8mm of the burner deck length with a porosity of 7,3% and the last zone with a length of 5.8mm of the burner deck length having a porosity of 16,5%. This pattern is repeated over the burner deck on the circumference of the burner. This provides a burner deck which has an overall porosity of 9,8%. This modification of the perforation pattern of the burner deck provided a burner which, next to the effect of the deletion of the diffuser and the removal of the humming noise, also had a more stable response on the second and higher Helmholtz or instable acoustic resonances of the heat exchanger, which therefore made that the burner did not provoke a whistling sound anymore. Next to that, during start sequences under cold conditions, the humming sound was eliminated and therefore the use of anti-noise devices in the mixing chamber of the burner could be omitted. Furthermore, this provided a stabilized deck over the full operating range of high to low CO2's, and for a broad range of gas qualities. Furthermore, for this specific example offig. 4 , the use of the relatively high porosity at the beginning and end of theburner deck 20 provide an even more stable flame pattern of the burner. - An example embodiment according to a further aspect of the claimed invention provides a gas burner with a
perforated metal plate 22 with a perforation pattern as shown infig. 5 . The shown perforation pattern is repeated over the circumference of the burner. Here theburner deck 20 has different patterns of perforations. Adding more patterns with different pitches showed an increased stability for a broader range of gas qualities and induced less NOx-emissions. The exemplary perforation pattern offig. 5 is an abrupt and stepwise variation of the perforation pattern in theburner deck 20. -
Figure 6 shows another example of a perforation pattern ofburner deck 20 according to a preferred aspect of the present invention, wherein the porosity of theburner deck 20 decreases stepwise in downstream direction. The shown perforation pattern is repeated in theperforated metal plate 22 over the circumference of the burner. -
Figure 7 shows an example of a perforation pattern ofburner deck 20 according to a preferred aspect of the present invention, wherein the porosity is gradually increasing. This perforation pattern is repeated in theperforated metal plate 22 over the circumference of the burner. -
Figure 8 shows an exemplary perforation pattern of theburner deck 20, which is repeated lengthwise over theperforated metal plate 22. -
Figure 9 shows a further exemplary perforation pattern which is repeated on the circumference of a burner. The perforation pattern is such that no repeat of pattern is occurring along the length of theburner deck 20. An exemplary burner with a length of 91,2mm and diameter of 70,4mm. The burner deck has a length of 70,4mm. The perforation pattern in theperforated plate 22 is a combination of slits and round holes as shown infigure 9 . For a thickness of theperforated plate 22 of 0,6 mm, the slits being 4,0x0,5mm, the holes having a diameter of 0,8mm, this burner deck has an overall porosity of 7.5%. - The person skilled in the art will acknowledge that any perforation pattern or set of perforation patterns can be repeated lengthwise or over the circumference to obtain the burner according to the present invention.
- Another preferred embodiment of the present invention is shown in
figure 10 . Theburner 10 made out ofperforated metal plate 22 has a completely randomperforated burner deck 20 with no repeatability over the full height or circumference of the burner deck which provides a stabilized deck without the additional devices as mentioned above. -
Figure 11 shows another exemplary embodiment of the present invention. This burner has aperforated end cap 24 with different perforation pattern than the perforatedmetal plate 22. Theperforations 30 together with theperforations 24 provide theburner deck 20.
Claims (10)
- A gas burner (10), preferably a premix burner, comprising a support (12) having a central gas inlet port (14) for supply of gas into a gas supply chamber (16), said gas supply chamber (16) being enclosed by a cylindrical perforated metal plate (22), said cylindrical perforated metal plate (22) connected at the bottom to said support (12) through a base section, said perforation (24) in said cylindrical perforated metal plate (22) providing a burner deck (20), characterised in that said burner deck (20) has an overall porosity being equal to or lower than 11 %;
wherein more than 50% of the burner deck has a porosity being equal to or lower than 9% and wherein up to 50% of the burner deck has a porosity being higher than 11%. - A gas burner (10), as in claim 1, said burner further comprising an end cap (18) substantially opposite to said gas inlet port (14), said end cap (18) being connected to said perforated metal plate (22).
- A gas burner as in claim 2, wherein said end cap (18) is also provided with perforations (30), said perforations (30) thereby enlarging said burner deck (20).
- A gas burner as in any of the previous claims, wherein said burner deck has different patterns of perforations.
- Gas burner as in claim 4, wherein said burner deck has at least two different patterns of perforations.
- Gas burner as in claim 4, wherein said burner deck has a gradually changing porosity.
- Gas burner as in claim 4, wherein said burner deck (20) has a substantially completely random porosity.
- Gas burner as in any of the preceding claims, wherein said gas burner is devoid of a gas diffuser between the gas inlet port (14) and the perforated metal plate (22).
- Use of the gas burner as in any of the preceding claims, in a heat exchanger.
- Use of the gas burner as in any of the claims 1 to 8, in a furnace or air heater.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP17191076.3A EP3282187B1 (en) | 2009-12-11 | 2010-11-26 | Burner with low porosity burner deck |
EP10782307.2A EP2510281B1 (en) | 2009-12-11 | 2010-11-26 | Burner with low porosity burner deck |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP09178982 | 2009-12-11 | ||
PCT/EP2010/068284 WO2011069839A1 (en) | 2009-12-11 | 2010-11-26 | Burner with low porosity burner deck |
EP10782307.2A EP2510281B1 (en) | 2009-12-11 | 2010-11-26 | Burner with low porosity burner deck |
Related Child Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP17191076.3A Division EP3282187B1 (en) | 2009-12-11 | 2010-11-26 | Burner with low porosity burner deck |
EP17191076.3A Division-Into EP3282187B1 (en) | 2009-12-11 | 2010-11-26 | Burner with low porosity burner deck |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2510281A1 EP2510281A1 (en) | 2012-10-17 |
EP2510281B1 true EP2510281B1 (en) | 2017-10-25 |
Family
ID=42126102
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP17191076.3A Active EP3282187B1 (en) | 2009-12-11 | 2010-11-26 | Burner with low porosity burner deck |
EP10782307.2A Active EP2510281B1 (en) | 2009-12-11 | 2010-11-26 | Burner with low porosity burner deck |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP17191076.3A Active EP3282187B1 (en) | 2009-12-11 | 2010-11-26 | Burner with low porosity burner deck |
Country Status (6)
Country | Link |
---|---|
US (1) | US20120193452A1 (en) |
EP (2) | EP3282187B1 (en) |
JP (1) | JP2013513774A (en) |
KR (1) | KR101817371B1 (en) |
CN (1) | CN102597624B (en) |
WO (1) | WO2011069839A1 (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL2007646C2 (en) | 2011-09-16 | 2013-03-19 | Micro Turbine Technology B V | Braided burner for premixed gas-phase combustion. |
EP2805111B1 (en) | 2012-01-19 | 2018-07-04 | Bekaert Combustion Technology B.V. | Cylindrical gas premix burner |
EP2815179A1 (en) | 2012-02-16 | 2014-12-24 | Bekaert Combustion Technology B.V. | Premix gas burner |
EP2815181A1 (en) | 2012-02-16 | 2014-12-24 | Bekaert Combustion Technology B.V. | Premix gas burner |
EP2856026B1 (en) | 2012-06-01 | 2016-02-24 | Ulrich Dreizler | Burner having surface combustion |
DE202013102110U1 (en) | 2012-07-27 | 2013-10-29 | Ulrich Dreizler | Burner with a surface combustion |
US11378273B2 (en) * | 2017-01-11 | 2022-07-05 | A. O. Smith Corporation | Reduced resonance burner |
US11326808B2 (en) * | 2017-07-13 | 2022-05-10 | Bekaert Combustion Technology B.V. | Premix gas burner |
NL2024101B1 (en) | 2019-10-25 | 2021-07-19 | Bekaert Combustion Tech Bv | Surface stabilized fully premixed gas premix burner for burning hydrogen gas, and method for starting such burner |
WO2021140036A1 (en) | 2020-01-08 | 2021-07-15 | Bekaert Combustion Technology B.V. | Gas burner and heating appliance |
IT202200004688A1 (en) * | 2022-03-11 | 2023-09-11 | Beckett Thermal Solutions S R L | BURNER |
Citations (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0339499A2 (en) | 1988-04-28 | 1989-11-02 | Joh. Vaillant GmbH u. Co. | Supervision device for the burner plate operation of a panel burner |
WO1995023315A1 (en) | 1994-02-23 | 1995-08-31 | Stichting Energieonderzoek Centrum Nederland | Method and apparatus for burning highly reactive gaseous fuel |
WO1997027428A1 (en) | 1996-01-26 | 1997-07-31 | Ygnis Holding S.A. | Burner surface |
EP1036984A1 (en) | 1999-03-18 | 2000-09-20 | G. Kromschröder Aktiengesellschaft | Premix type gas burner |
US6162049A (en) | 1999-03-05 | 2000-12-19 | Gas Research Institute | Premixed ionization modulated extendable burner |
US20040132607A1 (en) | 2003-01-08 | 2004-07-08 | 3M Innovative Properties Company | Ceramic fiber composite and method for making the same |
EP1337789B1 (en) | 2000-12-01 | 2004-12-01 | Bekaert Combustion Technology Nv | Premix burner with curved impermeable end cap |
FR2914396A1 (en) | 2007-03-30 | 2008-10-03 | Inst Francais Du Petrole | NEW VAPOREFORMING OVEN USING POROUS BURNERS |
EP2037175A2 (en) | 2007-09-12 | 2009-03-18 | Polidoro S.p.A. | Premixed burner |
WO2009059933A1 (en) | 2007-11-06 | 2009-05-14 | Sit La Precisa S.P.A. | A burner, specifically a premix gas burner |
WO2009065733A1 (en) | 2007-11-19 | 2009-05-28 | Sit La Precisa S.P.A. Con Socio Unico | A burner, specifically a premix burner |
WO2009077505A2 (en) | 2007-12-17 | 2009-06-25 | Bekaert Combust. Technologie. B.V. | New premix burner |
WO2009077333A1 (en) | 2007-12-19 | 2009-06-25 | Joseph Le Mer | Device and method for stabilising the pressure and the flow of a gaseous mixture supplied to a surface-combustion cylindrical burner |
DE102008000010A1 (en) | 2008-01-07 | 2009-07-09 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Plate-shaped ceramic heat radiating body of an infrared surface radiator |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2869626A (en) * | 1954-06-28 | 1959-01-20 | Silent Glow Oil Burner Corp | Fluid fuel burning apparatus |
US3176749A (en) * | 1963-02-25 | 1965-04-06 | Burner Dev Corp | Liquid fuel-burning heater |
US3240256A (en) * | 1963-11-19 | 1966-03-15 | Canadian Patents Dev | Catalytic heater |
US3384442A (en) * | 1966-10-20 | 1968-05-21 | Gen Motors Corp | Combustion apparatus |
US4231735A (en) * | 1978-03-13 | 1980-11-04 | Downs Edgar S | Radiant heater |
US4397631A (en) * | 1980-09-08 | 1983-08-09 | The Carlin Company | Pre-mix forced draft power gas burner |
FR2589555B1 (en) * | 1985-11-06 | 1989-11-10 | Gaz De France | BLOW AIR GAS BURNER |
US5540213A (en) * | 1994-04-15 | 1996-07-30 | Desa International | Portable kerosene heater |
FR2792394B1 (en) * | 1999-04-16 | 2001-07-27 | Gaz De France | METHOD FOR REALIZING A FLAME HANGING SURFACE |
CN1317536C (en) * | 2000-09-28 | 2007-05-23 | 金相南 | Brown gas combustion apparatus and heating system using the same |
CN2473462Y (en) * | 2001-04-25 | 2002-01-23 | 杨学银 | Energy saving gas range head |
GB2396402B (en) * | 2002-12-21 | 2006-01-11 | Aeromatix Ltd | Gas burner |
EP1616128B1 (en) * | 2003-04-18 | 2016-05-04 | N.V. Bekaert S.A. | A burner with a metal membrane |
ITMO20030154A1 (en) * | 2003-05-23 | 2004-11-24 | Worgas Bruciatori Srl | MODULABLE BURNER |
JP4001097B2 (en) * | 2003-10-14 | 2007-10-31 | 松下電器産業株式会社 | Burner |
US7025810B2 (en) * | 2004-01-13 | 2006-04-11 | Arvin Technologies, Inc. | Method and apparatus for shutting down a fuel-fired burner of an emission abatement assembly |
JP3958754B2 (en) * | 2004-04-09 | 2007-08-15 | リンナイ株式会社 | Cylindrical burner |
ITMI20060147A1 (en) * | 2006-01-27 | 2007-07-28 | Worgas Bruciatori Srl | BURNER DEVICE WITH HIGH POWER |
US7770646B2 (en) * | 2006-10-09 | 2010-08-10 | World Energy Systems, Inc. | System, method and apparatus for hydrogen-oxygen burner in downhole steam generator |
ITMO20070167A1 (en) * | 2007-05-21 | 2008-11-22 | Worgas Bruciatori Srl | MODULATING BURNER |
US8784096B2 (en) * | 2009-09-29 | 2014-07-22 | Honeywell International Inc. | Low NOx indirect fire burner |
-
2010
- 2010-11-26 WO PCT/EP2010/068284 patent/WO2011069839A1/en active Application Filing
- 2010-11-26 EP EP17191076.3A patent/EP3282187B1/en active Active
- 2010-11-26 EP EP10782307.2A patent/EP2510281B1/en active Active
- 2010-11-26 JP JP2012542446A patent/JP2013513774A/en active Pending
- 2010-11-26 US US13/497,587 patent/US20120193452A1/en not_active Abandoned
- 2010-11-26 CN CN201080050224.3A patent/CN102597624B/en active Active
- 2010-11-26 KR KR1020127014887A patent/KR101817371B1/en active IP Right Grant
Patent Citations (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0339499A2 (en) | 1988-04-28 | 1989-11-02 | Joh. Vaillant GmbH u. Co. | Supervision device for the burner plate operation of a panel burner |
WO1995023315A1 (en) | 1994-02-23 | 1995-08-31 | Stichting Energieonderzoek Centrum Nederland | Method and apparatus for burning highly reactive gaseous fuel |
WO1997027428A1 (en) | 1996-01-26 | 1997-07-31 | Ygnis Holding S.A. | Burner surface |
EP0876570A1 (en) | 1996-01-26 | 1998-11-11 | Ygnis Holding S.A. | Burner surface |
US6162049A (en) | 1999-03-05 | 2000-12-19 | Gas Research Institute | Premixed ionization modulated extendable burner |
EP1036984A1 (en) | 1999-03-18 | 2000-09-20 | G. Kromschröder Aktiengesellschaft | Premix type gas burner |
EP1337789B1 (en) | 2000-12-01 | 2004-12-01 | Bekaert Combustion Technology Nv | Premix burner with curved impermeable end cap |
US20040132607A1 (en) | 2003-01-08 | 2004-07-08 | 3M Innovative Properties Company | Ceramic fiber composite and method for making the same |
FR2914396A1 (en) | 2007-03-30 | 2008-10-03 | Inst Francais Du Petrole | NEW VAPOREFORMING OVEN USING POROUS BURNERS |
EP2037175A2 (en) | 2007-09-12 | 2009-03-18 | Polidoro S.p.A. | Premixed burner |
WO2009059933A1 (en) | 2007-11-06 | 2009-05-14 | Sit La Precisa S.P.A. | A burner, specifically a premix gas burner |
WO2009065733A1 (en) | 2007-11-19 | 2009-05-28 | Sit La Precisa S.P.A. Con Socio Unico | A burner, specifically a premix burner |
WO2009077505A2 (en) | 2007-12-17 | 2009-06-25 | Bekaert Combust. Technologie. B.V. | New premix burner |
WO2009077333A1 (en) | 2007-12-19 | 2009-06-25 | Joseph Le Mer | Device and method for stabilising the pressure and the flow of a gaseous mixture supplied to a surface-combustion cylindrical burner |
DE102008000010A1 (en) | 2008-01-07 | 2009-07-09 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Plate-shaped ceramic heat radiating body of an infrared surface radiator |
Non-Patent Citations (2)
Title |
---|
ANONYMOUS: "ferritic chromium stainless steel 1.4509 (AISI 441)", METALCOR - DATASHEET, 27 November 2014 (2014-11-27), XP055519979, Retrieved from the Internet <URL:https://web.archive.org/web/20141127181233/http://www.metalcor.de/en/datenblatt/25/> |
ANONYMOUS: "Montage-und Serviceanleitung für die Fachkraft Vitodens 200-W", VIESMANN WERKE GMBH & CO. KG, 1 September 2007 (2007-09-01), pages 1 - 136, XP055608558 |
Also Published As
Publication number | Publication date |
---|---|
CN102597624A (en) | 2012-07-18 |
EP2510281A1 (en) | 2012-10-17 |
EP3282187B1 (en) | 2019-04-10 |
CN102597624B (en) | 2015-04-15 |
JP2013513774A (en) | 2013-04-22 |
US20120193452A1 (en) | 2012-08-02 |
KR20120102691A (en) | 2012-09-18 |
KR101817371B1 (en) | 2018-01-11 |
EP3282187A1 (en) | 2018-02-14 |
WO2011069839A1 (en) | 2011-06-16 |
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