WO2019193025A1 - Conical premix gas burner - Google Patents

Conical premix gas burner Download PDF

Info

Publication number
WO2019193025A1
WO2019193025A1 PCT/EP2019/058350 EP2019058350W WO2019193025A1 WO 2019193025 A1 WO2019193025 A1 WO 2019193025A1 EP 2019058350 W EP2019058350 W EP 2019058350W WO 2019193025 A1 WO2019193025 A1 WO 2019193025A1
Authority
WO
WIPO (PCT)
Prior art keywords
conical shape
textile fabric
fiber based
based textile
burner
Prior art date
Application number
PCT/EP2019/058350
Other languages
French (fr)
Inventor
Bert ELZINGA
Jelmer DORSCHMAN
Kenneth RAMDAS
Esmée MAJOR
Diederik STERENBERG
Original Assignee
Bekaert Combustion Technology B.V.
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 Bekaert Combustion Technology B.V. filed Critical Bekaert Combustion Technology B.V.
Publication of WO2019193025A1 publication Critical patent/WO2019193025A1/en

Links

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
    • F23D14/12—Radiant burners
    • F23D14/14—Radiant burners using screens or perforated plates
    • F23D14/145—Radiant burners using screens or perforated plates combustion being stabilised at a screen or a perforated plate
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2203/00—Gaseous fuel burners
    • F23D2203/10—Flame diffusing means
    • F23D2203/106—Assemblies of different layers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2212/00—Burner material specifications
    • F23D2212/20—Burner material specifications metallic
    • F23D2212/201—Fibres
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2213/00—Burner manufacture specifications
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00019—Outlet manufactured from knitted fibres

Abstract

A premix gas burner comprises a composite porous substrate which comprises a fiber based textile fabric and a porous metal structure. The fiber based textile fabric is provided onto and contacting the porous metal structure. The fiber based textile fabric is provided for combustion of premix gas onto the fiber based textile fabric after the premix gas has flown through the composite porous substrate. The composite porous substrate comprises a conical shape. A rim is provided along the length of the conical shape. The rim is provided by contact of the internal sides or of the external sides of the two end strips of the composite porous substrate shaped into conical shape. The internal side of the composite porous substrate is the side internal to the conical shape. The rim comprises fiber based textile fabric and porous metal structure. The fiber based textile fabric is located at the inside of the conical shape. The porous metal structure is located at the outside of the conical shape. The rim is provided by contact of the internal sides of the two end strips of the composite porous substrate shaped into conical shape. The rim is directed to the outside of the conical shape. The conical shape has a first cone angle. The burner comprises an annular porous section. The annular porous section is connected to the conical shape at the cross section of the conical shape having the largest diameter. The annular porous section is flat or the annular porous section is frusto-conical with a cone angle larger than the first cone angle.

Description

Conical premix gas burner
Description
Technical Field
[1] The invention relates to conical premix gas burners at which combustion occurs on a fiber based burner deck, positioned onto a perforated plate or woven wire mesh.
Background Art
[2] Surface stabilized premix gas burners exist in a plurality of different shapes. Although US6065963 is entitled“Conical surface burner”, the document rather shows a burner with a frusto-conical shape. The combustion is stabilized on a knitted structure comprising heat-resistant stainless steel fibers. The knitted structure is supported by a net. The knitted structure can be attached to the net, e.g. by means of spot welds.
[3] EP2713105A1 discloses a surface stabilized premix burner having a conical or frusto- conical combustion surface. Combustion occurs at the inside of the cone or the frusto- cone. The combustion surface is formed by at least one sheet-shaped plate which has a plurality of openings. Such burner can be advantageously used in so-called two-pass boilers, also called flame-inversion type boilers.
Disclosure of Invention
[4] It is the objective of the invention to provide a conical premix gas burner that can be
manufactured more easily.
[5] The first aspect of the invention is a premix gas burner comprising a composite porous substrate. The composite porous substrate comprises a fiber based textile fabric and a porous metal structure. The fiber based textile fabric is provided onto and contacting the porous metal structure. The fiber based textile fabric is provided for combustion of premix gas onto the fiber based textile fabric after the premix gas has flown through the composite porous substrate. Thus, the fiber based textile fabric provides a burner deck in the burner. The composite porous substrate comprises a conical shape. A rim is provided along the length of the conical shape. The rim is provided by contact of the internal sides or of the external sides of the two end strips of the composite porous substrate shaped into conical shape. The internal side of the composite porous substrate is the side internal to the conical shape. The rim comprises fiber based textile fabric and porous metal structure. The fiber based textile fabric is located at the inside of the conical shape. The porous metal structure is located at the outside of the conical shape. The rim is provided by contact of the internal sides of the two end strips of the composite porous substrate shaped into conical shape. The rim is directed to the outside of the conical shape. The conical shape has a first cone angle. The burner comprises an annular porous section. The annular porous section is connected to the conical shape at the cross section of the conical shape having the largest diameter. The annular porous section is flat or the annular porous section is frusto-conical with a cone angle larger than the first cone angle. [6] The second aspect of the invention is a method for manufacturing a premix gas burner as in the first aspect of the invention. The method comprises the steps of
- providing a fiber based textile fabric and a porous metal structure;
- attaching - preferably by means of welding - the fiber based textile fabric and the porous metal structure to each other, thereby creating a composite porous substrate;
- folding the composite porous substrate such that the folded structure comprises a conical shape and such that a rim is provided along the length of the conical shape, wherein the rim is provided by contact of the internal sides or of the external sides of the two end strips of the composite porous substrate shaped into conical shape. The internal side of the composite porous substrate is the side internal to the conical shape; and
- bonding the two end strips in the rim to each other, preferably by means of welding.
[7] It has been shown to be difficult to make a burner deck having a conical shape. However, The invention provides an improved way to manufacture a premix gas burner having a conical burner deck. It is particularly more easy to shape the point of the cone correctly.
[8] In a preferred burner, the two end strips in the rim are bonded to each other, preferably by means of welds. As an example, capacitor discharge welding can be used to weld the two end strips in the rim to each other.
[9] Preferably, the fiber based textile fabric is bonded by means of welds onto the porous metal structure. More preferably, the welds are provided on discrete points, preferably spread over the surface of the fiber based textile fabric, even more preferably according to a regular pattern. As an example, capacitor discharge welding can be used to bond the fiber based textile fabric onto the porous metal structure.
[10] Preferably, the porous metal structure comprises or consists out of a woven wire mesh, a perforated metal plate or an expanded metal mesh.
[11] Preferably, the fiber based textile fabric comprises or consists out of a woven, knitted, braided or nonwoven fabric. Preferably, the fiber based textile fabric comprises or consists out of yarns, more preferably, the yarns comprise metal fibers, even more preferably stainless steel fibers. A particularly preferred fiber based textile fabric is a weft knitted fabric.
[12] Yarns for the fiber based textile fabric used in the invention can e.g. be spun from stretch broken fibers (such as bundle drawn stretch broken fibers) or e.g. yarns made from shaved or machined fibers. The yarns can be plied yarns, e.g. two ply, three ply...
Preferred fabrics made from metal fibers have a weight of between 0.6 and 3 kg/m2; preferably between 0.7 and 3 kg/m2, even more preferred between 1.2 and 2.5 kg/m2.
[13] The fiber based textile fabric can comprise or consist out of metal fibers. Examples of preferred ranges of metal fibers are stainless steel fibers. A specifically preferred range of stainless steel fibers are chromium and aluminium comprising stainless steel fibers as in DIN 1.4767, e.g. as are known under the trademark FeCrAlloy. Preferred are fibers with equivalent diameter less than 40 pm. With equivalent diameter of a fiber is meant the diameter of a circle with the same surface area as the cross sectional area of that fiber. [14] Metal fibers for the fiber based textile fabric, e.g. stainless steel fibers, e.g. with an equivalent diameter less than 40 micrometers, e.g. less than 25 micrometers, can be obtained by a bundle drawing technique. This technique is disclosed e.g. in US-A- 2050298, US-A-3277564 and in US-A-3394213. Metal wires are forming the starting material and are covered with a coating such as iron or copper. A bundle of these covered wires is subsequently enveloped in a metal pipe. Thereafter the thus enveloped pipe is reduced in diameter via subsequent wire drawing steps to come to a composite bundle with a smaller diameter. The subsequent wire drawing steps may or may not be alternated with an appropriate heat treatment to allow further drawing. Inside the composite bundle the initial wires have been transformed into thin fibers which are embedded separately in the matrix of the covering material. Such a bundle preferably comprises not more than 2000 fibers, e.g. between 500 and 1500 fibers. Once the desired final diameter has been obtained the covering material can be removed e.g. by solution in an adequate pickling agent or solvent. The final result is the naked fiber bundle.
[15] Alternatively metal fibers for the fiber based textile fabric, such as stainless steel fibers can be manufactured in a cost effective way by machining a thin plate material. Such a process is disclosed e.g. in US-A-4930199. A strip of a thin metal plate is the starting material. This strip is wound around the cylindrical outer surface of a rotatably supported main shaft a number of times and is fixed thereto. The main shaft is rotated at constant speed in a direction opposite to that in which the plate material is wound. A cutter having an edge line expending perpendicularly to the axis of the main shaft is fed at constant speed. The cutter has a specific face angle parallel to the axis of the main shaft. The end surface of the plate material is cut by means of the cutter.
[16] Yet an alternative way of producing metal fibers for the fiber based textile fabric is via extracting or extrusion from a melt.
[17] Another alternative way of producing metal fibers is machining fibers from a solid block of metal.
[18] As an alternative for or in combination with metal fibers, ceramic fibers can be used in the fiber based textile fabric.
[19] Preferably, the annular porous section comprises or consists out of a second fiber based textile fabric and a second porous metal structure. The second fiber based textile fabric is positioned onto the second porous metal structure. The second fiber based textile fabric is provided for combustion of premix gas onto the second fiber based textile fabric after the premix gas has flown first through the second porous metal structure and then through the second fiber based textile fabric. Thus, the second fiber based textile fabric forms another burner deck of the burner. The annular porous section is provided for stabilization of the combustion on the surface of the burner as the annular porous section anchors the flames well onto the burner and effectively prevents flame lift off.
More preferably, the second fiber based textile fabric is integrally part of the fiber based textile fabric, e.g. as an annular rim to the part of the fiber based textile fabric shaped into conical shape. The second porous metal structure can be an integral part of the porous metal structure, but is preferably a separate part, e.g. comprising or consisting out of a perforated plate structure. Even more preferably, the porosity of the second porous metal structure - e.g. a perforated plate structure - is lower than the porosity of the porous metal structure. The porosity determines the rate of flow of premix gas: a lower porosity results in a lower flow rate (per unit of time and per unit of surface area) of premix gas.
[20] In a preferred embodiment, the burner comprises a main body, a gas mixing chamber delimited by the main body and by the external surface of the conical shape; and an entrance for introducing a premix of combustible gas and air into the gas mixing chamber. In a preferred embodiment, the main body is cylindrical in shape or comprises a segment which is cylindrical in shape.
[21] A third aspect of the invention is a premix gas combustion system comprising a
combustion chamber having lateral walls; and a premix gas burner as in the first aspect of the invention. The premix gas burner is provided at a first longitudinal end of the combustion chamber. The second longitudinal end of the combustion chamber is closed by a wall. The combustion chamber is provided for combustion of the premix gas after the premix gas has flown from the gas mixing chamber through the composite porous substrate. An exit for combustion products is provided in the combustion chamber at the first longitudinal end of the combustion chamber.
[22] A fourth aspect of the invention is a heat cell comprising a premix gas burner as in any embodiment of the first aspect of the invention or comprising a premix gas combustion system as in the third aspect of the invention.
Brief Description of Figures in the Drawings
[23] Figure 1 shows a premix gas burner according to the invention.
Figure 2 shows a cross section of the burner of figure 1.
Figure 3 shows a premix gas combustion system comprising a premix gas burner according to the invention.
Mode(s) for Carrying Out the Invention
[24] Figure 1 shows an example of a premix gas burner 10 according to the invention. Figure 2 shows a cross section of the burner of figure 1 along plane ll-ll of figure 1. The premix gas burner 10 comprises a composite porous substrate 12. The composite porous substrate comprises a fiber based textile fabric 14 and a porous metal structure 16. In the example, the porous metal structure consists out of a woven wire mesh. The fiber based textile fabric is a weft knitted fabric knitted from yarns comprising heat resistant stainless steel fibers.
[25] The fiber based textile fabric 14 is provided onto and contacting the porous metal
structure 16. The fiber based textile fabric is provided for combustion of premix gas onto the fiber based textile fabric after the premix gas has flown through the composite porous substrate. The fiber based textile fabric is bonded onto the porous metal structure by means of spot welds 24.
[26] The composite porous substrate comprises a conical shape having a cone angle. The fiber based textile fabric 14 is located at the inside of the conical shape and the porous metal structure 16 is located at the outside of the conical shape. A rim 18 is provided along the length of the conical shape. The rim is provided by contact of the internal sides of the two end strips 20, 22 of the composite porous substrate shaped into conical shape. The rim comprises fiber based textile fabric and porous metal structure. In the rim the two end strips are bonded to each other by means of welds. The rim is directed to the outside of the conical shape.
[27] The fiber based textile fabric shaped into conical shape of the burner of the example comprises - although not essential for the invention - as an integral part of the fiber based textile fabric an annular rim 30 at the largest diameter of the cross section of the conical shape. The function of this annular rim will be explained when describing figure 3 which shows a premix gas combustion system comprising the premix gas burner of figure 1.
[28] The burner of figure 1 can be made in a simple and reliable way. A weft knitted fabric knitted from yarns comprising stainless steel fibers; and a woven wire mesh are provided. Both are cut to the required shape. The weft knitted fabric is spot welded at several positions over its surface to the woven wire mesh, thereby creating the composite substrate. Subsequently, the composite porous substrate is folded and shaped - with the weft knitted fabric to the inside - into conical shape and such that a rim is provided along the length of the conical shape. The rim is provided by contact of the internal sides of the two end strips of the composite porous substrate shaped into conical shape. The two end strips are bonded to each other in the rim by means of welding.
[29] Figure 3 shows a premix gas combustion system 40 comprising the premix gas burner 10 of figure 1 , with the annular rim 30 of the fiber based textile fabric 14. The rim of the premix gas burner is not shown in figure 3. The composite porous substrate of the burner comprises a conical shape having a cone angle a.
[30] The burner comprises an annular porous section 32. The annular porous section is
connected to the conical shape at the cross section of the conical shape having the largest diameter. In the example, the annular porous section is flat. The annular porous section consists out of the annular rim 30 of the fiber based textile fabric positioned onto a perforated plate 34 having an annular shape. The porosity of the perforated plate 34 having an annular shape is lower than the porosity of the woven wire mesh. Therefore, when the premix gas burner is in use the flow rate (per unit of time and per unit of surface area) of premix gas will be higher through the woven wire mesh than through the perforated plate having an annular shape.
[31] The burner further comprises a cylindrical main body 42, a gas mixing chamber 44
delimited by the main body and by the external surface of the conical shape; and an entrance 46 for introducing a premix of combustible gas and air into the gas mixing chamber.
[32] The premix gas combustion system 40 further comprises a combustion chamber 48 having lateral walls 50. The premix gas burner is provided at a first longitudinal end of the combustion chamber 48. The second longitudinal end of the combustion chamber is closed by a wall 52. The combustion chamber is provided for combustion (see flames 53) of the premix gas after the premix gas has flown from the gas mixing chamber through the composite porous substrate.
[33] The annular rim 30 of the fiber based textile fabric is provided for combustion of premix gas onto it after the premix gas has flown first through the perforated plate having an annular shape and then through the second fiber based textile fabric. Thus, the annular rim forms another burner deck of the burner. The annular rims is specifically provided for stabilization of the flames on the burner.
[34] The flow of the combustion products is represented by flow lines 54. An exit 56 for
combustion products is provided in the combustion chamber at the first longitudinal end of the combustion chamber.

Claims

Claims
1. Premix gas burner,
comprising a composite porous substrate;
wherein the composite porous substrate comprises a fiber based textile fabric and a porous metal structure;
wherein the fiber based textile fabric is provided onto and contacting the porous metal structure;
wherein the fiber based textile fabric is provided for combustion of premix gas onto the fiber based textile fabric after the premix gas has flown through the composite porous substrate; wherein the composite porous substrate comprises a conical shape;
wherein a rim is provided along the length of the conical shape, wherein the rim is provided by contact of the internal sides or of the external sides of the two end strips of the composite porous substrate shaped into conical shape; wherein the internal side of the composite porous substrate is the side internal to the conical shape;
wherein the rim comprises fiber based textile fabric and porous metal structure;
wherein the fiber based textile fabric is located at the inside of the conical shape;
wherein the porous metal structure is located at the outside of the conical shape;
wherein the rim is provided by contact of the internal sides of the two end strips of the composite porous substrate shaped into conical shape;
and wherein the rim is directed to the outside of the conical shape;
wherein the conical shape has a first cone angle;
wherein the burner comprises an annular porous section;
wherein the annular porous section is connected to the conical shape at the cross section of the conical shape having the largest diameter;
and wherein the annular porous section is flat or wherein the annular porous section is frusto- conical with a cone angle larger than the first cone angle.
2. Burner as in claim 1 , wherein in the rim the two end strips are bonded to each other, preferably by means of welds.
3. Burner as in any of the preceding claims, wherein the fiber based textile fabric is bonded by means of welds onto the porous metal structure.
4. Burner as in any of the preceding claims, wherein the porous metal structure comprises or consists out of a woven wire mesh, a perforated metal plate or an expanded metal mesh.
5. Burner as in any of the preceding claims, wherein the fiber based textile fabric comprises or consists out of a woven, knitted, braided or nonwoven fabric.
6. Burner as in any of the preceding claims,
wherein the annular porous section comprises or consists out of a second fiber based textile fabric and a second porous metal structure, wherein the second fiber based textile fabric is positioned on the second porous metal structure;
wherein the second fiber based textile fabric is provided for combustion of premix gas onto the second fiber based textile fabric after the premix gas has flown first through the second porous metal structure and then through the second fiber based textile fabric.
7. Burner as in claim 6, wherein the second fiber based textile fabric is integrally part of the fiber based textile fabric.
8. Burner as in claim 6 or 7, wherein the porosity of the second porous metal structure is lower than the porosity of the porous metal structure.
9. Burner as in any of the preceding claims, comprising
- a main body;
- a gas mixing chamber delimited by the main body and by the external surface of the conical shape; and
- an entrance, for introducing a premix of combustible gas and air into the gas mixing chamber.
10. Premix gas combustion system, comprising
- a combustion chamber having lateral walls; and
- a premix gas burner as in claim 9;
wherein the premix gas burner is provided at a first longitudinal end of the combustion chamber;
wherein the second longitudinal end of the combustion chamber is closed by a wall;
wherein the combustion chamber is provided for combustion of the premix gas after the premix gas has flown from the gas mixing chamber through the composite porous substrate; and wherein an exit for combustion products is provided in the combustion chamber at the first longitudinal end of the combustion chamber.
11. Heat cell comprising a premix gas burner as in any of the preceding claims 1 - 9 or comprising a premix gas combustion system as in claim 10.
12. Method for manufacturing a premix gas burner as in any of the claims 1 - 9, comprising the steps of
- providing a fiber based textile fabric and a porous metal structure;
- attaching - preferably by means of welding - the fiber based textile fabric and the porous metal structure to each other, thereby creating a composite porous substrate;
- folding the composite porous substrate such that the folded structure comprises a conical shape and such that a rim is provided along the length of the conical shape, wherein the rim is provided by contact of the internal sides or of the external sides of the two end strips of the composite porous substrate shaped into conical shape; wherein the internal side of the composite porous substrate is the side internal to the conical shape; and
- bonding the two end strips in the rim to each other, preferably by means of welding.
PCT/EP2019/058350 2018-04-05 2019-04-03 Conical premix gas burner WO2019193025A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP18165834 2018-04-05
EP18165834.5 2018-04-05

Publications (1)

Publication Number Publication Date
WO2019193025A1 true WO2019193025A1 (en) 2019-10-10

Family

ID=61906732

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2019/058350 WO2019193025A1 (en) 2018-04-05 2019-04-03 Conical premix gas burner

Country Status (1)

Country Link
WO (1) WO2019193025A1 (en)

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2050298A (en) 1934-04-25 1936-08-11 Thos Firth & John Brown Ltd Metal reducing method
US3277564A (en) 1965-06-14 1966-10-11 Roehr Prod Co Inc Method of simultaneously forming a plurality of filaments
US3391983A (en) * 1965-08-12 1968-07-09 Matsushita Electric Ind Co Ltd Radiating gas burner apparatus
US3394213A (en) 1964-03-02 1968-07-23 Roehr Prod Co Inc Method of forming filaments
US4930199A (en) 1987-12-09 1990-06-05 Akira Yanagisawa Method for manufacturing fiber from thin plate material
US6065963A (en) 1997-01-10 2000-05-23 N.V. Bekaert S.A. Conical surface burner
JP3098381B2 (en) * 1994-07-14 2000-10-16 リンナイ株式会社 Surface burning burner
US20030005892A1 (en) * 2000-01-10 2003-01-09 Baese David C. Water heater with continuously variable air and fuel input
US20130312700A1 (en) * 2012-05-23 2013-11-28 Paloma Co., Ltd. Rich-lean burner
EP2713105A1 (en) 2012-09-27 2014-04-02 Systema Polska Sp. zo. o Gas combustion head for premixed burners and burner provided with the aforesaid combustion head
US20150192291A1 (en) * 2014-01-06 2015-07-09 Rheem Manufacturing Company Multi-Cone Fuel Burner Apparatus For Multi-Tube Heat Exchanger
EP3064831A1 (en) * 2015-02-16 2016-09-07 Worgas Bruciatori S.r.l. Gas burner for a heater

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2050298A (en) 1934-04-25 1936-08-11 Thos Firth & John Brown Ltd Metal reducing method
US3394213A (en) 1964-03-02 1968-07-23 Roehr Prod Co Inc Method of forming filaments
US3277564A (en) 1965-06-14 1966-10-11 Roehr Prod Co Inc Method of simultaneously forming a plurality of filaments
US3391983A (en) * 1965-08-12 1968-07-09 Matsushita Electric Ind Co Ltd Radiating gas burner apparatus
US4930199A (en) 1987-12-09 1990-06-05 Akira Yanagisawa Method for manufacturing fiber from thin plate material
JP3098381B2 (en) * 1994-07-14 2000-10-16 リンナイ株式会社 Surface burning burner
US6065963A (en) 1997-01-10 2000-05-23 N.V. Bekaert S.A. Conical surface burner
US20030005892A1 (en) * 2000-01-10 2003-01-09 Baese David C. Water heater with continuously variable air and fuel input
US20130312700A1 (en) * 2012-05-23 2013-11-28 Paloma Co., Ltd. Rich-lean burner
EP2713105A1 (en) 2012-09-27 2014-04-02 Systema Polska Sp. zo. o Gas combustion head for premixed burners and burner provided with the aforesaid combustion head
US20150192291A1 (en) * 2014-01-06 2015-07-09 Rheem Manufacturing Company Multi-Cone Fuel Burner Apparatus For Multi-Tube Heat Exchanger
EP3064831A1 (en) * 2015-02-16 2016-09-07 Worgas Bruciatori S.r.l. Gas burner for a heater

Similar Documents

Publication Publication Date Title
EP3017098B1 (en) Gas premix burner
US6065963A (en) Conical surface burner
KR100352581B1 (en) Electrically Regenerated Diesel Particle Filter Cartridges and Filters
EP2914903B1 (en) Gas premix burner
EP2789911B1 (en) Gas premix burner
EP3017099B1 (en) Premix gas burner
WO2019193025A1 (en) Conical premix gas burner
EP3631295B1 (en) Inwardly firing premix gas burner, premix gas combustion system using the burner, and method of operating the burner or the system
EP2815181A1 (en) Premix gas burner
EP3572728B1 (en) Premix gas burner
EP2844920B1 (en) Gas premix burner
EP3431872A1 (en) Cylindrical premix gas burner
US20180112867A1 (en) Inwardly burning surface stabilized gas premix burner
CN101522282A (en) Wound wire filter elements
EP2815179A1 (en) Premix gas burner
KR101335553B1 (en) Manufacturing Method of Seamless Cylindrical Metal Fiber Mat
US20230375174A1 (en) Burner liner
CN117433016A (en) Combustion film for gas burner made of continuous fiber thread
JP2010084307A (en) Cylindrical air filter and production method thereof
JPH07109515A (en) Direct firing reduction heating method and burner structure for direct firing reduction heating

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 19713819

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

WWE Wipo information: entry into national phase

Ref document number: 2019713819

Country of ref document: EP

ENP Entry into the national phase

Ref document number: 2019713819

Country of ref document: EP

Effective date: 20201105

122 Ep: pct application non-entry in european phase

Ref document number: 19713819

Country of ref document: EP

Kind code of ref document: A1