WO2008065554A1 - Burner with means for changing the direction of fuel flow - Google Patents

Burner with means for changing the direction of fuel flow Download PDF

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Publication number
WO2008065554A1
WO2008065554A1 PCT/IB2007/054281 IB2007054281W WO2008065554A1 WO 2008065554 A1 WO2008065554 A1 WO 2008065554A1 IB 2007054281 W IB2007054281 W IB 2007054281W WO 2008065554 A1 WO2008065554 A1 WO 2008065554A1
Authority
WO
WIPO (PCT)
Prior art keywords
burner
duct
fuel
main axis
outlet
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.)
Ceased
Application number
PCT/IB2007/054281
Other languages
French (fr)
Inventor
Ib Ohlsen
Lars Skaarup Jensen
Jens Peter Hansen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
FLSmidth AS
Original Assignee
FLSmidth AS
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
Priority to UAA200904626A priority Critical patent/UA97963C2/en
Priority to CN2007800435162A priority patent/CN101542204B/en
Priority to AU2007326900A priority patent/AU2007326900B2/en
Priority to MX2009005411A priority patent/MX2009005411A/en
Priority to JP2009538807A priority patent/JP5394247B2/en
Priority to EP07826814.1A priority patent/EP2087285A4/en
Priority to CA 2667921 priority patent/CA2667921C/en
Priority to US12/513,901 priority patent/US20100003625A1/en
Priority to BRPI0719644-0A2A priority patent/BRPI0719644A2/en
Application filed by FLSmidth AS filed Critical FLSmidth AS
Publication of WO2008065554A1 publication Critical patent/WO2008065554A1/en
Priority to EG2009040594A priority patent/EG25502A/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D17/00—Burners for combustion simultaneously or alternately of gaseous or liquid or pulverulent fuel
    • 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
    • F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27—FURNACES; KILNS; OVENS; RETORTS
    • F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D99/00—Subject matter not provided for in other groups of this subclass
    • F27D99/0001—Heating elements or systems
    • F27D99/0033—Heating elements or systems using burners
    • 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
    • F23D2900/14—Special features of gas burners
    • F23D2900/14481—Burner nozzles incorporating flow adjusting means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27—FURNACES; KILNS; OVENS; RETORTS
    • F27B—FURNACES, KILNS, OVENS OR RETORTS IN GENERAL; OPEN SINTERING OR LIKE APPARATUS
    • F27B7/00—Rotary-drum furnaces, i.e. horizontal or slightly inclined
    • F27B7/20—Details, accessories or equipment specially adapted for rotary-drum furnaces
    • F27B7/34—Arrangements of heating devices

Definitions

  • Burner with means for changing the direction of fuel flow
  • the present invention relates to a burner for introducing solid, liquid or gaseous fuel to a burning zone of a kiln, such as a rotary kiln for manufacturing cement clinker or the like, said burner comprising a number of substantially concentric ducts, which are parallel to the main axis of the burner, for conveying fuel and primary air to nozzle openings, and a number of additional ducts for conveying solid, fluid or gaseous fuel to separate nozzle openings, with said additional ducts being located in the central part of the burner.
  • Burners of the aforementioned kind are known for example from EP 965 019 and EP 967 434. These known burners comprise in the central part one or several ducts for conveying fuel, said ducts being surrounded by annular, concentric channels for introducing primary air. These centrally located channels are often used for introducing alternative fuels such as solid fuels comprising for example plastics, paper, rubber and wood chips or liquid fuels such as for example oil or mixtures of solid and/or liquid fuels.
  • the burner comprises means for changing the flow direction of the fuel which is introduced via at least one of the additional ducts in the central part of the burner, relative to the main axis of the burner, at least partially in an ascending direction.
  • the means for changing the flow direction of the fuel may be made up of any suitable means.
  • the means for changing the flow direction of the fuel which is introduced via at least one of the additional ducts in the central part of the burner comprises an injection duct which is located at the outlet point of the duct in question in immediate extension hereof, with its centreline forming an angle relative to the main axis of the burner. It is preferred that the injection duct is located so that it points upward in relation to the main axis of the burner at an angle between 1° and 25°, preferentially between 5° and 15° and most preferentially between 7° and 10°. It is further preferred that the lowest point of the outlet of the injection duct is located at a level above the upper part of the pipes of the duct in question.
  • the injection duct may in a special embodiment have an oval cross-section or may otherwise be configured so that the height/width ratio is less than 1. If this is the case, the injection velocity may be varied either by changing the cross-sectional area of the injection duct or by changing the airflow rate which is injected simultaneously with the fuel.
  • the fuel is introduced in parallel to the main axis of the burner.
  • the means for changing the flow direction of the fuel which is introduced via at least one of the additional ducts in the central part of the burner comprises an air duct, the outlet of which is located immediately at or at least partially enclosing the duct in question in such a way that the centre of gravity of the outlet cross-section of the air duct is displaced in relation to the centre of gravity of the outlet cross-section of the duct in question.
  • the change in the flow direction of the fuel is effected according to a method which involves that the cross-section of the outlet, or in other words the flow-through area of the air duct outlet is not uniformly distributed across the outlet of the fuel duct in question, entailing also that the quantity of air flowing through the air duct outlet is not uniformly distributed across the circumference of the fuel duct outlet in question. Since the greatest movement quantity of the air will occur in the area or areas of the air duct outlet where the highest air passage rates occur, the airflow in this area or these areas will physically impact the fuel so that this flow direction is changed in direction toward this area or these areas.
  • This second embodiment of the invention may be combined with the aforementioned first embodiment.
  • the fuel is also introduced in parallel to the main axis of the burner.
  • the means for changing the flow direction of the fuel which is introduced via at least one of the additional ducts in the central part of the burner comprises a separate air duct, the outlet of which is located immediately at or at least partially enclosing the duct in question, and forming an angle relative to the main axis of the burner.
  • the flow direction of the fuel is changed according to a method whereby the air being injected via the separate air duct forces the fuel in a different direction determined as a function of the angle formed by the air duct in relation to the main axis of the burner.
  • the air duct is fitted so that it points upward relative to the main axis of the burner at an angle of between 8° and 80°, preferentially between 35° and 60°. In this embodiment the direction and velocity of injection will be changed by varying the airflow rate.
  • This third embodiment of the invention may be combined with one or both of the embodiments described above.
  • the duct 4a, 4 may be configured with an outlet cross-section which forms an angle which is different from 90° relative to the centreline through the duct. Such a configuration can be used to effect a change in the direction of the fuel stream exclusively or in combination with the above-mentioned embodiments.
  • Fig. 1 shows a first embodiment of the burner according to the invention
  • Fig. 2 shows a second embodiment of the burner according to the invention
  • Fig. 3 shows a third embodiment of the burner according to the invention.
  • Figs. 1-3 show front views as well as sectional views of three different embodiments of the burner according to the invention, and they all comprise two substantially concentric ducts 1 and 2 for conveying primary air which are parallel to the main axis B a , and a herewith concentric duct 3 for pneumatic conveyance of coal dust and a central part 10 which comprises a duct 4 for conveying solid alternative fuel, and a number of additional ducts or pipes 6, 7 and 8 for ignition gas burner, oil burner and gas burner, respectively.
  • the burners shown in Figs. 2 and 3 also comprise an air duct 5 which encloses the duct 4.
  • the burner comprises an introduction duct 4a which is fitted in extension of the duct 4 for conveying solid alternative fuel.
  • the introduction duct 4a is arranged so that it points upward relative to the main axis of the burner at an angle ⁇ of approximately 8° relative to its centreline.
  • the injection velocity of the fuel can be varied by changing the cross-sectional area of the introduction duct 4a or by varying the airflow rate which is injected simultaneously with the fuel.
  • the burner comprises, as mentioned, an air duct 5, the outlet of which is located so that it encloses the duct 4 for conveying solid alternative fuel.
  • the air duct 5 is arranged so that the centre of gravity of the outlet cross-section of the air duct 5 is displaced upwards relative to the centre of gravity of the outlet cross- section of the duct 4.
  • the largest quantity of air will flow through the upper part of the air duct 5, thereby impacting the fuel stream in upward direction, hence changing the flow of direction of the fuel in the upward direction.
  • the movement quantity of the air in the shown embodiment will be greatest in the upper area of the outlet of the air duct 5.
  • this second embodiment of the invention may be combined with the first embodiment described above, although this is not shown in the drawing.
  • the burner comprises, as mentioned, an air duct 5 the outlet of which is located so that it encloses the duct 4 for conveying solid alternative fuel.
  • the air duct 5 is arranged so that it points upwards, forming an angle ⁇ of approximately 65° relative to the main axis of the burner. This will cause the flow direction of the fuel to be changed in the upward direction due to the fact that the airflow being injected via the air duct 5 will force the fuel in the upward direction.
  • the direction and velocity of injection can be changed by varying the airflow rate.
  • This third embodiment of the invention may as previously mentioned be combined with one or both of the aforementioned embodiments.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Curing Cements, Concrete, And Artificial Stone (AREA)
  • Muffle Furnaces And Rotary Kilns (AREA)
  • Furnace Details (AREA)
  • Combustion Of Fluid Fuel (AREA)
  • Gas Burners (AREA)

Abstract

A description is given of a burner for introducing solid, liquid or gaseous fuel to a burning zone of a kiln, such as a rotary kiln for manufacturing cement clinker or the like, said burner comprising a number of substantially concentric ducts (1, 2, 3), being parallel to the main axis B3 of the burner, for conveying fuel and primary air to nozzle openings, as well as a number of additional ducts (4, 6, 7, 8) for conveying solid, fluid or gaseous fuel to separate nozzle openings, said additional ducts being located in the central part (10) of the burner. The burner is characterized in that it comprises means (4a, 5) for changing the flow direction of the fuel which is introduced via at least one of the additional ducts in the central part (10) of the burner, relative to the main axis B3 of the burner, at least in an ascending direction. This will allow the individual fuel particles to travel in a curved, approximately ballistic path, thereby extending the time they can be maintained in the flame. Another advantage of this configuration of the burner is that the large particles will attain the highest, and hence the longest, path, since the path of the smaller particles will to a greater extent than is the case for the large ones be deflected by the primary air which is injected via the outer annular primary air nozzle which is parallel to the main axis of the burner. Hence it will be possible to achieve a more uniform combustion of all particles, regardless of their size. It will be possible to change the path of the particles by altering the velocity or direction of injection.

Description

Burner with means for changing the direction of fuel flow
The present invention relates to a burner for introducing solid, liquid or gaseous fuel to a burning zone of a kiln, such as a rotary kiln for manufacturing cement clinker or the like, said burner comprising a number of substantially concentric ducts, which are parallel to the main axis of the burner, for conveying fuel and primary air to nozzle openings, and a number of additional ducts for conveying solid, fluid or gaseous fuel to separate nozzle openings, with said additional ducts being located in the central part of the burner.
Burners of the aforementioned kind are known for example from EP 965 019 and EP 967 434. These known burners comprise in the central part one or several ducts for conveying fuel, said ducts being surrounded by annular, concentric channels for introducing primary air. These centrally located channels are often used for introducing alternative fuels such as solid fuels comprising for example plastics, paper, rubber and wood chips or liquid fuels such as for example oil or mixtures of solid and/or liquid fuels.
When for example solid fuel is injected via a fuel duct into a flame in a rotary kiln for cement manufacturing, it is essential to ensure that the individual fuel particles are kept suspended for as long as possible in order to achieve complete combustion of the majority of the particles before they drop into the material charge. However, it will rarely be possible to achieve complete combustion of the largest fuel particles which will drop into the material charge, with a continuation of the combustion process at this location. In such cases, it would be advantageous for these particles to be led so far into the kiln as is practicably possible in order to achieve full combustion of the particles prior to the discharge of the material from the kiln, always providing that the material, as is the case in a typical rotary kiln for manufacturing of cement, is transported in direction which is opposite to that in which the fuel is injected. If this is not the case, unburned particles may cause damage to the material charge in the rotary kiln. Quite often, solid alternative fuels will have a highly variable particle size and, as a rule, they will be less finely comminuted than solid fossil fuels. Also, the comminution of alternative fuels may be a relatively complex and expensive process. Therefore, many burners are configured so that a small amount of the primary air is injected through annular, concentric ducts surrounding the individual ducts for alternative fuel. Such a configuration will allow even relatively large particles to remain suspended until complete combustion has been achieved. In EP 967 434, a description is given of separate annular ducts for primary air which are concentrically positioned around the ducts for solid fuel. Such a configuration would make it possible to increase the time the fuel particles can be maintained in a state of suspension, thereby leading to improved combustion efficiency. It is also proposed in this patent application that the primary air is injected subject to rotation causing the fuel particles to be scattered further outwards in the cross-sectional area of the flame, thereby improving combustion efficiency. However, disadvantages may be associated with the injection of air subject to rotation since it may cause large particles to be thrust outward all the way to the point of the flame before complete combustion of these particles has been achieved. This may entail risk of the fuel particles dropping through, with attendant risk of the quality of the material in the kiln being impaired. Also, it is a common characteristic of the known burners that the fuel is introduced to the kiln in a flow of direction which is substantially parallel to the main axis of the burner. In this context, the expression "flow direction" is taken to mean the direction described, on average, by the fuel particles in a fuel stream. In cases where the fuel is introduced subject to rotation, the flow direction of the fuel will thus coincide approximately with the line of symmetry for the fuel stream. It is the objective of the present invention to provide a burner by means of which the alternative fuel can be maintained in the flame for a longer period of time without any of the aforementioned disadvantages.
According to the invention this is achieved by a method of the kind mentioned in the introduction and being characterized in that the burner comprises means for changing the flow direction of the fuel which is introduced via at least one of the additional ducts in the central part of the burner, relative to the main axis of the burner, at least partially in an ascending direction.
Hence it will be possible for the individual fuel particles to travel in a curved, approximately ballistic path, thereby extending the time they can be maintained in the flame. Another advantage of this configuration of the burner is that the large particles will attain the highest, and hence the longest, path, since the path of the smaller particles will to a greater extent than is the case for the large ones be deflected by the primary air which is injected via the outer annular primary air nozzle which is parallel to the main axis of the burner. Hence it will be possible to achieve a more uniform combustion of all particles, regardless of their size. It will be possible to change the path of the particles by altering the velocity or direction of injection.
In principle, the means for changing the flow direction of the fuel may be made up of any suitable means.
In one embodiment of the invention the means for changing the flow direction of the fuel which is introduced via at least one of the additional ducts in the central part of the burner comprises an injection duct which is located at the outlet point of the duct in question in immediate extension hereof, with its centreline forming an angle relative to the main axis of the burner. It is preferred that the injection duct is located so that it points upward in relation to the main axis of the burner at an angle between 1° and 25°, preferentially between 5° and 15° and most preferentially between 7° and 10°. It is further preferred that the lowest point of the outlet of the injection duct is located at a level above the upper part of the pipes of the duct in question. The injection duct may in a special embodiment have an oval cross-section or may otherwise be configured so that the height/width ratio is less than 1. If this is the case, the injection velocity may be varied either by changing the cross-sectional area of the injection duct or by changing the airflow rate which is injected simultaneously with the fuel.
In a second embodiment of the invention, the fuel is introduced in parallel to the main axis of the burner. In this embodiment of the invention the means for changing the flow direction of the fuel which is introduced via at least one of the additional ducts in the central part of the burner comprises an air duct, the outlet of which is located immediately at or at least partially enclosing the duct in question in such a way that the centre of gravity of the outlet cross-section of the air duct is displaced in relation to the centre of gravity of the outlet cross-section of the duct in question. In this embodiment according to the invention, the change in the flow direction of the fuel is effected according to a method which involves that the cross-section of the outlet, or in other words the flow-through area of the air duct outlet is not uniformly distributed across the outlet of the fuel duct in question, entailing also that the quantity of air flowing through the air duct outlet is not uniformly distributed across the circumference of the fuel duct outlet in question. Since the greatest movement quantity of the air will occur in the area or areas of the air duct outlet where the highest air passage rates occur, the airflow in this area or these areas will physically impact the fuel so that this flow direction is changed in direction toward this area or these areas. This second embodiment of the invention may be combined with the aforementioned first embodiment.
In a third embodiment of the invention the fuel is also introduced in parallel to the main axis of the burner. In this third embodiment of the invention the means for changing the flow direction of the fuel which is introduced via at least one of the additional ducts in the central part of the burner comprises a separate air duct, the outlet of which is located immediately at or at least partially enclosing the duct in question, and forming an angle relative to the main axis of the burner. In this embodiment the flow direction of the fuel is changed according to a method whereby the air being injected via the separate air duct forces the fuel in a different direction determined as a function of the angle formed by the air duct in relation to the main axis of the burner. It is preferred that the air duct is fitted so that it points upward relative to the main axis of the burner at an angle of between 8° and 80°, preferentially between 35° and 60°. In this embodiment the direction and velocity of injection will be changed by varying the airflow rate. This third embodiment of the invention may be combined with one or both of the embodiments described above.
The duct 4a, 4 may be configured with an outlet cross-section which forms an angle which is different from 90° relative to the centreline through the duct. Such a configuration can be used to effect a change in the direction of the fuel stream exclusively or in combination with the above-mentioned embodiments. The invention will now be described in further details with reference to the drawing, being diagrammatical, and where
Fig. 1 shows a first embodiment of the burner according to the invention,
Fig. 2 shows a second embodiment of the burner according to the invention, and
Fig. 3 shows a third embodiment of the burner according to the invention.
The Figs. 1-3 show front views as well as sectional views of three different embodiments of the burner according to the invention, and they all comprise two substantially concentric ducts 1 and 2 for conveying primary air which are parallel to the main axis Ba, and a herewith concentric duct 3 for pneumatic conveyance of coal dust and a central part 10 which comprises a duct 4 for conveying solid alternative fuel, and a number of additional ducts or pipes 6, 7 and 8 for ignition gas burner, oil burner and gas burner, respectively. The burners shown in Figs. 2 and 3 also comprise an air duct 5 which encloses the duct 4.
According to the first embodiment of the invention which is shown in Fig. 1 the burner comprises an introduction duct 4a which is fitted in extension of the duct 4 for conveying solid alternative fuel. The introduction duct 4a is arranged so that it points upward relative to the main axis of the burner at an angle α of approximately 8° relative to its centreline. As previously mentioned, the injection velocity of the fuel can be varied by changing the cross-sectional area of the introduction duct 4a or by varying the airflow rate which is injected simultaneously with the fuel. According to the second embodiment of the invention which is shown in Fig. 2, the burner comprises, as mentioned, an air duct 5, the outlet of which is located so that it encloses the duct 4 for conveying solid alternative fuel. In this embodiment, the air duct 5 is arranged so that the centre of gravity of the outlet cross-section of the air duct 5 is displaced upwards relative to the centre of gravity of the outlet cross- section of the duct 4. Hence the largest quantity of air will flow through the upper part of the air duct 5, thereby impacting the fuel stream in upward direction, hence changing the flow of direction of the fuel in the upward direction. This is due to the fact that the movement quantity of the air in the shown embodiment will be greatest in the upper area of the outlet of the air duct 5. As mentioned in the introduction, this second embodiment of the invention may be combined with the first embodiment described above, although this is not shown in the drawing.
According to the third embodiment of the invention, which is shown in Fig. 3, the burner comprises, as mentioned, an air duct 5 the outlet of which is located so that it encloses the duct 4 for conveying solid alternative fuel. In the shown embodiment the air duct 5 is arranged so that it points upwards, forming an angle β of approximately 65° relative to the main axis of the burner. This will cause the flow direction of the fuel to be changed in the upward direction due to the fact that the airflow being injected via the air duct 5 will force the fuel in the upward direction. As previously mentioned, the direction and velocity of injection can be changed by varying the airflow rate. This third embodiment of the invention may as previously mentioned be combined with one or both of the aforementioned embodiments.

Claims

Patent claims
1. A burner for introducing solid, liquid or gaseous fuel to a burning zone of a kiln, such as a rotary kiln for manufacturing cement clinker or the like, said burner comprising a number of substantially concentric ducts (1, 2, 3), which are parallel to the main axis (B3) of the burner, for conveying fuel and primary air to nozzle openings, and a number of additional ducts (4, 6, 7, 8) for conveying solid, fluid or gaseous fuel to separate nozzle openings, with said additional ducts being located in the central part of the burner (10), characterized in that the burner comprises means (4a, 5) for changing the flow direction of the fuel which is introduced via at least one of the additional ducts in the central part (10) of the burner, relative to the main axis B3 of the burner, at least partially in an ascending direction.
2. A burner according to claim 1, characterized in that the means for changing the flow direction of the fuel being introduced via at least one of the additional ducts in the central part of the burner, comprises an introduction duct (4a) which is located at the outlet end of the duct in question in immediate extension hereof, with its centreline forming an angle relative to the main axis (B3) of the burner.
3. A burner according to claim 2, characterized in that the introduction duct (4a) is arranged so that it points upward relative to the main axis (B3) of the burner at an angle between 1° and 25°, preferentially between 5° and 15° and most preferentially between 7° and 10°.
4. A burner according to claim 1, characterized in that the means for changing the flow direction of the fuel which is introduced via at least one of the additional ducts in the central part of the burner, comprises an air duct (5) the outlet of which is located immediately at or at least partially enclosing the duct in question in such a way that the centre of gravity of the outlet cross-section of the air duct (5) is displaced in relation to the centre of gravity of the outlet cross-section of the duct in question.
5. A burner according to claims 2 or 3, characterized in that the means further comprises an air duct (5), the outlet of which is located immediately at or at least partially enclosing the duct (4a) in such a way that the point of gravity of the outlet cross-section of the air duct (5) is displaced in relation to the centre of gravity of the outlet cross-section of the duct (4a).
6. A burner according to claim 1, characterized in that the means for changing the flow direction of the fuel which is introduced via at least one of the additional ducts in the central part of the burner comprises a separate air duct (5), the outlet of which is immediately at or at least partially enclosing the duct in question, and forming an angle relative to the main axis (B3) of the burner.
7. A burner according to claim 6, characterized in that the air duct (5) is arranged so that it points upward relative to the main axis of the burner at an angle between 8° and 80°, preferentially between 35° and 60°.
8. A burner according to the claims 2 or 3, characterized in that the means further comprises a separate air duct (5), the outlet of which is immediately at or at least partially enclosing the duct in question, and forming an angle relative to the main axis (B3) of the burner.
9. A burner according to claim 8, characterized in that the air duct (5) is located so that it points upward relative to the main axis at an angle between 8° and 80°, preferentially between 35° and 60°.
10. A burner according to claim 5, characterized in that the air duct (5), having an outlet immediately at or at least partially enclosing the duct (4a), forms an angle relative to the main axis (B3) of the burner.
PCT/IB2007/054281 2006-11-29 2007-10-22 Burner with means for changing the direction of fuel flow Ceased WO2008065554A1 (en)

Priority Applications (10)

Application Number Priority Date Filing Date Title
US12/513,901 US20100003625A1 (en) 2006-11-29 2007-10-22 Burner with means for changing the direction of fuel flow
CN2007800435162A CN101542204B (en) 2006-11-29 2007-10-22 Burner with means for changing the direction of fuel flow
AU2007326900A AU2007326900B2 (en) 2006-11-29 2007-10-22 Burner with means for changing the direction of fuel flow
MX2009005411A MX2009005411A (en) 2006-11-29 2007-10-22 Burner with means for changing the direction of fuel flow.
JP2009538807A JP5394247B2 (en) 2006-11-29 2007-10-22 Combustor with means for changing the direction of fuel flow
UAA200904626A UA97963C2 (en) 2006-11-29 2007-10-22 Burner for introduction of solid, liquid or gaseous fuel to burning zone of a kiln
CA 2667921 CA2667921C (en) 2006-11-29 2007-10-22 Burner with means for changing the direction of fuel flow
EP07826814.1A EP2087285A4 (en) 2006-11-29 2007-10-22 Burner with means for changing the direction of fuel flow
BRPI0719644-0A2A BRPI0719644A2 (en) 2006-11-29 2007-10-22 BURNER WITH MEANS TO CHANGE THE FUEL FLOW DIRECTION
EG2009040594A EG25502A (en) 2006-11-29 2009-04-27 Burner with means for changing the direction of fuel flow

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DKPA200601564 2006-11-29
DKPA200601564 2006-11-29

Publications (1)

Publication Number Publication Date
WO2008065554A1 true WO2008065554A1 (en) 2008-06-05

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PCT/IB2007/054281 Ceased WO2008065554A1 (en) 2006-11-29 2007-10-22 Burner with means for changing the direction of fuel flow

Country Status (13)

Country Link
US (1) US20100003625A1 (en)
EP (1) EP2087285A4 (en)
JP (1) JP5394247B2 (en)
CN (1) CN101542204B (en)
AU (1) AU2007326900B2 (en)
BR (1) BRPI0719644A2 (en)
CA (1) CA2667921C (en)
EG (1) EG25502A (en)
MX (1) MX2009005411A (en)
RU (1) RU2437029C2 (en)
UA (1) UA97963C2 (en)
WO (1) WO2008065554A1 (en)
ZA (1) ZA200902956B (en)

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WO2010122529A1 (en) * 2009-04-24 2010-10-28 Flsmidth A/S A burner
WO2012084575A3 (en) * 2010-12-22 2012-08-16 Thyssenkrupp Polysius Ag Tubular burner and method for operating a tubular burner
EP2719948A1 (en) * 2012-10-11 2014-04-16 Linde Aktiengesellschaft Burner
WO2014058381A1 (en) * 2012-10-11 2014-04-17 Ecomb Ab (Publ) Supply device for a combustion chamber
EP2775203A1 (en) * 2013-03-08 2014-09-10 Messer Austria GmbH Multi-fuel burner and method for heating an oven

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CA2667921C (en) 2015-04-21
RU2437029C2 (en) 2011-12-20
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UA97963C2 (en) 2012-04-10
EG25502A (en) 2012-01-22
JP5394247B2 (en) 2014-01-22
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MX2009005411A (en) 2009-06-01
ZA200902956B (en) 2010-07-28

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