CN104696959A - Burner and igniter thereof - Google Patents

Burner and igniter thereof Download PDF

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Publication number
CN104696959A
CN104696959A CN201510095666.4A CN201510095666A CN104696959A CN 104696959 A CN104696959 A CN 104696959A CN 201510095666 A CN201510095666 A CN 201510095666A CN 104696959 A CN104696959 A CN 104696959A
Authority
CN
China
Prior art keywords
air
introducing device
air duct
pressure air
igniter
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.)
Granted
Application number
CN201510095666.4A
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Chinese (zh)
Other versions
CN104696959B (en
Inventor
姚康明
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.)
Million Xuan Neng Science And Technology Ltds
Original Assignee
Million Xuan Neng Science And Technology Ltds
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 Million Xuan Neng Science And Technology Ltds filed Critical Million Xuan Neng Science And Technology Ltds
Priority to CN201510095666.4A priority Critical patent/CN104696959B/en
Publication of CN104696959A publication Critical patent/CN104696959A/en
Priority to HK15106890.1A priority patent/HK1206412A1/en
Priority to PCT/CN2016/075411 priority patent/WO2016138866A1/en
Application granted granted Critical
Publication of CN104696959B publication Critical patent/CN104696959B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/20Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22Non-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
    • F23D14/24Non-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 at least one of the fluids being submitted to a swirling motion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23QIGNITION; EXTINGUISHING-DEVICES
    • F23Q13/00Igniters not otherwise provided for
    • F23Q13/02Igniters not otherwise provided for using gas burners, e.g. gas pokers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/34Burners specially adapted for use with means for pressurising the gaseous fuel or the combustion air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2203/00Gaseous fuel burners

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lighters Containing Fuel (AREA)
  • Gas Burners (AREA)
  • Regulation And Control Of Combustion (AREA)

Abstract

The invention relates to an igniter and a burner comprising the same. The igniter comprises a pressure air introducing device (1) and an ignition channel (2) penetrating through the pressure air introducing device (1), wherein a concave platform area (3) is arranged at the top end of the pressure air introducing device (1), and a plurality of air channels (6) surrounding the center of the pressure air introducing device (1) are formed in the bottom end of the pressure air introducing device (1); the axes of the air channels (6) incline to the same direction, so as to introduce compressed air into the bottom of the concave platform area (3) to form upwards-rotating air flow; the inclined direction of the axes of the air channels (6) is consistent with the direction of gas entering the concave platform area (3) from the gas channel, so that the gas is introduced into the low pressure area (3) of upwards-rotating air flow to fully mix the air and the gas.

Description

A kind of burner and igniter thereof
Technical field
The present invention relates to a kind of stove and accessory for dining room or kitchen and gas burner system, more particularly, relate to a kind of igniter and comprise the burner of this igniter.
Background technology
Existing burner igniter, cannot mix combustion gas and air fully usually.Often cause incomplete combustion, heat to pass many, the problem such as combustion efficiency is poor and carbonomonoxide concentration is high due to combustion gas and air undercompounding.Therefore, need one can fully air mixture and air, thus make can clean-burning igniter in combustion zone.
Summary of the invention
The technical problem to be solved in the present invention is, combustion gas and air cannot be mixed sufficient defect by the igniter for prior art, provides one can fully air mixture and air, thus make can clean-burning igniter in combustion zone.
The technical solution adopted for the present invention to solve the technical problems is: construct a kind of igniter, comprise the ignition channel of pressure air introducing device and through described pressure air introducing device, the top of described pressure air introducing device arranges concave station district, bottom arranges the air duct at multiple center around described pressure air introducing device, the axis of described multiple air duct tilts compressed air to be incorporated into the bottom in described concave station district thus the rotary air stream formed upwards all in the same direction, the axis incline direction of described multiple air duct is consistent with the approach axis of the combustion gas being entered described concave station district by blast tube, thus the low-pressure area of rotary air stream upwards described in combustion gas being introduced is fully to mix described air and described combustion gas.
In igniter of the present invention, described multiple air duct is formed around the different annulus of the diameter at the center of described pressure air introducing device.
In igniter of the present invention, the axis of described multiple air duct is along tilting clockwise or counterclockwise.
In igniter of the present invention, the diameter of described multiple air duct is homogeneous.
In igniter of the present invention, described pressure air introducing device comprises cylindrical upper portion and cylinder bottom, the diameter of described cylindrical upper portion is greater than the diameter of described cylinder bottom, described concave station district is arranged on the top of described cylindrical upper portion, and described multiple air duct is arranged on the bottom of described cylindrical upper portion.
In igniter of the present invention, described ignition channel is the stepped cylindrical hole of downward increasing diameter; The active combustion control combustion gas of setting based on burner and the safety device of air supply in described ignition channel.
The present invention solves another technical scheme that its technical problem adopts: construct a kind of burner, comprise gas combustion apparatus, pressure air room, igniter and combustion zone, described gas combustion apparatus comprises fuel chamber, blast tube and gas outlet, described igniter comprises the ignition channel of pressure air introducing device and through described pressure air introducing device, igniter is established in described ignition channel, the top of described pressure air introducing device arranges concave station district, bottom arranges the air duct at multiple center around described pressure air introducing device, the axis of described multiple air duct tilts compressed air to be incorporated into the bottom in described concave station district from described pressure air room thus the rotary air stream formed upwards all in the same direction, the axis incline direction of described multiple air duct is consistent with the approach axis of the combustion gas being entered described concave station district by described blast tube from described fuel chamber through described gas outlet, thus the low-pressure area of rotary air stream upwards described in combustion gas being introduced is fully to mix described air and described combustion gas, well-mixed empty combustion gas enters described combustion zone through empty blast tube.
In burner of the present invention, described multiple air duct is formed around the different annulus of the diameter at the center of described pressure air introducing device, and the axis edge of described multiple air duct tilts clockwise or counterclockwise and the diameter of described multiple air duct is homogeneous.
In burner of the present invention, described ignition channel is the stepped cylindrical hole of downward increasing diameter; The active combustion control combustion gas of setting based on burner and the safety device of air supply in described ignition channel.
In burner of the present invention, described pressure air introducing device comprises cylindrical upper portion and cylinder bottom, the diameter of described cylindrical upper portion is greater than the diameter of described cylinder bottom, described concave station district is arranged on the top of described cylindrical upper portion, and described multiple air duct is arranged on the bottom of described cylindrical upper portion.
Implement igniter of the present invention and burner, there is following beneficial effect: generation rotates up air-flow to the pressure air that is arranged so that of pressure air introducing device in concave station district, thus low-pressure area is formed centrally in this swirling eddy, and then combustion gas is introduced, thus make air and combustion gas mixing more abundant, improve the efficiency of combustion of gaseous mixture, reduce further the emission index of the waste gas such as carbon monoxide.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the invention will be further described, in accompanying drawing:
Fig. 1 is the structural representation of the first embodiment of igniter of the present invention;
Fig. 2 is the structural representation of the air duct of the igniter shown in Fig. 1;
Fig. 3 is the structural representation of the first embodiment of burner of the present invention.
Detailed description of the invention
As shown in Figure 1, igniter of the present invention comprises the ignition channel 2 of pressure air introducing device 1 and through described pressure air introducing device 1.In ignition channel 2, igniter and/or safety device can be set.Described pressure air introducing device 1 comprises cylindrical upper portion 4 and cylinder bottom 5, and the diameter of described cylindrical upper portion 4 is greater than the diameter of described cylinder bottom 5.The top of described cylindrical upper portion 4 arranges concave station district 3.The degree of depth in described concave station district 3 is about 1/2 of the thickness of described cylindrical upper portion 4.The bottom of described cylindrical upper portion 4 arranges the air duct 6 at multiple center around described pressure air introducing device 1.The axis of described multiple air duct 6 tilts compressed air to be incorporated into the bottom in described concave station district 3 thus the rotary air stream formed upwards all in the same direction.The axis incline direction of described multiple air duct 6 is consistent with the approach axis of the combustion gas being entered described concave station district 3 by blast tube, thus the low-pressure area of rotary air stream upwards described in combustion gas being introduced is fully to mix described air and described combustion gas.
Fig. 2 is the structural representation of the air duct of the igniter shown in Fig. 1.As shown in Figure 2,6 air ducts 6 are arranged to circular around the center of described pressure air introducing device 1, and the bottom running through described cylindrical upper portion 4 arrives described concave station district 3.The axis of described 6 air ducts 6 all becomes 45 degree with vertical axis and diameter is homogeneous.Described 6 air ducts 6 tilt along clockwise direction.Now, the setting combustion gas by blast tube being arranged to enter along clockwise direction to coordinate this air duct 6 is needed.
Due to pressure air enter from these 6 air channels 6 time, the air-flow that turns clockwise upwards will be produced, thus be formed centrally low-pressure area in this swirling eddy upwards.When combustion gas is arranged to enter along clockwise direction equally, due to the existence of this low-pressure area, combustion gas will be inhaled into this low-pressure area, thus rotate up mixing clockwise together with pressure air, so make air and combustion gas mixing more abundant.Further, this strand rotates mixed airflow simultaneously can the igniter of protection setting in ignition channel 2 and/or safety device (such as thermoelectricity occasionally fire defector rod), reduces high temperature to its loss.
Those skilled in the art know, in other embodiments of the invention, can arrange the air duct 6 of other quantity, such as 3, four, five, seven or more.Many group air ducts 6 also can be set, often organize air duct and formed around the different annulus of the diameter at the center of described pressure air introducing device 1.The diameter of described multiple air duct 6 can be the same or different.The axis of described air duct 6 can become 20-70 degree by vertical axis.
In another embodiment of the invention, can arrange 8 described air ducts 6 in the counterclockwise direction Relative vertical axis become 60 degree of inclinations.Now, the setting combustion gas by blast tube being arranged to enter in the counterclockwise direction to coordinate this air duct 6 is needed.Due to pressure air enter from these 8 air channels 6 time, will produce upwards be rotated counterclockwise air-flow, thus be formed centrally low-pressure area in this swirling eddy upwards.When combustion gas is arranged to enter in the counterclockwise direction equally, due to the existence of this low-pressure area, combustion gas will be inhaled into this low-pressure area, thus rotate up mixing counterclockwise together with pressure air, so make air and combustion gas mixing more abundant.
In other embodiments of the invention, described pressure air introducing device 1 also can be arranged to other shapes, such as square column type, triangle cylindricality etc.Now, the top of described pressure air introducing device 1 arranges concave station district 3, bottom arranges the air duct 6 at multiple center around described pressure air introducing device 1, the axis of described multiple air duct 6 tilts compressed air to be incorporated into the bottom in described concave station district 3 from described pressure air room thus the rotary air stream formed upwards all in the same direction, the axis incline direction of described multiple air duct 6 is consistent with the approach axis of combustion gas, thus the low-pressure area of rotary air stream upwards described in combustion gas being introduced is fully to mix described air and described combustion gas, well-mixed empty combustion gas enters combustion zone through empty blast tube 12.
Further as shown in Figure 1, described ignition channel 2 is be made up of stepped cylindrical hole that is identical, that diametrically increase progressively down, four centers.One, the bottom of largest diameter cylindrical hole inwall can arrange internal thread 21 with fixed ignition device and/or safety device.
Implement igniter of the present invention, wherein pressure air introducing device be arranged so that pressure air concave station district produce rotate up air-flow, thus low-pressure area is formed centrally in this swirling eddy, and then combustion gas is introduced, thus make air and combustion gas mixing more abundant, improve the efficiency of combustion of gaseous mixture, reduce further the emission index of the waste gas such as carbon monoxide.Further, this strand rotates mixed airflow simultaneously can the igniter of protection setting in ignition channel and/or safety device (such as thermoelectricity occasionally fire defector rod), reduces high temperature to its loss.
Fig. 3 is the structural representation of the first embodiment of burner of the present invention.As shown in Figure 3, burner of the present invention, comprises gas combustion apparatus, pressure air room, igniter and combustion zone.Described gas combustion apparatus comprises fuel chamber 7, blast tube 8 and gas outlet 9, and described igniter comprises the ignition channel 2 of pressure air introducing device 1 and through described pressure air introducing device 1.The safety device 11 burner being set in described ignition channel 2 and supplying based on active combustion control combustion gas and the air of burner.This safety device 11 can be thermocouple or flame monitor.Described pressure air introducing device 1 comprises cylindrical upper portion 4 and cylinder bottom 5, and the diameter of described cylindrical upper portion 4 is greater than the diameter of described cylinder bottom 5.The top of described cylindrical upper portion 4 arranges concave station district 3.The degree of depth in described concave station district 3 is about 1/5 of the thickness of described cylindrical upper portion 4.The bottom of described cylindrical upper portion 4 arranges the air duct 6 at multiple center around described pressure air introducing device 1.The axis of described multiple air duct 6 tilts compressed air to be incorporated into the bottom in described concave station district 3 thus the rotary air stream formed upwards all in the same direction.Be stored in combustion gas in fuel chamber 7 through blast tube 8, be input to the top in concave station district 3 from gas outlet 9.Now, the approach axis of combustion gas is consistent with the axis incline direction of described multiple air duct 6, such as, is clockwise or is counterclockwise.Now, due to pressure air enter from air channels 6 time, will produce upwards clockwise or be rotated counterclockwise air-flow, thus be formed centrally low-pressure area in this swirling eddy upwards.When combustion gas is arranged to enter clockwise or counterclockwise equally, due to the existence of this low-pressure area, combustion gas will be inhaled into this low-pressure area, thus rotate up mixing clockwise or counterclockwise together with pressure air, and then form air fuel gas mixed air vessel 13 above concave station district 3.In air fuel gas mixed air vessel 13, air and combustion gas mixing more abundant.This air fuel gas mixed air vessel 13 is made up of upper cylindrical cavity and lower cylindrical cavity.On this, the diameter of cylindrical cavity is less, and the diameter of lower cylindrical cavity is larger.Empty blast tube 12 is communicated with the upper cylindrical cavity of air fuel gas mixed air vessel 13, and the diameter of empty blast tube 12 is less than the diameter of the upper cylindrical cavity of air fuel gas mixed air vessel 13.Diameter due to air fuel gas mixed air vessel 13 times large upper and lower and empty blast tubes 12 is less than the design of the diameter of cylindrical cavity on this, make portion of air and combustion gas mixing gas can not be discharged to combustion zone in time, but continue to rotate mixing in air fuel gas mixed air vessel 13, thus further ensure that air and combustion gas mixing more abundant, improve the efficiency of combustion of gaseous mixture, reduce further the emission index of the waste gas such as carbon monoxide.Further, this strand rotates mixed airflow simultaneously can the igniter of protection setting in ignition channel and/or safety device (such as thermoelectricity occasionally fire defector rod), reduces high temperature to its loss.
Those skilled in the art know, the igniter in the present embodiment can based on the embodiment manufacture of the igniter shown in Fig. 1-2.Those skilled in the art know further, can adopt any design as known in the art and parts for the miscellaneous part in burner or design.Based on instruction of the present invention, those skilled in the art can adopt parts as known in the art and design, construct burner of the present invention, are just not repeated at this.
Implement burner of the present invention, there is following beneficial effect: generation rotates up air-flow to the pressure air that is arranged so that of pressure air introducing device in concave station district, thus low-pressure area is formed centrally in this swirling eddy, and then combustion gas is introduced, thus make air and combustion gas mixing more abundant, improve the efficiency of combustion of gaseous mixture, reduce further the emission index of the waste gas such as carbon monoxide.
Although the present invention is described by specific embodiment, it will be appreciated by those skilled in the art that, without departing from the present invention, various conversion can also be carried out and be equal to substituting to the present invention.Therefore, the present invention is not limited to disclosed specific embodiment, and should comprise the whole embodiments fallen within the scope of the claims in the present invention.

Claims (10)

1. an igniter, it is characterized in that, comprise the ignition channel (2) of pressure air introducing device (1) and through described pressure air introducing device (1), the top of described pressure air introducing device (1) arranges concave station district (3), bottom arranges the air duct (6) at multiple center around described pressure air introducing device (1), the axis of described multiple air duct (6) tilts compressed air to be incorporated into the bottom of described concave station district (3) thus the rotary air stream formed upwards all in the same direction, the axis incline direction of described multiple air duct (6) is consistent with the approach axis of the combustion gas being entered described concave station district (3) by blast tube, thus the low-pressure area of rotary air stream upwards described in combustion gas being introduced is fully to mix described air and described combustion gas.
2. igniter according to claim 1, is characterized in that, described multiple air duct (6) is formed around the different annulus of the diameter at the center of described pressure air introducing device (1).
3. igniter according to claim 2, is characterized in that, the axis of described multiple air duct (6) is along tilting clockwise or counterclockwise.
4. igniter according to claim 2, is characterized in that, the diameter of described multiple air duct (6) is homogeneous.
5. according to the igniter in claim 1-4 described in any one, it is characterized in that, described pressure air introducing device (1) comprises cylindrical upper portion (4) and cylinder bottom (5), the diameter of described cylindrical upper portion (4) is greater than the diameter of described cylinder bottom (5), described concave station district (3) is arranged on the top of described cylindrical upper portion (4), and described multiple air duct (6) is arranged on the bottom of described cylindrical upper portion (4).
6. igniter according to claim 1, it is characterized in that, the stepped cylindrical hole that described ignition channel (2) is downward increasing diameter, the active combustion control combustion gas of setting based on burner and the safety device (11) of air supply in described ignition channel (2).
7. a burner, comprise gas combustion apparatus, pressure air room, igniter and combustion zone, it is characterized in that, described gas combustion apparatus comprises fuel chamber (7), blast tube (8) and gas outlet (9), described igniter comprises the ignition channel (2) of pressure air introducing device (1) and through described pressure air introducing device (1), the top of described pressure air introducing device (1) arranges concave station district (3), bottom arranges the air duct (6) at multiple center around described pressure air introducing device (1), the axis of described multiple air duct (6) tilts compressed air to be incorporated into the bottom of described concave station district (3) from described pressure air room thus the rotary air stream formed upwards all in the same direction, the axis incline direction of described multiple air duct (6) is consistent with the approach axis of the combustion gas being entered described concave station district (3) by described blast tube (8) from described fuel chamber (7) through described gas outlet (9), thus the low-pressure area of rotary air stream upwards described in combustion gas being introduced is fully to mix described air and described combustion gas, well-mixed empty combustion gas enters described combustion zone through empty blast tube (12).
8. burner according to claim 7, it is characterized in that, described multiple air duct (6) is formed around the different annulus of the diameter at the center of described pressure air introducing device (1), and the axis edge of described multiple air duct (6) tilts clockwise or counterclockwise and the diameter of described multiple air duct (6) is homogeneous.
9. burner according to claim 7, is characterized in that, the stepped cylindrical hole that described ignition channel (2) is downward increasing diameter; The active combustion control combustion gas of setting based on burner and the safety device (11) of air supply in described ignition channel (2).
10. according to the burner in claim 7-9 described in any one, it is characterized in that, described pressure air introducing device (1) comprises cylindrical upper portion (4) and cylinder bottom (5), the diameter of described cylindrical upper portion (4) is greater than the diameter of described cylinder bottom (5), described concave station district (3) is arranged on the top of described cylindrical upper portion (4), and described multiple air duct (6) is arranged on the bottom of described cylindrical upper portion (4).
CN201510095666.4A 2015-03-03 2015-03-03 A kind of burner and its lighter Expired - Fee Related CN104696959B (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CN201510095666.4A CN104696959B (en) 2015-03-03 2015-03-03 A kind of burner and its lighter
HK15106890.1A HK1206412A1 (en) 2015-03-03 2015-07-20 A burner and its ignition device
PCT/CN2016/075411 WO2016138866A1 (en) 2015-03-03 2016-03-03 Burner and igniter thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510095666.4A CN104696959B (en) 2015-03-03 2015-03-03 A kind of burner and its lighter

Publications (2)

Publication Number Publication Date
CN104696959A true CN104696959A (en) 2015-06-10
CN104696959B CN104696959B (en) 2017-03-29

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CN201510095666.4A Expired - Fee Related CN104696959B (en) 2015-03-03 2015-03-03 A kind of burner and its lighter

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CN (1) CN104696959B (en)
HK (1) HK1206412A1 (en)
WO (1) WO2016138866A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016138866A1 (en) * 2015-03-03 2016-09-09 兆轩能科技有限公司 Burner and igniter thereof

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111911912B (en) * 2020-07-31 2023-07-11 辛胜杰 Solid fuel column, burner and solid fuel combustion method

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EP0619457B1 (en) * 1993-04-08 1997-10-08 Asea Brown Boveri Ag Premix burner
CN101526233A (en) * 2009-03-17 2009-09-09 胡端志 Safe and energy-saving gas stove
CN201599795U (en) * 2009-12-13 2010-10-06 康金英 Top combustion hot-blast stove burner
CN201819218U (en) * 2010-10-14 2011-05-04 河北钢铁股份有限公司承德分公司 Horizontal internal mixing type ceramics burner used for top combustion stove
CN103062769A (en) * 2013-01-14 2013-04-24 兆轩能科技有限公司 Combustor
CN204513395U (en) * 2015-03-03 2015-07-29 兆轩能科技有限公司 A kind of igniter and comprise the burner of this igniter

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FR2545196B1 (en) * 1983-04-29 1985-08-16 Gaz De France BURNER FOR GAS FUELS WITH INCORPORATED IGNITION AND SAFETY SYSTEMS
CN2533391Y (en) * 2002-03-21 2003-01-29 许东山 Mother fire ignition structure for enclosed blast furnace
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CN101245914A (en) * 2008-03-18 2008-08-20 上海复济节能技术有限公司 Premixed high-efficiency energy-saving environment protection combustor with ignition and flame-out protection device
CN104696959B (en) * 2015-03-03 2017-03-29 兆轩能科技有限公司 A kind of burner and its lighter

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0619457B1 (en) * 1993-04-08 1997-10-08 Asea Brown Boveri Ag Premix burner
CN101526233A (en) * 2009-03-17 2009-09-09 胡端志 Safe and energy-saving gas stove
CN201599795U (en) * 2009-12-13 2010-10-06 康金英 Top combustion hot-blast stove burner
CN201819218U (en) * 2010-10-14 2011-05-04 河北钢铁股份有限公司承德分公司 Horizontal internal mixing type ceramics burner used for top combustion stove
CN103062769A (en) * 2013-01-14 2013-04-24 兆轩能科技有限公司 Combustor
CN204513395U (en) * 2015-03-03 2015-07-29 兆轩能科技有限公司 A kind of igniter and comprise the burner of this igniter

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016138866A1 (en) * 2015-03-03 2016-09-09 兆轩能科技有限公司 Burner and igniter thereof

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CN104696959B (en) 2017-03-29
WO2016138866A1 (en) 2016-09-09
HK1206412A1 (en) 2016-01-08

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