CN106482103A - The igniter burner that integrated igniting is examined with ion fire - Google Patents
The igniter burner that integrated igniting is examined with ion fire Download PDFInfo
- Publication number
- CN106482103A CN106482103A CN201610946023.0A CN201610946023A CN106482103A CN 106482103 A CN106482103 A CN 106482103A CN 201610946023 A CN201610946023 A CN 201610946023A CN 106482103 A CN106482103 A CN 106482103A
- Authority
- CN
- China
- Prior art keywords
- compressed air
- igniter
- igniter burner
- aperture
- connecting pipe
- 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
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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
- F23D14/20—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
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/48—Nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23Q—IGNITION; EXTINGUISHING-DEVICES
- F23Q13/00—Igniters not otherwise provided for
- F23Q13/02—Igniters not otherwise provided for using gas burners, e.g. gas pokers
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Other Investigation Or Analysis Of Materials By Electrical Means (AREA)
Abstract
The present invention provides the igniter burner of a kind of integrated igniting and ion fire inspection, including：Compressed air cavity, its one end is provided with the first aperture and the second aperture, and the compressed air interface being located at this end side surface；It is fixed on the combustion gas connecting pipe in compressed air cell body by the first aperture, including connecting pipe body, be connected and be located at the external combustion gas interface of compressed air cell with its one end, and be connected with its other end and be located at the nozzle in compressed air cell body；Igniter in compressed air cell body is fixed on by the second aperture, including electrode tube, igniting and detecting electrode, and spark plug；And it is fixed on reducer in combustion gas connecting pipe and igniter respectively by the first fixing hole and the second fixing hole, reducer is provided with multiple throttle orifices.The integrated igniting being provided by the present invention and the igniter burner of ion fire inspection, solve existing igniter burner complex structure, and using the unstable problem of process moderate heat inspection.
Description
Technical field
The present invention relates to heat storage type combustion field, the igniter burner that more particularly to a kind of integrated igniting is examined with ion fire.
Background technology
Developing rapidly with HTAC, regenerative combustion technology seems more in the effect of combustion field
Important, igniter burner arises at the historic moment therewith, is widely used in heat storage type combustion field.
Although however, ionic flame detection and burning torch are integrated together by traditional igniter burner, letter to a certain extent
Change the structure of igniter burner, but but require preferable flame forms when carrying out fire defector, to various mass of medium
And sky gas proportion and flow velocity have higher requirements, flare up fire otherwise cannot be detected, can not carry out burning stable in time
Mouth igniting and fire defector, the judgement that the combustion case of burner work is made mistake, the safe operation of impact equipment.
In consideration of it, being necessary the igniter burner providing a kind of new integrated igniting and ion fire inspection in order to solve this problem.
Content of the invention
The shortcoming of prior art in view of the above, it is an object of the invention to provide a kind of integrated igniting and ion fire inspection
Igniter burner, for solving the problems, such as that conventional point burns that mouth structure is complicated and fire defector is unstable.
For achieving the above object and other related purposes, the present invention provides a kind of integrated igniting and the point of ion fire inspection to burn
Mouth, described igniter burner includes：
Compressed air cavity, one end of described compressed air cavity is provided with the first aperture and the second aperture, and is located at institute
State the compressed air interface of this end side surface；
Combustion gas connecting pipe in described compressed air cell body is fixed on by the first aperture, described combustion gas connecting pipe includes leading
Pressure pipe body, is connected and is located at the external combustion gas of described compressed air cell by the first aperture with described connecting pipe body one end
Interface, and be connected with the described connecting pipe body other end and be located at the nozzle in described compressed air cell body；
Igniter in described compressed air cell body is fixed on by the second aperture, described igniter includes electrode
Pipe, is connected with described electrode tube by the second aperture and positioned at the external spark plug of described compressed air cell, and with described electricity
Igniting and detecting electrode that the pole pipe other end connects and is located in described compressed air cell body；
And be fixed on described combustion gas connecting pipe and igniter by the first fixing hole and the second fixing hole respectively
Reducer, described reducer is provided with some throttle orifices.
Preferably, described reducer and the distance of described nozzle are 50～80mm.
Preferably, the area of described some throttle orifices accounts for the 1/4～1/3 of whole reducer area.
Preferably, the quantity of described some throttle orifices is 4～6.
Preferably, described reducer and throttle orifice are circle.
Preferably, a diameter of 3～5mm of described throttle orifice.
Preferably, described igniter also includes the high temperature insulator on described electrode tube.
Preferably, described nozzle is radial porous nozzle arrangements.
Preferably, described nozzle is heat-resisting steel part or ceramic member.
Preferably, described igniter burner is additionally provided with adpting flange.
As described above, the integrated igniting of the present invention and the igniter burner of ion fire inspection, have the advantages that：The present invention
Described igniter burner structure is simple, and by improving to the reducer of igniter burner of the present invention, substantially increases
The fire defector stability of igniter burner of the present invention is so that the fire defector stability of described igniter burner is up to 99.9%.
Brief description
Fig. 1 is shown as the structural representation of igniter burner of the present invention.
Fig. 2 is shown as the structural representation of igniter burner compressed air cavity of the present invention.
Fig. 3 is shown as the structural representation of igniter burner combustion gas airway of the present invention.
Fig. 4 is shown as the structural representation of igniter burner igniter of the present invention.
Fig. 5 is shown as the structural representation of igniter burner reducer of the present invention.
Component label instructions
1 compressed air cavity
11 first apertures
12 second apertures
13 compressed air interfaces
2 combustion gas connecting pipes
21 connecting pipe bodys
22 combustion gas interface
23 nozzles
3 igniters
31 electrode tubes
32 spark plugs
33 igniting and detecting electrode
34 high temperature insulator
4 reducers
41 first fixing holes
42 second fixing holes
43 throttle orifices
Specific embodiment
Hereinafter embodiments of the present invention are illustrated by particular specific embodiment, those skilled in the art can be by this explanation
Content disclosed by book understands other advantages and effect of the present invention easily.
Refer to Fig. 1 to Fig. 5.It should be clear that structure depicted in this specification institute accompanying drawings, ratio, size etc., all only in order to
Content disclosed in cooperation description, so that those skilled in the art understands and reads, being not limited to the present invention can be real
The qualificationss applied, therefore do not have technical essential meaning, the tune of the modification of any structure, the change of proportionate relationship or size
Whole, under not affecting present invention effect that can be generated by and the purpose that can reach, all should still fall in disclosed skill
In the range of art content obtains and can cover.Meanwhile, in this specification cited as " on ", D score, "left", "right", " middle " and
The term of " one " etc., is merely convenient to understanding of narration, and is not used to limit the enforceable scope of the present invention, its relativeness
It is altered or modified, under no essence change technology contents, when being also considered as the enforceable category of the present invention.
As shown in Figures 1 to 5, the present invention provides the igniter burner of a kind of integrated igniting and ion fire inspection, and described point is burnt
Mouth includes：
Compressed air cavity 1, one end of described compressed air cavity 1 is provided with the first aperture 11 and the second aperture 12, and
Compressed air interface 13 positioned at this end side surface described；
Combustion gas connecting pipe 2 in described compressed air cavity 1, described combustion gas connecting pipe 2 are fixed on by the first aperture 11
Including connecting pipe body 21, it is connected with described connecting pipe body 21 one end by the first aperture 11 and is located at described compressed air
Combustion gas interface 22 outside cavity 1, and be connected with described connecting pipe body 21 other end and be located at described compressed air cavity 1
Interior nozzle 23；
Igniter 3 in described compressed air cavity 1 is fixed on by the second aperture 12, described igniter 3 includes
Electrode tube 31, is connected with described electrode tube 31 by the second aperture 12 and is located at the spark plug outside described compressed air cavity 1
32, and be connected with described electrode tube 31 other end and the igniting in described compressed air cavity 1 and detecting electrode 33；
And respectively described combustion gas connecting pipe 2 and igniter are fixed on by the first fixing hole 41 and the second fixing hole 42
Reducer 4 on 3, described reducer 4 is provided with some throttle orifices 43.
Wherein, described igniter burner is additionally provided with adpting flange.
It should be noted that described adpting flange is fixed on described compressed air cavity 1, and pass through described adpting flange
Realize the fixation of described igniter burner.
Specifically, described compressed air interface 13 arrives the distance of described nozzle 23 less than described combustion gas interface 22 to described spray
The distance of mouth 23, and it is located at the length of the igniter 3 within described compressed air cavity 1 less than positioned at described compressed air
The length of the internal described combustion gas connecting pipe 2 of cavity 1.
Specifically, described nozzle 23 is radial porous nozzle arrangements, in case non-return is fiery.
Specifically, described nozzle 23 is heat-resisting steel part or ceramic member.Preferably, in the present embodiment, described nozzle 23 is
Ceramic member；Certainly, in other embodiments, described nozzle 23 can also be heat-resisting steel part.
It should be noted that by nozzle 23 is set to heat-resisting steel part or ceramic member it is ensured that nozzle 23 can be resisted
The erosion of high temperature, the service life of prolonging nozzle 23.
Specifically, described igniter 3 also includes the high temperature insulator 34 on described electrode tube, to realize to electrode
The high temperature protection of pipe 31.
Specifically, described reducer 4 and the distance of described nozzle 23 are 50～80mm, and described some throttle orifices 43
Area accounts for the 1/4～1/3 of whole reducer 4 area.
Preferably, in the present embodiment, described reducer 4 and the distance of described nozzle 23 are 65mm；Certainly, other real
Apply in example, described reducer 4 can also be 50mm, 60mm, 70mm or 80mm etc. with the distance of described nozzle 23.
Preferably, in the present embodiment, the area of described some throttle orifices 43 accounts for the 7/24 of whole reducer 4 area；When
So, in other embodiments, the area that the area of described some throttle orifices 43 accounts for whole reducer 4 can also be 1/4 or 1/3.
It should be noted that by the distance of described reducer and described nozzle is set to 50～80mm, and if described
The area of dry throttle orifice accounts for the 1/4～1/3 of whole reducer area；Air and combustion gas is made while reducing air velocity
Ratio, closer to complete combusted proportion, both can guarantee that air was burnt completely with combustion gas, will not cross senior general's combustion gas because of air velocity again
Take away combustion zone, lead to not carry out fire defector, and also improve the adaptability to various media.
Specifically, the quantity of described some throttle orifices 43 is 4～6.Preferably, in the present embodiment, described throttle orifice
43 quantity is 5；Certainly, in other embodiments, the quantity of described throttle orifice 43 can also be 4 or 6.
Preferably, in the present embodiment, described reducer 4 and throttle orifice 43 are circle；Certainly, in other embodiments
In, described throttle orifice 43 can also be other shapes.
Specifically, a diameter of 3～5mm of described throttle orifice 43.Preferably, in the present embodiment, described throttle orifice 43
A diameter of 4mm；Certainly, in other embodiments, the diameter of described throttle orifice 43 can also be 3mm, 3.5mm, 4.5mm or 5mm
Deng.
In sum, the integrated igniting of the present invention and the igniter burner of ion fire inspection, have the advantages that：The present invention
Described igniter burner structure is simple, and by improving to the reducer of igniter burner of the present invention, substantially increases
The fire defector stability of igniter burner of the present invention is so that the fire defector stability of described igniter burner is up to 99.9%.
So, the present invention effectively overcomes various shortcoming of the prior art and has high industrial utilization.
Above-described embodiment only principle of the illustrative present invention and its effect, not for the restriction present invention.Any ripe
The personage knowing this technology all can carry out modifications and changes without prejudice under the spirit and the scope of the present invention to above-described embodiment.Cause
This, those of ordinary skill in the art is complete with institute under technological thought without departing from disclosed spirit such as
All equivalent modifications becoming or change, must be covered by the claim of the present invention.
Claims (10)
1. a kind of integrated igniting and the igniter burner of ion fire inspection are it is characterised in that described igniter burner includes：
Compressed air cavity, one end of described compressed air cavity is provided with the first aperture and the second aperture, and is located at described being somebody's turn to do
The compressed air interface of end side surface；
Combustion gas connecting pipe in described compressed air cell body is fixed on by the first aperture, described combustion gas connecting pipe includes connecting pipe
Body, is connected and is located at the external combustion gas interface of described compressed air cell by the first aperture with described connecting pipe body one end,
And be connected and the nozzle in described compressed air cell body with the described connecting pipe body other end；
Igniter in described compressed air cell body is fixed on by the second aperture, described igniter includes electrode tube, leads to
Cross the second aperture to be connected with described electrode tube and be located at the external spark plug of described compressed air cell, and with described electrode tube
Igniting and detecting electrode that the other end connects and is located in described compressed air cell body；
And respectively the throttling on described combustion gas connecting pipe and igniter is fixed on by the first fixing hole and the second fixing hole
Device, described reducer is provided with some throttle orifices.
2. the inspection of integrated igniting according to claim 1 and ion fire igniter burner it is characterised in that described reducer with
The distance of described nozzle is 50～80mm.
3. the igniter burner of integrated igniting according to claim 1 and ion fire inspection is it is characterised in that described some throttlings
The area in hole accounts for the 1/4～1/3 of whole reducer area.
4. the igniter burner of integrated igniting according to claim 1 and ion fire inspection is it is characterised in that described some throttlings
The quantity in hole is 4～6.
5. the inspection of integrated igniting according to claim 1 and ion fire igniter burner it is characterised in that described reducer with
And throttle orifice is circle.
6. the igniter burner of integrated igniting according to claim 5 and ion fire inspection is it is characterised in that described throttle orifice
A diameter of 3～5mm.
7. the igniter burner of integrated igniting according to claim 1 and ion fire inspection is it is characterised in that described igniter
Also include the high temperature insulator on described electrode tube.
8. integrated igniting according to claim 1 and the igniter burner of ion fire inspection are it is characterised in that described nozzle is footpath
To jet rose structure.
9. integrated igniting according to claim 1 and the igniter burner of ion fire inspection are it is characterised in that described nozzle is resistance to
Hot steel part or ceramic member.
10. integrated igniting according to claim 1 and the igniter burner of ion fire inspection are it is characterised in that described point is burnt
Adpting flange is additionally provided with mouth.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610946023.0A CN106482103B (en) | 2016-10-26 | 2016-10-26 | Ignition burner integrating ignition and ion fire detection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610946023.0A CN106482103B (en) | 2016-10-26 | 2016-10-26 | Ignition burner integrating ignition and ion fire detection |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106482103A true CN106482103A (en) | 2017-03-08 |
| CN106482103B CN106482103B (en) | 2020-06-19 |
Family
ID=58273005
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610946023.0A Active CN106482103B (en) | 2016-10-26 | 2016-10-26 | Ignition burner integrating ignition and ion fire detection |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106482103B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113654082A (en) * | 2021-08-31 | 2021-11-16 | 宝钢工程技术集团有限公司 | Constant-power low-nitrogen oxide ignition gun and using method thereof |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1068510A (en) * | 1996-08-27 | 1998-03-10 | Nippon Furnace Kogyo Kaisha Ltd | Fuel injection gun |
| CN203177176U (en) * | 2013-01-14 | 2013-09-04 | 大连昌荣炉业股份有限公司 | Igniting burner with automatic igniting detection function |
| CN204285464U (en) * | 2014-12-08 | 2015-04-22 | 武汉钢铁(集团)公司 | A kind of radiation pipe burner tip burning torch |
| CN206176374U (en) * | 2016-10-26 | 2017-05-17 | 上海安可科技股份有限公司 | Ignition burner that integration point fire and ion fire were examined |
-
2016
- 2016-10-26 CN CN201610946023.0A patent/CN106482103B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1068510A (en) * | 1996-08-27 | 1998-03-10 | Nippon Furnace Kogyo Kaisha Ltd | Fuel injection gun |
| CN203177176U (en) * | 2013-01-14 | 2013-09-04 | 大连昌荣炉业股份有限公司 | Igniting burner with automatic igniting detection function |
| CN204285464U (en) * | 2014-12-08 | 2015-04-22 | 武汉钢铁(集团)公司 | A kind of radiation pipe burner tip burning torch |
| CN206176374U (en) * | 2016-10-26 | 2017-05-17 | 上海安可科技股份有限公司 | Ignition burner that integration point fire and ion fire were examined |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113654082A (en) * | 2021-08-31 | 2021-11-16 | 宝钢工程技术集团有限公司 | Constant-power low-nitrogen oxide ignition gun and using method thereof |
| CN113654082B (en) * | 2021-08-31 | 2023-11-17 | 宝钢工程技术集团有限公司 | Constant-power low-nitrogen oxide ignition gun and use method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106482103B (en) | 2020-06-19 |
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Denomination of invention: Ignition burner with integrated ignition and ion ignition detection Effective date of registration: 20220830 Granted publication date: 20200619 Pledgee: Bank of Nanjing Limited by Share Ltd. Shanghai branch Pledgor: SHANGHAI ANCHOR TECHNOLOGY Co.,Ltd. Registration number: Y2022310000215 |