CN103175202A - Non-premix type start-up burner - Google Patents

Non-premix type start-up burner Download PDF

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Publication number
CN103175202A
CN103175202A CN201110437017XA CN201110437017A CN103175202A CN 103175202 A CN103175202 A CN 103175202A CN 201110437017X A CN201110437017X A CN 201110437017XA CN 201110437017 A CN201110437017 A CN 201110437017A CN 103175202 A CN103175202 A CN 103175202A
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CN
China
Prior art keywords
nozzle
oxidant
incendiary agent
burner
fuel
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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.)
Pending
Application number
CN201110437017XA
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Chinese (zh)
Inventor
于晓亮
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.)
Xian Aerospace Yuanzheng Fluid Control Co Ltd
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Xian Aerospace Yuanzheng Fluid Control Co Ltd
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.)
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Application filed by Xian Aerospace Yuanzheng Fluid Control Co Ltd filed Critical Xian Aerospace Yuanzheng Fluid Control Co Ltd
Priority to CN201110437017XA priority Critical patent/CN103175202A/en
Publication of CN103175202A publication Critical patent/CN103175202A/en
Pending legal-status Critical Current

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Abstract

The invention relates to a non-premix type start-up burner. A head jet piece is provided with an oxidant nozzle and a fuel agent nozzle, the oxidant nozzle is connected with an oxidant channel, the fuel agent nozzle is connected with a fuel agent channel, and an atomizer is arranged between the fuel agent nozzle and the fuel agent channel. According to the non-premix type start-up burner, the mode that fuel agents are atomized independently is used, the fuel agents can be jetted out in an atomizing mode under an oxidant condition or a non-oxidant condition, and once the oxidants are jetted out, the two media can be mixed to achieve burning. Thus, the demands to the pressures of the fuel agents and the oxidants and sequential control of the aspect of system control are greatly lowered, the adjusting range of mixing ratio of the oxidants and the fuel agents is greatly widened, fire cutoff is avoided, the cost caused by repeating to drive a car because of supply wave of the media due to system reasons is avoided, the problem that an original premix burner is easy to temper in driving of the car and shutting down of the car is fundamentally solved, and damage to the heat jet piece by high-temperature flame is avoided.

Description

Non-premixed startup burner
Technical field
The present invention relates to a kind of startup burner, relate in particular to a kind of non-premixed startup burner.
Background technology
China is the country that an oil starvation weak breath, coal resources enrich relatively, and coal methyl alcohol processed, coal liquefaction, coal preparing natural gas, olefin hydrocarbon making by coal etc. account for critical role in China's energy sustainable use.The Development of Coal chemical industry be unable to do without the preparation of synthesis gas.The pressurized gasification of coal is the necessary means of making synthesis gas.System's core component in the equipment just and igniting of gasification furnace goes into operation.
It is very high that the design principle of existing startup burner is controlled requirement to system, and existing goes into operation is not easy successfully, the defective that wastes time and energy.Be mainly because existing product has adopted the premix mode in the nozzle structure body, that is to say that incendiary agent and oxidant two media did not just mix before flowing out the nozzle structure body, both burn with mixture mode one superhigh speed ejection nozzle structure body.The atomizing of incendiary agent need to by the high speed impact of oxidant, be controlled the pressure proportioning of incendiary agent and oxidant and propose higher requirement so like this.All run into to some extent in use procedure and control improper or enter the bad problem that startup burner even constantly burns out by tempering of defeating that goes into operation that causes of SECO because of two media pressure.
Summary of the invention
Harsh for the specification requirement that solves existing startup burner existence, as easily to be burned technical problem the invention provides a kind of non-premixed startup burner.
Technical solution of the present invention is:
A kind of non-premixed startup burner, described burner head is provided with head spray part 2, its special character is: described head spray part 2 comprises end plates, oxidant channel 4, incendiary agent passage 5, water-cooling sandwich, described end plates respectively with oxidant channel 4, incendiary agent passage 5, water-cooling sandwich 3 welded seals; The end plates 12 of described head spray part are provided with flame-thrower nozzle, described flame-thrower nozzle comprises eight oxidize nozzles 7 and an incendiary agent nozzle 6, described oxidize nozzle 7 is connected with oxidant channel 4, described incendiary agent nozzle 6 is positioned at the end plates center and is connected with incendiary agent passage 5, is provided with atomizer 9 between described incendiary agent nozzle 6 and incendiary agent passage 5; Described a plurality of oxidize nozzle 7 evenly is arranged on around incendiary agent nozzle 6 and the angle between oxidize nozzle 7 axis and head spray part end plates 12 is 34 degree; Described water-cooling sandwich 3 is logical with the outer loop water.
The present invention has advantages of:
1, utilize incendiary agent independence atomizing type to realize that in oxidant or non-oxidation agent situation, incendiary agent all can spray by atomizing type, in case the oxidant ejection is arranged, two media can mix and realize burning.So greatly simplify the aspect that system controls incendiary agent oxidant stress and sequential have been controlled requirement, greatly widened the adjustable range of oxidant incendiary agent mixing ratio, can cutoff, avoided the cost that repeats to drive due to system's reason medium supply fluctuation.
2, the present invention is by mixing incendiary agent and oxidant after first spray burning agent again, the problem of easy tempering when having solved original premix burner nozzle at all and driving and cut-off.
3, head spray part of the present invention is the integral type structure, and namely oxidize nozzle and incendiary agent nozzle are arranged on same part, and the quality of flame just can guarantee by processing, has avoided so original product repeatedly to load and unload and has caused the problem that flame quality descends.
4, incendiary agent of the present invention and oxidant be separately by the ejection of self nozzle, then passes through certain apart from blending, through just beginning to produce flame after certain blending distance.By cold fluid and mixture, flame and the head spray part head of high temperature are fully isolated like this, avoided the destruction of thermal-flame to head spray part.And the expansion process after cold fluid high-speed ejection head spray part is again a process of cooling in fact, has so just realized the cooling itself of medium to head spray part head itself.So having overcome original burner thermal-flame, the present invention directly is attached to the defective that the burning of head spray part wall causes head spray part easily to destroy.
5, be provided with water-cooling sandwich in head spray part, in addition cooling to the burner outer wall by the turnover of cooling water.Simultaneously, water-cooling sandwich of the present invention only needs to resist the radiant heat from gasification furnace, and needn't consider thermal-flame to the destruction of head, so simple in structure.
Description of drawings
Fig. 1 is the structural representation of the first structure of the present invention:
Fig. 2 is the right view of Fig. 1;
Wherein: 2-head spray part, 3-water-cooling sandwich, 4-oxidant channel, 5-incendiary agent passage, 6-incendiary agent nozzle, 7-oxidize nozzle, the 8-cooling jacket, 9-atomizer, 10-cooling water inlet, the 11-coolant outlet, 12-head spray part end plates, 13-oxidize nozzle exit end face, 14-incendiary agent nozzle exit end face, 21-flame zone, 22-mixed zone, the 23-range of atomization, the 24-booster zone.
The specific embodiment
Be as depicted in figs. 1 and 2 the non-premixed startup burner of the present invention, the burner head is provided with head spray part 2, head spray part comprises end plates, oxidant channel 4, incendiary agent passage 5, water-cooling sandwich 3, end plates respectively with oxidant channel, incendiary agent passage, water-cooling sandwich welded seal; Head spray part end plates 12 are provided with flame-thrower nozzle, and flame-thrower nozzle comprises oxidize nozzle 7 and incendiary agent nozzle 6, and the quantity of incendiary agent nozzle is one; The quantity of oxidize nozzle is eight; Oxidize nozzle is connected with oxidant channel, and the incendiary agent nozzle is connected with the incendiary agent passage, is provided with atomizer 9 between each incendiary agent nozzle and incendiary agent passage; Eight oxidize nozzles evenly are arranged on around the incendiary agent nozzle and the scope of the angle between oxidize nozzle axis and head spray part end plates is 34 degree.The oxidize nozzle outlet just sprays the gas oxidant with the angle that tilts like this, can wholely consist of suitable eddy flow.
In order to prevent from the impact on medium in oxidant channel or incendiary agent passage of the radiant heat of gasification furnace, be provided with water-cooling sandwich in head spray part, be provided with cooling jacket 8 in cooling sandwith layer for increasing the water circulation effect, water-cooling sandwich and outer loop water are logical.
The principle of the invention:
Referring to Fig. 1, the present invention includes the incendiary agent nozzle that is positioned at center ring, the oxidize nozzle that is positioned at outer shroud and outer loop cooling water system.Incendiary agent nozzle ejection by center ring after fuel combustion agent independent atomizing mechanically forms range of atomization 23, the number of incendiary agent nozzle is according to the requirement of actual condition, can be single injector or multiinjector, combustion-supporting gas oxidant sprays at a high speed by the oxidize nozzle of outer shroud, forms booster zone 24.Guaranteed like this if the upstream provide enough incendiary agents press (<2MPa), the incendiary agent that sprays burner has been in spray pattern.Oxidant flows through burner by passage independently, and through oxidize nozzle with ejection at a high speed.Oxidize nozzle number and jet size are also according to the requirement of actual working condition respective change.The incendiary agent oxidant is walked respectively oneself independently runner separately like this, until nozzle structure is external, the incendiary agent of atomizing just meets with oxidant and mixes and forms incendiary agent mist mixed zone 22, and is lighted by outer burning things which may cause a fire disaster, burns, and forms flame zone 21.So not only igniting easily, is not easy again fire extinguishing.And the flame firing point has been realized the cooling itself of fluid to burner away from burner body, has avoided the high temperature destruction of flame to burner.The burner outer wall arranges the cooling duct interlayer, by cooling water to burner wall cooling protection in addition.Outer cooling duct cooling agent can be cooling water or other safe water.

Claims (1)

1. non-premixed startup burner, described burner head is provided with head spray part (2), it is characterized in that: described head spray part (2) comprises end plates, oxidant channel (4), incendiary agent passage (5), water-cooling sandwich, described end plates respectively with oxidant channel (4), incendiary agent passage (5), water-cooling sandwich (3) welded seal; The end plates (12) of described head spray part are provided with flame-thrower nozzle, described flame-thrower nozzle comprises eight oxidize nozzles (7) and an incendiary agent nozzle (6), described oxidize nozzle (7) is connected with oxidant channel (4), described incendiary agent nozzle (6) is positioned at the end plates center and is connected with incendiary agent passage (5), is provided with atomizer (9) between described incendiary agent nozzle (6) and incendiary agent passage (5); Described a plurality of oxidize nozzle (7) evenly be arranged on incendiary agent nozzle (6) on every side and oxidize nozzle (7) axis and head spray part end plates (12) between angle be 34 the degree; Described water-cooling sandwich (3) is logical with the outer loop water.
CN201110437017XA 2011-12-20 2011-12-20 Non-premix type start-up burner Pending CN103175202A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201110437017XA CN103175202A (en) 2011-12-20 2011-12-20 Non-premix type start-up burner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201110437017XA CN103175202A (en) 2011-12-20 2011-12-20 Non-premix type start-up burner

Publications (1)

Publication Number Publication Date
CN103175202A true CN103175202A (en) 2013-06-26

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CN (1) CN103175202A (en)

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3239205A (en) * 1960-02-19 1966-03-08 A R B E D Acieries Reunies De Double lances
US3847564A (en) * 1970-01-23 1974-11-12 Texaco Development Corp Apparatus and process for burning liquid hydrocarbons in a synthesis gas generator
EP0120517A2 (en) * 1983-03-18 1984-10-03 Shell Internationale Researchmaatschappij B.V. Burner and process for the partial combustion of solid fuel
US4775314A (en) * 1985-05-20 1988-10-04 Shell Oil Company Coal gasification burner
EP0640679A1 (en) * 1991-12-23 1995-03-01 Texaco Development Corporation Partial oxidation process and burner with porous tip
CN1121156A (en) * 1994-06-13 1996-04-24 普拉塞尔技术有限公司 Staged combustion for reducing nitrogen oxides
CN2489202Y (en) * 2001-07-10 2002-05-01 陕西杨凌航天节水科技股份有限公司 Burner with water-cooling wall technique of coal-water slurry
CN101098750A (en) * 2005-01-06 2008-01-02 陶氏环球技术公司 Feed nozzle assembly and burner apparatus for gas/liquid reactions
CN101936527A (en) * 2010-09-07 2011-01-05 西安航天远征流体控制股份有限公司 Oil-oxygen burning pre-mixed type starting burner
CN202419645U (en) * 2011-12-20 2012-09-05 西安航天远征流体控制股份有限公司 Non-premixing startup burner

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3239205A (en) * 1960-02-19 1966-03-08 A R B E D Acieries Reunies De Double lances
US3847564A (en) * 1970-01-23 1974-11-12 Texaco Development Corp Apparatus and process for burning liquid hydrocarbons in a synthesis gas generator
EP0120517A2 (en) * 1983-03-18 1984-10-03 Shell Internationale Researchmaatschappij B.V. Burner and process for the partial combustion of solid fuel
US4775314A (en) * 1985-05-20 1988-10-04 Shell Oil Company Coal gasification burner
EP0640679A1 (en) * 1991-12-23 1995-03-01 Texaco Development Corporation Partial oxidation process and burner with porous tip
CN1121156A (en) * 1994-06-13 1996-04-24 普拉塞尔技术有限公司 Staged combustion for reducing nitrogen oxides
CN2489202Y (en) * 2001-07-10 2002-05-01 陕西杨凌航天节水科技股份有限公司 Burner with water-cooling wall technique of coal-water slurry
CN101098750A (en) * 2005-01-06 2008-01-02 陶氏环球技术公司 Feed nozzle assembly and burner apparatus for gas/liquid reactions
CN101936527A (en) * 2010-09-07 2011-01-05 西安航天远征流体控制股份有限公司 Oil-oxygen burning pre-mixed type starting burner
CN202419645U (en) * 2011-12-20 2012-09-05 西安航天远征流体控制股份有限公司 Non-premixing startup burner

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