CN105546531B - A kind of combustor - Google Patents

A kind of combustor Download PDF

Info

Publication number
CN105546531B
CN105546531B CN201610073156.1A CN201610073156A CN105546531B CN 105546531 B CN105546531 B CN 105546531B CN 201610073156 A CN201610073156 A CN 201610073156A CN 105546531 B CN105546531 B CN 105546531B
Authority
CN
China
Prior art keywords
fuel
fuel nozzle
combustion barrel
nozzle
combustor
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.)
Active
Application number
CN201610073156.1A
Other languages
Chinese (zh)
Other versions
CN105546531A (en
Inventor
杨义和
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.)
Shenzhen Yongyuan Equipment Technology Development Co Ltd
Original Assignee
Shenzhen Yongyuan Equipment Technology Development 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.)
Filing date
Publication date
Application filed by Shenzhen Yongyuan Equipment Technology Development Co Ltd filed Critical Shenzhen Yongyuan Equipment Technology Development Co Ltd
Priority to CN201610073156.1A priority Critical patent/CN105546531B/en
Publication of CN105546531A publication Critical patent/CN105546531A/en
Application granted granted Critical
Publication of CN105546531B publication Critical patent/CN105546531B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/24Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36Details, e.g. burner cooling means, noise reduction means
    • F23D11/38Nozzles; Cleaning devices therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

Two fuel nozzles are at least arranged in combustor provided by the present invention, including combustion barrel, the inner cavity of combustion barrel, and fuel nozzle is respectively positioned on the air intake of combustion barrel, fuel is enable to be uniformly mixed with air.By respective fuel oil pump feed, fuel is pumped into fuel nozzle by petrolift by cartridge to be sprayed each fuel nozzle outward.By presetting, the fuel ejected in each fuel nozzle can mutually cross the angle of fuel nozzle installation.It can be easier to realize starting in combustor ignition operation, as long as wherein there is a fuel nozzle to realize igniting, it will be able to which related others fuel nozzle works together, and improves the success rate of igniting.And the fuel ejected in fuel nozzle can mutually cross, fuel nozzle ejects flame when normal operation, forms high-temperature region, and the fuel for not being able to achieve completely burned in a fuel nozzle can be ejected on the flame of another fuel nozzle, it is ignited by another fuel nozzle, to realize completely burned.

Description

A kind of combustor
Technical field
The present invention relates to fuel heat generating device technical fields, concretely relate to a kind of combustor.
Background technique
Combustor is a kind of heating plant using fuel combustion, converts thermal energy for the chemical energy of fuel.Combustor benefit Air is quickly sucked with by turbine, is mixed and burned with the fuel sprayed in the nozzle of fuel, outwardly discharges heat.Make With in the process, it is not high that traditional combustor lights rate in igniting, it is sometimes desirable to repeat sparking for several times could normal combustion, and In burning, fuel injection is unstable, is also easy to that flame-out phenomenon occurs.In addition, big to flame injection due to needing to continue when burning Measure fuel, fuel at a high speed enter flame in, it is understood that there may be part of fuel can not completely burned the phenomenon that, cause waste of fuel.
Therefore, for those skilled in the art, a kind of starting ignition fast and stable how is designed, while guaranteeing to fire Complete combustor is burnt, is the current technical issues that need to address.
Summary of the invention
In order to solve the above technical problems, the present invention provides a kind of combustor, including combustion barrel, the burning tube inner chamber Two fuel nozzles are at least arranged in air intake, and the fuel nozzle passes through cartridge respectively and is connected to respective petrolift;It is described The direction and at an acute angle, the combustion that the fuel nozzle ejects into the angle of the combustion barrel air-flow that fuel nozzle sprays fuel Material can mutually cross.
Optionally, the end that each fuel nozzle connects the cartridge, which is respectively fixedly installed, is able to detect the combustion Expect nozzle whether the detection electric eye of normal ignition, the detection electric eye controls the petrolift and igniter by feedback effect Working condition.
Optionally, burning web is also fixedly mounted in the combustion barrel, the fuel of the fuel nozzle injection can touch The burning web.
Optionally, the burning web is the round high temperature titanium net that can be covered with the combustion barrel cross section.
It optionally, further include being set to bottom of shell, the mounting flange with strip waist hole.
Optionally, the fuel nozzle is high pressure atomizing nozzle, also sets up the steady flame device of eddy flow air distribution in the combustion barrel.
Optionally, temperature sensor and pressure sensor are also set up in the combustion barrel, for fuel described in feedback regulation The supply of pump.
Combustor provided by the present invention includes combustion barrel, and two fuel nozzles are at least arranged in the inner cavity of combustion barrel, Fuel nozzle is respectively positioned on the air intake of combustion barrel, and fuel is enable to be uniformly mixed with air.Each fuel nozzle is by respective Fuel oil pump feed, fuel is pumped into fuel nozzle by petrolift by cartridge to be sprayed outward.The angle of fuel nozzle installation By presetting, the fuel ejected in each fuel nozzle can mutually cross.
Due to being at least provided with two fuel nozzles, can be easier to realize starting in combustor ignition operation, As long as wherein there is a fuel nozzle to realize igniting, it will be able to which related others fuel nozzle works together, therefore greatly improves The success rate of igniting.And the fuel ejected in fuel nozzle can mutually cross, fuel nozzle ejects when normal operation Flame forms high-temperature region, and the fuel for not being able to achieve completely burned in a fuel nozzle can be ejected into the fire of another fuel nozzle It on flame, is ignited by another fuel nozzle, to realize completely burned, and more cluster flames converge at one jointly, can reach Higher temperature is conducive to fuel completely burned.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this Some embodiments of invention for those of ordinary skill in the art without creative efforts, can be with It obtains other drawings based on these drawings.
Fig. 1 is the axis geodesic structure figure of combustor provided by the invention.
Wherein:
Combustion barrel 1, petrolift 2, cartridge 21, igniter 3, casing 4.
Specific embodiment
Core of the invention is to provide a kind of combustor, ignition success rate height, and can make fuel completely burned.
In order to make those skilled in the art more fully understand technical solution of the present invention, below in conjunction with attached drawing and specifically Embodiment combustor provided by the invention is described in detail.
As shown in Figure 1, the structural schematic diagram of the combustor provided for the present invention.Combustor in the present invention, including burning Cylinder 1, combustion barrel 1 is cylindrical, and turbine can be passed through air thereto.In the inner cavity of combustion barrel 1, two fuel are at least set Nozzle, fuel nozzle are located at the air intake of combustion barrel 1, enter in combustion barrel 1 from the fuel sprayed in fuel nozzle, mixed with air It closes.The airflow direction that fuel nozzle sprays the direction of fuel and enters combustion barrel 1 has certain angle, and angle is acute angle, combustion Expect that the one-component of emission direction is identical as air motion direction.Each fuel nozzle has a set of independent fuel supply system System, each fuel nozzle passes through cartridge 21 respectively and is connected to corresponding petrolift 2, by petrolift 2 to fuel nozzle Middle pumping fuel.Fuel nozzle is fixedly installed in combustion barrel 1, and the angle of each fuel nozzle corresponds to each other setting, makes difference Fuel in fuel nozzle can mutually cross.
Two or more fuel nozzles are accordingly also equipped with the igniter of identical quantity, each fuel spray of lighting a fire every time Mouth is attempted to start, as long as there is a completion igniting at this time, other related fuel nozzles of the flame ejected ignite together.One The probability that igniter can not ignite is higher, and the probability that two or more igniters can not ignite simultaneously will be greatly reduced, To improve the success rate of igniting.Combustor enters normal operating conditions, the fuel energy in each fuel nozzle after lighting Enough injections mutually cross, the fuel that a fuel nozzle sprays can not completely burned when utilizing, can be sprayed on another fuel nozzle, It is lighted by the thermal-flame of another fuel nozzle, to realize that full combustion utilizes.Multiply flame crosses jointly, can make combustion barrel Higher temperature is formed in 1, higher temperature can also promote burning complete.Under normal circumstances, as long as there is two groups of fuel nozzle phases It mutually crosses, another is ignited by one of them, relative to the combustion system of one flame, can more efficiently utilize combustion Material.
A preferred technical solution is provided in the present invention, that is, two fuel nozzles are set and petrolift 2, cartridge 21 are adopted With copper pipe, petrolift 2 and cartridge 21 are exposed to outside, are able to bear high temperature in a certain range.
Further, it being also correspondingly arranged on detection electric eye in the present invention, a detection electric eye is respectively arranged in each fuel nozzle, Detection electric eye is located at one end that fuel nozzle connects cartridge 21, for detect fuel nozzle whether normal ignition, and by signal It transmits and feedback effect is to petrolift 2 and igniter 3, control the working condition of petrolift 2 and igniter 3.When loss of ignition or Extinguish suddenly in operation, petrolift 2 locks automatically, and stopping continues to supply fuel;In ignition phase, if lighted a fire successfully, control Igniter 3 processed stops igniting, and burned flame continues to ignite fuel.Two or more detection electric eyes can be more accurately The working condition for measuring fuel nozzle, provides more accurate data-signal.
The utilization rate of fuel when in order to further increase burning, is also fixedly installed with burning web, burning web in combustion barrel 1 Positioned at the open end of fuel nozzle, fuel injection goes out to touch burning web, and burning web is by high temp fire in normal work The heating of flame keeps very high temperature, and a high-temperature region is formed in combustion barrel 1.Under mutual ignition condition still not by The part of fuel of full utilization can be ejected on burning web, heated and lighted again by the burning web of high temperature, to further increase combustion Expect the degree of burning.Burning web may be provided at the mutual intersection of fuel, may also set up in closer to exit, by it is secondary ignite with It ignites and separates three times.
Specifically, lasting high temperature can be born when burning web use, selects heat-resisting material, preferably may be configured as height Warm titanium net.It certainly, can also be first with other materials with similar quality.
It needs to be fixed when combustor is installed, the bottom of casing 4 is provided with mounting flange, in order to finely tune installation The waist hole of strip is arranged in the position of flange on mounting flange, and the part of 4 or more casing can be made sliding along the direction of waist hole Dynamic, when installation, only needs that combustor is fixed on fire door by flange.
Specifically, the fuel nozzle selected in the present invention is high pressure atomizing nozzle, and eddy flow air distribution is also set up in combustion barrel 1 Steady flame device.
Temperature sensor and pressure sensor are also set up in combustion barrel 1, for providing feedback to petrolift 2, adjust fuel The number of supply.Large and small fire is automatically adjusted according to the load variations of heat power equipment, while adjusting the supply of combustion air, is protected Card burning is complete, it is reliable to run smoothly, while saving the energy.
During installation first by flange asbestos pad on combustor, combustion barrel 1 is protruded into burner hearth, position is right after adjusting Mounting flange is fixed on furnace body by quasi- screwhole position.After the position of burner hearth is protruded into confirmation, bolt everywhere is locked, guarantees combustion Burning machine firmly installs.
Combustor of the invention is ignited by the way that the opposite fuel nozzle mutual cooperation of multiple angles is arranged, on the one hand can Improve igniting success rate, on the other hand also can mutually light a fire, make cannot clean-burning fuel completely burned, carry out secondary benefit With.In addition, being additionally provided with burning web, a high-temperature region is formed in the case where not hindering normally to divulge information, if there are also not yet complete The fuel of complete utilization, by can also be lighted utilization when this high-temperature region again, realization is lighted a fire three times.These structures can play Combustion-supporting effect promotes fuel availability, avoids wasting, and saves cost.
The foregoing description of the disclosed embodiments enables those skilled in the art to implement or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, as defined herein General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, this hair It is bright to be not intended to be limited to the embodiments shown herein, and be to fit to and the principles and novel features disclosed herein phase Consistent widest scope.

Claims (6)

1. a kind of combustor, including combustion barrel (1), which is characterized in that the air intake of combustion barrel (1) inner cavity is at least arranged two A fuel nozzle, the fuel nozzle pass through cartridge (21) respectively and are connected to respective petrolift (2), the fuel nozzle pair The igniter of identical quantity is set with answering;The fuel nozzle sprays the direction of fuel and enters the combustion barrel (1) air-flow Angle it is at an acute angle, the fuel that each fuel nozzle ejects can mutually cross;
Burning web is also fixedly mounted in the combustion barrel (1), the fuel of the fuel nozzle injection can touch the burning Net.
2. the combustor according to claim 1, which is characterized in that each fuel nozzle connects the cartridge (21) end be respectively fixedly installed be able to detect the fuel nozzle whether the detection electric eye of normal ignition, the detection electric eye The working condition of the petrolift (2) and igniter (3) is controlled by feedback effect.
3. combustor according to claim 2, which is characterized in that the burning web is can be by the combustion barrel cross section The round high temperature titanium net being covered with.
4. combustor according to any one of claims 1 to 3, which is characterized in that further include be set to casing (4) bottom, Mounting flange with strip waist hole.
5. combustor according to claim 4, which is characterized in that the fuel nozzle is high pressure atomizing nozzle, the combustion It burns in cylinder (1) and also sets up the steady flame device of eddy flow air distribution.
6. combustor according to claim 4, which is characterized in that also set up in the combustion barrel (1) temperature sensor and Pressure sensor, the supply for petrolift (2) described in feedback regulation.
CN201610073156.1A 2016-02-02 2016-02-02 A kind of combustor Active CN105546531B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610073156.1A CN105546531B (en) 2016-02-02 2016-02-02 A kind of combustor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610073156.1A CN105546531B (en) 2016-02-02 2016-02-02 A kind of combustor

Publications (2)

Publication Number Publication Date
CN105546531A CN105546531A (en) 2016-05-04
CN105546531B true CN105546531B (en) 2019-05-24

Family

ID=55825913

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610073156.1A Active CN105546531B (en) 2016-02-02 2016-02-02 A kind of combustor

Country Status (1)

Country Link
CN (1) CN105546531B (en)

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2797783B2 (en) * 1991-11-08 1998-09-17 松下電器産業株式会社 Liquid fuel combustion device
JP3533302B2 (en) * 1996-12-29 2004-05-31 東京瓦斯株式会社 Combustion equipment
CN201137938Y (en) * 2007-11-30 2008-10-22 陈伟雄 Fuel liquid combustion machine
CN201297644Y (en) * 2008-10-24 2009-08-26 孙明路 Alcohol group combustor as well as alcohol group combustion nozzles and pneumatic shear knife thereof
CN202274484U (en) * 2011-09-08 2012-06-13 钮铜山 Methanol combustion engine
CN102954487B (en) * 2011-12-02 2015-06-24 浙江永源机电制造有限公司 Burning system
CN204100559U (en) * 2014-09-02 2015-01-14 李良君 A kind of alcohol-group fuel water heater
CN204301050U (en) * 2014-11-25 2015-04-29 李坤桦 A kind of combustor
CN205480975U (en) * 2016-02-02 2016-08-17 深圳涌源设备科技开发有限公司 Combustion engine

Also Published As

Publication number Publication date
CN105546531A (en) 2016-05-04

Similar Documents

Publication Publication Date Title
JPH01212819A (en) Fuel nozzle
CN106257138B (en) Combustion device with controllable output heat source temperature
US20120260664A1 (en) Fuel injector arrangement having an igniter
CN205480975U (en) Combustion engine
US6971235B2 (en) Evaporative burner
CN104595927B (en) Low heat value of gas turbine fuel combustion chamber
US5391075A (en) Multi-fuel burner
CN107883405B (en) Vaporizer tube combustor quick start structure, method, small aero
CN110594743B (en) Mixed fuel burner for burning low-heat-value waste gas by using high-heat-value waste liquid
CN105546531B (en) A kind of combustor
CN208794414U (en) Burner and gas-cooker with it
EP3531797B1 (en) Infrared radiant heater
CN215637143U (en) Staged combustion low-nitrogen burner
CN213208226U (en) Novel gas heating boiler
CN106032907B (en) Blast furnace gas burner igniter
JP6497098B2 (en) Ignition control device for pressure spray pot burner
CN103900088B (en) A kind of kitchen range air blast burner
RU2229062C2 (en) Hot-bulb ignition burner
CN204648230U (en) Be applicable to the burner using low heat value fuel oil and pluralities of fuel oil
JP5507720B1 (en) Automatic ignition type oil burner
CN208606259U (en) A kind of infra-red radiation gas heating positive pressure generator using hot surface ignitor
KR0132199Y1 (en) Combustion apparatus of hot air blower
JP2000274608A (en) Burner
JPH0335944Y2 (en)
CN206989269U (en) A kind of energy-conserving and environment-protective cooking stove

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant