CN111853771B - Liquid fuel porous medium combustor with cold flame pre-evaporation function - Google Patents
Liquid fuel porous medium combustor with cold flame pre-evaporation function Download PDFInfo
- Publication number
- CN111853771B CN111853771B CN202010734974.8A CN202010734974A CN111853771B CN 111853771 B CN111853771 B CN 111853771B CN 202010734974 A CN202010734974 A CN 202010734974A CN 111853771 B CN111853771 B CN 111853771B
- Authority
- CN
- China
- Prior art keywords
- cold flame
- channel
- combustion chamber
- combustion
- water
- 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.)
- Expired - Fee Related
Links
- 239000007788 liquid Substances 0.000 title claims abstract description 90
- 239000000446 fuel Substances 0.000 title claims abstract description 76
- 238000001704 evaporation Methods 0.000 title claims abstract description 31
- 230000008020 evaporation Effects 0.000 title claims abstract description 28
- 238000002485 combustion reaction Methods 0.000 claims abstract description 136
- 239000003546 flue gas Substances 0.000 claims abstract description 68
- 238000001816 cooling Methods 0.000 claims abstract description 67
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 claims abstract description 64
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 43
- 239000000498 cooling water Substances 0.000 claims abstract description 37
- 238000009413 insulation Methods 0.000 claims abstract description 19
- 239000003344 environmental pollutant Substances 0.000 claims abstract description 15
- 231100000719 pollutant Toxicity 0.000 claims abstract description 15
- 239000007789 gas Substances 0.000 claims description 17
- 238000002347 injection Methods 0.000 claims description 7
- 239000007924 injection Substances 0.000 claims description 7
- 230000000694 effects Effects 0.000 claims description 3
- 238000000034 method Methods 0.000 claims description 3
- 230000006641 stabilisation Effects 0.000 claims description 3
- 238000011105 stabilization Methods 0.000 claims description 3
- 239000006200 vaporizer Substances 0.000 claims description 3
- 239000000779 smoke Substances 0.000 claims 3
- 230000007613 environmental effect Effects 0.000 abstract 1
- IMNFDUFMRHMDMM-UHFFFAOYSA-N N-Heptane Chemical compound CCCCCCC IMNFDUFMRHMDMM-UHFFFAOYSA-N 0.000 description 28
- 239000000463 material Substances 0.000 description 6
- 238000006243 chemical reaction Methods 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 3
- 239000003921 oil Substances 0.000 description 3
- 239000012774 insulation material Substances 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 238000009423 ventilation Methods 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000004964 aerogel Substances 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000010992 reflux Methods 0.000 description 1
- 230000001172 regenerating effect Effects 0.000 description 1
- 238000009877 rendering Methods 0.000 description 1
- 229910052814 silicon oxide Inorganic materials 0.000 description 1
- 150000003384 small molecules Chemical class 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
- F23D11/22—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour the gaseous medium being vaporised fuel, e.g. for a soldering lamp, or other gaseous fuel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
- F23D11/38—Nozzles; Cleaning devices therefor
- F23D11/383—Nozzles; Cleaning devices therefor with swirl means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
- F23D11/44—Preheating devices; Vaporising devices
- F23D11/441—Vaporising devices incorporated with burners
- F23D11/446—Vaporising devices incorporated with burners heated by an auxiliary flame
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Abstract
本发明公开的一种具备冷焰预蒸发的液体燃料多孔介质燃烧器,属于微能源领域。本发明包括压力旋流喷嘴,冷焰气化器固定环,冷却水出口,燃烧室水冷通道,燃烧室壳体,冷却水引流通道,烟气通道水冷通道,冷却水入口,燃烧室绝热层,燃烧段多孔介质,预热段多孔介质,冷焰气化器,冷焰气化器绝热层,空气入口以及燃烧器上盖等。本液体燃料多孔介质燃烧器结合冷焰预蒸发和微燃烧技术,能够提高燃烧器的燃烧效率,降低污染物排放并且具有宽的燃烧器功率调节范围和燃烧当量比范围。用户只需向压力旋流喷嘴供入液体燃料就能获得燃烧产生的能量,具有环保、高效、便携的优点。本发明通过将液态燃料预蒸发进而燃烧产生能量,能够作为微小型设备的能量来源。
The invention discloses a liquid fuel porous medium burner with cold flame pre-evaporation, which belongs to the field of micro-energy. The invention includes a pressure swirl nozzle, a cold flame gasifier fixing ring, a cooling water outlet, a combustion chamber water cooling channel, a combustion chamber shell, a cooling water drainage channel, a flue gas channel water cooling channel, a cooling water inlet, and a combustion chamber thermal insulation layer. Porous medium in combustion section, porous medium in preheating section, cold flame gasifier, insulation layer of cold flame gasifier, air inlet and burner upper cover, etc. The liquid fuel porous media burner combines cold flame pre-evaporation and micro-combustion technology, which can improve the combustion efficiency of the burner, reduce pollutant emissions, and has a wide burner power adjustment range and combustion equivalence ratio range. Users only need to supply liquid fuel to the pressure swirl nozzle to obtain the energy generated by combustion, which has the advantages of environmental protection, high efficiency and portability. The present invention generates energy by pre-evaporating the liquid fuel and then burning it, and can be used as an energy source for micro-miniature equipment.
Description
技术领域technical field
本发明涉及一种具备冷焰预蒸发的液体燃料多孔介质燃烧器,特别涉及一种使用液体燃料且具备预蒸发能力的多孔介质燃烧器,属于微能源领域。The invention relates to a liquid fuel porous medium burner with cold flame pre-evaporation, in particular to a porous medium burner using liquid fuel and having pre-evaporation capability, belonging to the field of micro-energy.
背景技术Background technique
随着科学技术的发展,微型设备加工技术越发成熟,人们对于微型设备也越发关注,同时将液体燃料作为能量来源,具有较之于一般气体燃料易于储存且能量密度大的优势。然而,在微型设备日趋成熟,需求日益扩大的同时,对于其中的电源设备也提出了新的要求,将微型燃烧设备作为电源设备的能量来源是其中的选择之一,同样要求微型燃烧设备具有外形尺寸小、污染物排放低、燃烧的当量比范围宽以及燃烧器功率可调节范围宽等特性。With the development of science and technology, the processing technology of micro-devices has become more and more mature, and people are paying more and more attention to micro-devices. At the same time, using liquid fuel as an energy source has the advantages of easy storage and high energy density compared with general gas fuels. However, while the micro-devices are becoming more mature and the demand is expanding, new requirements are also put forward for the power supply equipment in them. Using the micro-combustion device as the energy source of the power supply device is one of the choices, and the micro-combustion device is also required to have a shape. Small size, low pollutant emissions, wide range of equivalence ratio of combustion and wide adjustable range of burner power.
而目前传统的液体燃料燃烧技术是将液体燃料喷入高温的燃烧室内,利用燃烧室的高温加强液体燃料的蒸发预混,但是由于液体燃料的蒸发和燃烧过程不能很好的分离,不利于液体燃料与空气的预混燃烧,不可避免地造成了液体燃料燃烧不充分,从而产生燃烧装置能量密度低,污染物排放高的问题。此外,液体燃料不充分燃烧产生的固体颗粒很可能阻塞多孔介质,使得多孔介质燃烧器失效。而本发明利用液体燃料的冷焰反应放热,在液体燃料燃烧前预蒸发液体燃料,将液体燃料的蒸发与燃烧过程相互分离,提高燃烧器的燃烧效率。因此,发明一种具备冷焰预蒸发的液体燃料多孔介质燃烧器就变得很有现实意义。The current traditional liquid fuel combustion technology is to inject liquid fuel into a high temperature combustion chamber, and use the high temperature of the combustion chamber to enhance the evaporation and premixing of the liquid fuel. However, because the evaporation and combustion processes of the liquid fuel cannot be well separated, it is not conducive to the liquid The premixed combustion of fuel and air inevitably results in insufficient combustion of liquid fuel, resulting in the problems of low energy density and high pollutant emission of the combustion device. In addition, solid particles from insufficient combustion of the liquid fuel are likely to clog the porous media, rendering the porous media burner ineffective. The present invention utilizes the cold flame reaction heat release of the liquid fuel, pre-evaporates the liquid fuel before the liquid fuel burns, separates the vaporization and combustion processes of the liquid fuel from each other, and improves the combustion efficiency of the burner. Therefore, it becomes very practical to invent a liquid fuel porous media burner with cold flame pre-evaporation.
发明内容SUMMARY OF THE INVENTION
为了解决传统液体燃料燃烧中液体燃料蒸发与燃烧过程不能很好的分离,从而引起的污染物排放高,能量密度低等一系列问题,本发明的目的是提供一种具备冷焰预蒸发的液体燃料多孔介质燃烧器,以液体燃料作为燃烧物质,能量密度显著高于传统微型液体燃烧装置,且污染物排放低。液体燃料能够通过压力旋流喷嘴进液口供入燃烧器中,并且能够通过调节压力旋流喷嘴的供油压力调节燃烧器的燃烧功率,为外界提供能量。In order to solve a series of problems such as high pollutant discharge and low energy density caused by the inability to separate liquid fuel evaporation and combustion process well in traditional liquid fuel combustion, the purpose of the present invention is to provide a liquid with cold flame pre-evaporation The fuel porous media burner uses liquid fuel as the combustion material, the energy density is significantly higher than that of the traditional micro liquid combustion device, and the pollutant emission is low. The liquid fuel can be supplied into the burner through the liquid inlet of the pressure swirl nozzle, and the combustion power of the burner can be adjusted by adjusting the oil supply pressure of the pressure swirl nozzle to provide energy to the outside world.
本发明的目的是通过下述技术方案实现的。The purpose of the present invention is achieved through the following technical solutions.
本发明公开的一种具备冷焰预蒸发的液体燃料多孔介质燃烧器,包括压力旋流喷嘴、喷嘴旋流室进液口、旋流室、喷嘴出口、螺栓、垫圈、螺母、压力旋流喷嘴进液口。还包括冷却水出口、冷焰气化器固定环、燃烧室水冷通道、燃烧室壳体、燃烧室水冷通道壁面、燃烧室水冷通道支撑体、烟气通道连接体、冷却水引流通道、烟气通道水冷通道壁面、烟气通道水冷通道、冷却水入口、烟气通道壁面、烟气通道水冷通道支撑体、燃烧室绝热层、燃烧段多孔介质、预热段多孔介质、冷焰气化器壁面、冷焰气化器、冷焰气化器绝热层、空气入口、燃烧器上盖。The invention discloses a liquid fuel porous medium burner with cold flame pre-evaporation, comprising a pressure swirl nozzle, a nozzle swirl chamber liquid inlet, a swirl chamber, a nozzle outlet, a bolt, a washer, a nut, and a pressure swirl nozzle. liquid inlet. It also includes cooling water outlet, cold flame gasifier fixing ring, combustion chamber water cooling channel, combustion chamber shell, combustion chamber water cooling channel wall surface, combustion chamber water cooling channel support body, flue gas channel connecting body, cooling water drainage channel, flue gas Channel water cooling channel wall surface, flue gas channel water cooling channel, cooling water inlet, flue gas channel wall surface, flue gas channel water cooling channel support body, combustion chamber insulation layer, combustion section porous medium, preheating section porous medium, cold flame gasifier wall surface , Cold flame gasifier, cold flame gasifier insulation layer, air inlet, burner cover.
压力旋流喷嘴包括上端的液体燃料进液和下端的旋流喷射两个部分;上端的液体燃料进液部分设置有压力旋流喷嘴进液口,下端的旋流喷射部分设置有喷嘴旋流室进液口、旋流室以及喷嘴出口;上端的液体燃料进液和下端的旋流喷射两部分通过螺纹相互连接,压力旋流喷嘴再通过螺纹连接到燃烧器上盖上;燃烧器上盖设置有压力旋流喷嘴连接孔,孔内设置用于连接压力旋流喷嘴的内螺纹,同时在燃烧器上盖的侧面对称设置空气入口;燃烧器上盖通过相同的螺栓与燃烧室主体部分连接;燃烧器主体部分为一中通的圆柱体,中间设置冷焰气化器,冷焰气化器通过上下布置的冷焰气化器固定环固定于燃烧室主体中央;冷焰气化器为上端开口,下端封闭的圆筒结构;冷焰气化器四周填充预热段多孔介质和燃烧段多孔介质,所述的预热段多孔介质用于预热来流燃料空气预混气体,提高预混气体的温度,有利于后续燃烧过程降低污染物排放,且有利于预混气体的均匀燃烧;所述的燃烧段多孔介质,主要用于预混气体燃烧和火焰稳定,具有降低污染物排放和有利于预混气体均匀燃烧的作用;燃烧室壳体通过与燃烧室水冷通道壁面连接形成环形的燃烧室水冷通道;燃烧室主体与下端的烟气通道连接体通过相同的螺栓相互连接;烟气通道连接体与烟气通道相连接,烟气通道为一中通的圆柱体;烟气通道壁面与烟气通道水冷通道壁面共同形成中空的烟气通道水冷通道。The pressure swirl nozzle includes two parts: the liquid fuel inlet at the upper end and the swirl injection at the lower end; the liquid fuel inlet part at the upper end is provided with a pressure swirl nozzle inlet, and the swirl injection part at the lower end is provided with a nozzle swirl chamber The liquid inlet, the swirl chamber and the nozzle outlet; the liquid fuel inlet at the upper end and the swirl jet at the lower end are connected to each other by threads, and the pressure swirl nozzle is then connected to the upper cover of the burner through threads; the upper cover of the burner is provided with There is a connection hole for the pressure swirl nozzle, and the inner thread for connecting the pressure swirl nozzle is arranged in the hole, and the air inlet is symmetrically arranged on the side of the upper cover of the burner; the upper cover of the burner is connected with the main part of the combustion chamber through the same bolt; The main part of the burner is a cylinder with a central passage, and a cold flame gasifier is arranged in the middle. The cold flame gasifier is fixed in the center of the main body of the combustion chamber through the cold flame gasifier fixing ring arranged up and down; the cold flame gasifier is the upper end. A cylindrical structure with an open end and a closed lower end; the cold flame gasifier is filled with porous media in the preheating section and porous media in the combustion section. The temperature of the gas is conducive to the subsequent combustion process to reduce pollutant emissions, and is conducive to the uniform combustion of the premixed gas; the porous medium in the combustion section is mainly used for the combustion of the premixed gas and flame stabilization, which has the advantages of reducing pollutant emissions and having a certain effect. It is beneficial to the uniform combustion of the premixed gas; the combustion chamber shell is connected with the wall surface of the combustion chamber water cooling channel to form an annular combustion chamber water cooling channel; the combustion chamber main body and the lower end of the flue gas channel connecting body are connected to each other by the same bolts; the flue gas channel The connecting body is connected with the flue gas channel, and the flue gas channel is a centrally connected cylinder; the wall surface of the flue gas channel and the wall surface of the water-cooling channel of the flue gas channel together form a hollow water-cooling channel of the flue gas channel.
所述的冷焰气化器壁面外侧和燃烧室壳体内侧分别敷设冷焰气化器绝热层和燃烧室绝热层。The outer side of the cold flame gasifier wall surface and the inner side of the combustion chamber shell are respectively laid with a cold flame gasifier thermal insulation layer and a combustion chamber thermal insulation layer.
所述的冷焰气化器固定环为环形结构,环壁上围绕中心孔均匀地分布有通气孔。The cold flame gasifier fixing ring has an annular structure, and ventilation holes are evenly distributed around the central hole on the ring wall.
所述的燃烧室水冷通道和烟气通道水冷通道通过烟气通道连接体上的冷却水引流通道相连接,实现冷却水流的贯通,冷却水引流通道横截面呈现圆环形。The water cooling channel of the combustion chamber and the water cooling channel of the flue gas channel are connected by the cooling water drainage channel on the flue gas channel connecting body to realize the penetration of the cooling water flow, and the cross section of the cooling water drainage channel is circular.
所述的烟气通道水冷通道壁面和燃烧室水冷通道壁面上分别设置冷却水入口和冷却水出口,同时冷却水入口和冷却水出口的横截面形状均为圆环形。The cooling water inlet and the cooling water outlet are respectively provided on the wall surface of the water cooling channel of the flue gas channel and the wall surface of the water cooling channel of the combustion chamber, and the cross-sectional shapes of the cooling water inlet and the cooling water outlet are both circular.
所述的烟气通道壁面与烟气通道水冷通道壁面通过周向均匀分布的烟气通道水冷通道支撑体实现烟气通道水冷通道壁面的固定连接。The wall surface of the flue gas channel and the wall surface of the water cooling channel of the flue gas channel are fixedly connected to the wall surface of the water cooling channel of the flue gas channel through the evenly distributed flue gas channel water cooling channel support body.
所述的燃烧室壳体通过与燃烧室水冷通道壁面通过周向均匀分布的燃烧室水冷通道支撑体实现燃烧室水冷通道壁面的固定连接。The combustion chamber casing is fixedly connected to the wall surface of the water cooling channel of the combustion chamber through the support body of the water cooling channel of the combustion chamber uniformly distributed in the circumferential direction.
有益效果:Beneficial effects:
1、为了解决传统液体燃料燃烧中液体燃料蒸发与燃烧过程不能很好的分离,从而引起的污染物排放高,能量密度低等一系列问题,本发明公开的一种具备冷焰预蒸发的液体燃料多孔介质燃烧器,以液体燃料作为燃烧物质,能量密度显著高于传统微型液体燃烧装置,且污染物排放低,燃料添加方便。液体燃料能够通过压力旋流喷嘴进液口供入燃烧器中,并且能够通过调节压力旋流喷嘴的供油压力调节燃烧器的燃烧功率,为外界提供能量。1. In order to solve a series of problems such as high pollutant discharge and low energy density caused by the inability to separate liquid fuel evaporation and combustion process well in traditional liquid fuel combustion, the present invention discloses a liquid with cold flame pre-evaporation. The fuel porous medium burner uses liquid fuel as the combustion material, and the energy density is significantly higher than that of the traditional micro liquid combustion device, and the pollutant emission is low, and the fuel addition is convenient. The liquid fuel can be supplied into the burner through the liquid inlet of the pressure swirl nozzle, and the combustion power of the burner can be adjusted by adjusting the oil supply pressure of the pressure swirl nozzle to provide energy to the outside world.
2、本发明公开的一种具备冷焰预蒸发的液体燃料多孔介质燃烧器,采用液体燃料的冷焰反应放热预先蒸发液体燃料的预蒸发方案,能够将液体燃料的蒸发和燃烧过程很好地分离,有利于燃料与空气的预混燃烧,从而提高燃烧器的燃烧效率,拓宽燃烧器功率的调节范围。2. A liquid fuel porous medium burner with cold flame pre-evaporation disclosed in the present invention adopts the pre-evaporation scheme of pre-evaporating the liquid fuel by using the cold flame reaction heat release of the liquid fuel, which can improve the evaporation and combustion process of the liquid fuel. It is beneficial to the premixed combustion of fuel and air, thereby improving the combustion efficiency of the burner and broadening the adjustment range of the burner power.
3、本发明公开的一种具备冷焰预蒸发的液体燃料多孔介质燃烧器,采用多孔介质微燃烧技术,具有燃烧充分,热损失低,燃烧污染物排放低的优点,此外在该燃烧器采用多孔介质燃烧技术,利用多孔介质燃烧技术具有的回热特性预热来流预混气体,极大拓宽该燃烧器燃烧当量比范围。3. A liquid fuel porous medium burner with cold flame pre-evaporation disclosed in the present invention adopts porous medium micro-combustion technology, which has the advantages of sufficient combustion, low heat loss and low emission of combustion pollutants. Porous medium combustion technology uses the regenerative characteristics of porous medium combustion technology to preheat the premixed gas, which greatly broadens the range of the burner's combustion equivalence ratio.
4、本发明公开的一种具备冷焰预蒸发的液体燃料多孔介质燃烧器,采用水流冷却和绝热材料相结合的方式,保证燃烧器热强度、减小燃烧器结构尺寸且控制燃烧器向外界的热量释放,具有热损失小,燃烧器外壁温度低,能有效防止人员烫伤,人机环境好的优点。此外通过烟气冷却通道降低污染物的排放。4. A liquid fuel porous medium burner with cold flame pre-evaporation disclosed in the present invention adopts the combination of water flow cooling and thermal insulation material to ensure the thermal strength of the burner, reduce the structural size of the burner, and control the burner to the outside world. It has the advantages of small heat loss, low temperature of the outer wall of the burner, which can effectively prevent personnel from being scalded and a good man-machine environment. In addition, pollutant emissions are reduced by the flue gas cooling channel.
5、本发明公开的一种具备冷焰预蒸发的液体燃料多孔介质燃烧器,液体燃料能够通过压力旋流喷嘴进液口供入燃烧器中,并且能够通过调节压力旋流喷嘴的供油压力调节燃烧器的燃烧功率,提高能量的利用率。5. A liquid fuel porous medium burner with cold flame pre-evaporation disclosed in the present invention, the liquid fuel can be supplied into the burner through the liquid inlet of the pressure swirl nozzle, and can be adjusted by adjusting the oil supply pressure of the pressure swirl nozzle The combustion power of the burner improves the utilization rate of energy.
附图说明Description of drawings
图1为具体实施方式中的液体燃料多孔介质燃烧器的剖视视图;1 is a cross-sectional view of a liquid fuel porous media burner in an embodiment;
图2为具体实施方式中的液体燃料多孔介质燃烧器的压力旋流喷嘴旋流喷射部分的主剖视图和俯视图;2 is a front cross-sectional view and a top view of a pressure swirl nozzle swirl injection portion of a liquid fuel porous media burner in a specific embodiment;
图3为具体实施方式中的液体燃料多孔介质燃烧器的A-A、B-B和C-C线剖视图;3 is a cross-sectional view along lines A-A, B-B and C-C of a liquid fuel porous media burner in a specific embodiment;
图4为具体实施方式中的液体燃料多孔介质燃烧器的烟气通道连接体主视图和俯视图;4 is a front view and a top view of a flue gas channel connecting body of a liquid fuel porous medium burner in a specific embodiment;
图5为具体实施方式中的液体燃料多孔介质燃烧器的冷焰气化器固定环示意图。5 is a schematic diagram of a cold flame gasifier fixing ring of a liquid fuel porous media burner in a specific embodiment.
其中,1—压力旋流喷嘴,2—喷嘴旋流室进液口,3—旋流室,4—喷嘴出口,5—螺栓,6—垫圈,7—螺母,8—冷却水出口,9—冷焰气化器固定环,10—燃烧室水冷通道,11—燃烧室壳体,12—燃烧室水冷通道壁面,13—燃烧室水冷通道支撑体,14—烟气通道连接体,15—冷却水引流通道,16—烟气通道水冷通道壁面,17—烟气通道水冷通道,18—冷却水入口,19—烟气通道壁面,20—烟气通道水冷通道支撑体,21—燃烧室绝热层,22—燃烧段多孔介质,23—预热段多孔介质,24—冷焰气化器壁面,25—冷焰气化器,26—冷焰气化器绝热层,27—空气入口,28—燃烧器上盖,29—压力旋流喷嘴进液口。Among them, 1—pressure swirl nozzle, 2—nozzle swirl chamber inlet, 3—swirl chamber, 4—nozzle outlet, 5—bolt, 6—washer, 7—nut, 8—cooling water outlet, 9— Cold flame vaporizer fixing ring, 10—water cooling passage of combustion chamber, 11—combustion chamber shell, 12—wall surface of water cooling passage of combustion chamber, 13—support body of water cooling passage of combustion chamber, 14—connecting body of flue gas passage, 15—cooling Water drainage channel, 16—flue gas channel water cooling channel wall surface, 17—flue gas channel water cooling channel, 18—cooling water inlet, 19—flue gas channel wall surface, 20—flue gas channel water cooling channel support body, 21—combustion chamber insulation layer , 22—porous medium in combustion section, 23—porous medium in preheating section, 24—wall surface of cold flame gasifier, 25—cold flame gasifier, 26—cold flame gasifier insulation layer, 27—air inlet, 28— The upper cover of the burner, 29—the liquid inlet of the pressure swirl nozzle.
具体实施方式Detailed ways
为了更好的说明本发明的目的和优点,下面结合图和具体实施例来对本发明进一步说明。In order to better illustrate the purpose and advantages of the present invention, the present invention will be further described below with reference to the drawings and specific embodiments.
实施例1Example 1
本实施例的液体燃料多孔介质燃烧器采用液体庚烷作为燃料,如图1所示,液态庚烷燃料通过压力旋流喷嘴进液口29供入压力旋流喷嘴1内,进而雾化喷入燃烧装置,只需通过调节压力旋流喷嘴1的供油压力进而调节燃料供入量即可调节燃烧器的功率。The liquid fuel porous medium burner of this embodiment uses liquid heptane as the fuel. As shown in FIG. 1 , the liquid heptane fuel is fed into the pressure swirl nozzle 1 through the pressure swirl nozzle
本实施例公开的一种具备冷焰预蒸发的液体燃料多孔介质燃烧器,如图1所示,包括压力旋流喷嘴1、喷嘴旋流室进液口2、旋流室3、喷嘴出口4、螺栓5、垫圈6、螺母7、压力旋流喷嘴进液口29。还包括冷却水出口8、冷焰气化器固定环9、燃烧室水冷通道10、燃烧室壳体11、燃烧室水冷通道壁面12、燃烧室水冷通道支撑体13、烟气通道连接体14、冷却水引流通道15、烟气通道水冷通道壁面16、烟气通道水冷通道17、冷却水入口18、烟气通道壁面19、烟气通道水冷通道支撑体20、燃烧室绝热层21、燃烧段多孔介质22、预热段多孔介质23、冷焰气化器壁面24、冷焰气化器25、冷焰气化器绝热层26、空气入口27、燃烧器上盖28。A liquid fuel porous medium burner with cold flame pre-evaporation disclosed in this embodiment, as shown in FIG. 1 , includes a pressure swirl nozzle 1 , a nozzle swirl chamber liquid inlet 2 , a swirl chamber 3 , and a nozzle outlet 4 , bolt 5, washer 6, nut 7, pressure
压力旋流喷嘴1采用95Cr18不锈钢材料,压力旋流喷嘴1包括上端的液体燃料进液部分和下端的旋流喷射部分;上端的液体燃料进液部分设置有压力旋流喷嘴进液口29,进液口直径为14mm,下端的旋流喷射部分设置有喷嘴旋流室进液口2、旋流室3以及喷嘴出口4,其中喷嘴旋流室进液口2直径为3mm,周向均匀分布,如图2所示,旋流室3直径为16mm,喷嘴出口4直径为2mm;上端的液体燃料进液和下端的旋流喷射两部分通过公称直径36mm,螺距1.5mm螺纹副相互连接;压力旋流喷嘴1再通过公称直径22mm,螺距1.5mm的螺纹副连接到燃烧器上盖28上;燃烧器上盖28设置有压力旋流喷嘴连接孔,孔内设置用于连接压力旋流喷嘴的内螺纹,同时在燃烧器上盖28的侧面对称设置两个空气入口27,空气入口27直径为3mm,其中可以布置风扇用于空气流量的调节;燃烧器上盖28通过4个M5螺栓与燃烧室主体部分连接;燃烧器主体部分为一中通的圆柱体,中间设置冷焰气化器25,冷焰气化器25内径为25mm,壁厚为2mm,长度为70mm,冷焰气化器25通过两个上下布置的冷焰气化器固定环9固定于燃烧室主体中央;冷焰气化器25为上端开口,下端封闭的圆筒结构;冷焰气化器25四周填充预热段多孔介质23和燃烧段多孔介质22,其中预热段多孔介质23采用孔径65ppi,孔隙率84%的泡沫型氧化铝材料制成,燃烧段多孔介质22采用孔径10ppi,孔隙率87%的泡沫型氧化铝材料制成,两段多孔介质的填充厚度均为75mm;所述的预热段多孔介质23用于预热来流燃料空气预混气体,提高预混气体的温度,有利于后续燃烧过程降低污染物排放,且有利于预混气体的均匀燃烧;所述的燃烧段多孔介质22,主要用于预混气体燃烧和火焰稳定,具有降低污染物排放和有利于预混气体均匀燃烧的作用;燃烧室壳体11壁厚为3mm,燃烧室水冷通道壁面12厚度为2mm;燃烧室水冷通道10横截面呈圆环形,圆环内环直径为45mm,外环直径为53mm,由燃烧室壳体11通过与燃烧室水冷通道壁面12连接形成;燃烧室主体与下端的烟气通道连接体14通过4个M5螺栓相互连接,烟气通道连接体外直径为83mm,中心设置直径为28mm的烟气收敛通道,如图4所示;烟气通道连接体14与烟气通道相连接,烟气通道为一中通的圆柱体,烟气通道直径为24mm,烟气通道壁面19厚度为1mm;烟气通道壁面19与烟气通道水冷通道壁面16共同形成中通的烟气通道水冷通道17,烟气通道水冷通道17横截面呈圆环形,内圆环直径为26mm,外圆环直径为34mm,烟气通道水冷通道壁面16厚度为2mm;以上提及的燃烧器部件及结构除压力旋流喷嘴1、预热段多孔介质23、燃烧段多孔介质22、燃烧室绝热层21、冷焰气化器绝热层26以及冷焰气化器固定环9外,其余燃烧器部件及结构均采用压力容器钢Q345R材料。The pressure swirl nozzle 1 is made of 95Cr18 stainless steel, and the pressure swirl nozzle 1 includes a liquid fuel inlet part at the upper end and a swirl injection part at the lower end; The diameter of the liquid port is 14mm, and the swirl jet part at the lower end is provided with a nozzle swirl chamber liquid inlet 2, a swirl chamber 3 and a nozzle outlet 4, wherein the nozzle swirl chamber liquid inlet 2 has a diameter of 3mm and is evenly distributed in the circumferential direction. As shown in Figure 2, the diameter of the swirl chamber 3 is 16mm, and the diameter of the nozzle outlet 4 is 2mm; the liquid fuel inlet at the upper end and the swirl jet at the lower end are connected to each other by a screw pair with a nominal diameter of 36mm and a pitch of 1.5mm; The flow nozzle 1 is then connected to the burner
所述的冷焰气化器壁面24外侧和燃烧室壳体11内侧分别敷设冷焰气化器绝热层26和燃烧室绝热层21,其中冷焰气化器绝热层26敷设厚度为1mm,燃烧室绝热层21敷设厚度为1.5mm,材料均采用氧化硅气凝胶绝热材料。The cold flame gasifier
所述的冷焰气化器固定环9为环形结构,如图5所示,环壁上围绕中心孔均匀的分布有通气孔,采用耐高温的陶瓷材料制成,固定环厚度为3mm。The cold flame vaporizer fixing ring 9 is a ring structure, as shown in FIG. 5 , there are ventilation holes evenly distributed around the central hole on the ring wall, made of high temperature resistant ceramic material, and the thickness of the fixing ring is 3mm.
所述的燃烧室水冷通道10和烟气通道水冷通道17通过烟气通道连接体14上的冷却水引流通道15相连接,实现冷却水流的贯通,冷却水引流通道横截面呈现圆环形,内径为3mm,壁厚为1mm,烟气通道连接体主视图和俯视图如图4所示。The water-cooling channel 10 of the combustion chamber and the water-cooling
所述的烟气通道水冷通道壁面16和燃烧室水冷通道壁面12上分别设置冷却水入口18和冷却水出口8,同时冷却水入口18和冷却水出口8的横截面形状都为圆环形,冷却水入口18和冷却水出口8内径均为3mm,壁厚为1mm。The cooling
所述的烟气通道壁面19与烟气通道水冷通道壁面16通过16个周向均匀分布的烟气通道水冷通道支撑体20实现烟气通道水冷通道壁面16的固定连接,支撑体均为直径为4mm的球形。The
所述的燃烧室壳体11通过与燃烧室水冷通道壁面12通过12个周向均匀分布的燃烧室水冷通道支撑体13实现燃烧室水冷通道壁面12的固定连接,支撑体均为直径为4mm的球形。The combustion chamber shell 11 is fixedly connected to the wall surface of the water-cooled channel of the combustion chamber 12 through 12 support bodies 13 of the water-cooled channel of the combustion chamber that are evenly distributed in the circumferential direction, and the supporting bodies are all 4 mm in diameter. spherical.
所述的燃烧器总长度为254mm,燃烧器压力旋流喷嘴的横截面直径为42mm,燃烧器横截面最大直径为83mm。燃烧器内部结构如图3所示。The total length of the burner is 254 mm, the diameter of the cross section of the pressure swirl nozzle of the burner is 42 mm, and the maximum diameter of the cross section of the burner is 83 mm. The internal structure of the burner is shown in Figure 3.
本实施例公开的一种具备冷焰预蒸发的液体燃料多孔介质燃烧器的工作方法为:向燃烧器的压力旋流喷嘴1的压力旋流喷嘴进液口29供入液态庚烷燃料,液态庚烷经过压力旋流喷嘴的旋流室3旋转破碎后经喷嘴出口4喷出形成细小的液滴。空气通过空气入口27进入燃烧器内,也可在空气入口27处安装风扇用于空气流量调节。然后庚烷液滴与空气进入冷焰气化器25内,同时由于燃烧室内燃烧产生的热量通过冷焰气化器绝热层26和冷焰气化器壁面24传入冷焰气化器内,使得冷焰气化器25内的温度达到液态庚烷燃料冷焰反应发生的条件,从而庚烷发生冷焰反应释放出热量使得液态庚烷得到完全的蒸发,蒸发后的气态庚烷回流同时与空气充分预混进入燃烧室的多孔介质区域内,经过预热段多孔介质23预热升温后进入燃烧段多孔介质22内燃烧,火焰稳定在预热段多孔介质23和燃烧段多孔介质22交界面处,燃烧释放的热量一部分由烟气通过烟气通道排出,另一部分热量进入冷焰气化器25内用于蒸发液态庚烷燃料,其余热量通过燃烧室壳体11进入冷却水中,由冷却水带走,保证整个燃烧器外壁面温度不致太高而发生人员烫伤。当燃烧器需要停止工作时,只需停止燃料供应与空气供入即可停止燃烧器。在燃烧器的启动阶段,由于液态庚烷的冷焰反应产生的小分子和活性基较容易点燃,因此采用外部点火器在燃烧器烟气通道出口处点燃预热燃烧器,达到稳定状态时只要不断供入液态庚烷就能够燃烧庚烷燃料释放热量。The working method of a liquid fuel porous medium burner with cold flame pre-evaporation disclosed in this embodiment is as follows: supplying liquid heptane fuel to the pressure swirl
以上所述的描述对本发明的目的、技术方案和优点进行了进一步消息说明,所应理解的是,以上所述仅为本发明的具体实施例,用于解释本发明,并不用于限定本发明的保护范围,凡在本发明的精神和原则之内,所做的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above description further explains the purpose, technical solutions and advantages of the present invention. It should be understood that the above are only specific embodiments of the present invention, which are used to explain the present invention and are not intended to limit the present invention. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included within the protection scope of the present invention.
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010734974.8A CN111853771B (en) | 2020-07-28 | 2020-07-28 | Liquid fuel porous medium combustor with cold flame pre-evaporation function |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010734974.8A CN111853771B (en) | 2020-07-28 | 2020-07-28 | Liquid fuel porous medium combustor with cold flame pre-evaporation function |
Publications (2)
Publication Number | Publication Date |
---|---|
CN111853771A CN111853771A (en) | 2020-10-30 |
CN111853771B true CN111853771B (en) | 2022-08-09 |
Family
ID=72947321
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202010734974.8A Expired - Fee Related CN111853771B (en) | 2020-07-28 | 2020-07-28 | Liquid fuel porous medium combustor with cold flame pre-evaporation function |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN111853771B (en) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59144106U (en) * | 1983-03-18 | 1984-09-26 | 日産自動車株式会社 | Burner for regeneration of trap for collecting exhaust particulates |
CN101832554A (en) * | 2010-05-18 | 2010-09-15 | 杭州电子科技大学 | Liquid fuel porous medium combusting device and combusting method thereof |
CN101846318A (en) * | 2009-03-27 | 2010-09-29 | 大日工业株式会社 | combustion device |
CN102563639A (en) * | 2011-12-30 | 2012-07-11 | 西安交通大学 | Porous medium and heat pipe combustor for liquid fuel |
CN202938295U (en) * | 2012-11-16 | 2013-05-15 | 航天长征化学工程股份有限公司 | Pressure-variable working-condition-variable oil burning nozzle |
CN109869719A (en) * | 2019-03-05 | 2019-06-11 | 山东理工大学 | A high temperature and high pressure porous medium burner |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3324921A (en) * | 1965-02-11 | 1967-06-13 | Westinghouse Electric Corp | Wick type burner |
JPH1194213A (en) * | 1997-09-19 | 1999-04-09 | Aisin Seiki Co Ltd | Combustor |
SE531133C2 (en) * | 2005-07-05 | 2008-12-23 | Zemission Ab | Catalytic burner and control procedure |
CN202835350U (en) * | 2012-09-11 | 2013-03-27 | 中天新能源农业科技投资有限公司 | A Novel Biological Liquid Fuel Burner |
-
2020
- 2020-07-28 CN CN202010734974.8A patent/CN111853771B/en not_active Expired - Fee Related
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59144106U (en) * | 1983-03-18 | 1984-09-26 | 日産自動車株式会社 | Burner for regeneration of trap for collecting exhaust particulates |
CN101846318A (en) * | 2009-03-27 | 2010-09-29 | 大日工业株式会社 | combustion device |
CN101832554A (en) * | 2010-05-18 | 2010-09-15 | 杭州电子科技大学 | Liquid fuel porous medium combusting device and combusting method thereof |
CN102563639A (en) * | 2011-12-30 | 2012-07-11 | 西安交通大学 | Porous medium and heat pipe combustor for liquid fuel |
CN202938295U (en) * | 2012-11-16 | 2013-05-15 | 航天长征化学工程股份有限公司 | Pressure-variable working-condition-variable oil burning nozzle |
CN109869719A (en) * | 2019-03-05 | 2019-06-11 | 山东理工大学 | A high temperature and high pressure porous medium burner |
Non-Patent Citations (1)
Title |
---|
液体正庚烷在微细直管燃烧器中的燃烧特性研究;赵俊英等;《热能动力工程》;20130320(第02期);164-170 * |
Also Published As
Publication number | Publication date |
---|---|
CN111853771A (en) | 2020-10-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN101832554B (en) | A liquid fuel porous medium combustion device and its combustion method | |
WO2021022584A1 (en) | Angular porous medium burner | |
CN108592020B (en) | A combustor with staged anti-swirling airflow to promote the evaporation of liquid fuel | |
JPS6367086B2 (en) | ||
CN108844061A (en) | A kind of backheating type liquid fuel porous medium burner | |
CN112443838B (en) | Blast premixed porous medium combustion radiator with secondary air and combustion method thereof | |
CN107166395A (en) | A kind of self-loopa low nitrogen oxide swirling burner | |
CN108266726A (en) | A kind of porous media combustor of subsidiary heat exchange function | |
CN103471101B (en) | Multi-spray-nozzle bulky combustion low-NOx gas combustor | |
CN205079447U (en) | Thermoelectric fuel electric fan heater | |
CN201184609Y (en) | Micro oil long flame ignition burner | |
CN107084390A (en) | A kind of gas-liquid double fuel Dual-cyclone combustor of high-efficiency cleaning | |
CN101975397B (en) | Liquid-fuel micro-combustor and design method thereof | |
CN106196172A (en) | Tiny engine combustor annular concave-convex wall evaporation tube | |
CN201652342U (en) | A liquid fuel porous medium combustion device | |
CN116398880A (en) | Micro-scale pure hydrogen fuel premixing burner | |
JPS5837413A (en) | Combustion equipment for liquid fuel | |
CN111853771B (en) | Liquid fuel porous medium combustor with cold flame pre-evaporation function | |
CN208886764U (en) | A regenerative liquid fuel porous medium burner | |
CN201688402U (en) | Heat regeneration type liquid fuel miniature combustor | |
CN202501473U (en) | Internal combustion gas burner | |
JPS6220372B2 (en) | ||
CN2527867Y (en) | Oil-less direct ignition burner for coal powder-fired boiler | |
CN100389286C (en) | A Pulverized Coal Ignition Burner Using Porous Media to Realize Ignition with Minimal Oil | |
CN114562742A (en) | An annular combustion chamber wall integrating fuel oil preheating and oil-gas ratio control |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220809 |