CN108844068B - Full-premix surface type burner gas-air blender - Google Patents
Full-premix surface type burner gas-air blender Download PDFInfo
- Publication number
- CN108844068B CN108844068B CN201811020990.XA CN201811020990A CN108844068B CN 108844068 B CN108844068 B CN 108844068B CN 201811020990 A CN201811020990 A CN 201811020990A CN 108844068 B CN108844068 B CN 108844068B
- Authority
- CN
- China
- Prior art keywords
- gas
- air
- venturi
- chamber
- 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.)
- Active
Links
- 238000011144 upstream manufacturing Methods 0.000 claims abstract description 32
- 238000002347 injection Methods 0.000 claims description 18
- 239000007924 injection Substances 0.000 claims description 18
- 238000007789 sealing Methods 0.000 claims description 4
- 238000002156 mixing Methods 0.000 abstract description 17
- 238000002485 combustion reaction Methods 0.000 abstract description 12
- 239000003344 environmental pollutant Substances 0.000 abstract description 2
- 231100000719 pollutant Toxicity 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 4
- 239000003638 chemical reducing agent Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 230000002708 enhancing effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
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
- F23D14/46—Details, e.g. noise reduction means
- F23D14/62—Mixing devices; Mixing tubes
- F23D14/64—Mixing devices; Mixing tubes with injectors
-
- 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)
- Gas Burners (AREA)
Abstract
一种全预混表面式燃烧器燃气空气掺混器,属于燃烧设备技术领域,本发明为了解决传统燃烧器难以达到燃气空气均匀掺混,燃烧器易回火,燃烧效率低,污染气体排放含量高的问题。文丘里环形燃气腔位于燃气空气预混室内且同轴设置,主燃气管的一端通过固定法兰固定在燃气空气预混室上,另一端穿过燃气空气预混室与文丘里环形燃气腔相连通,文丘里环形燃气腔内设有内风道,文丘里环形燃气腔与燃气空气预混室之间设有外风道,文丘里环形燃气腔的两端分别设有上游旋流叶片和下游旋流叶片,上游旋流叶片和下游旋流叶片与轴向均设有夹角。本发明的一种全预混表面式燃烧器燃气空气掺混器可以使空气与燃气充分的混合,最后经过旋流叶片可以实现燃气空气均匀混合。
A fully premixed surface burner gas-air blender, which belongs to the technical field of combustion equipment. The invention is intended to solve the problem that traditional burners are difficult to achieve uniform mixing of gas and air, and the burners are prone to backfire, have low combustion efficiency, and have low levels of pollutant gas emissions. high question. The Venturi annular gas chamber is located in the gas and air premixing chamber and is coaxially arranged. One end of the main gas pipe is fixed on the gas and air premixing chamber through a fixed flange, and the other end passes through the gas and air premixing chamber and is connected to the Venturi annular gas chamber. There is an inner air duct in the Venturi annular gas chamber, and an outer air duct is provided between the Venturi annular gas chamber and the gas air premixing chamber. The two ends of the Venturi annular gas chamber are respectively equipped with upstream swirl blades and downstream The swirl blades, the upstream swirl blades and the downstream swirl blades are all provided with an included angle with the axial direction. The fully premixed surface burner gas-air blender of the present invention can fully mix air and gas, and finally achieve uniform mixing of gas and air through swirl blades.
Description
技术领域Technical field
本发明涉及一种全预混表面式燃烧器燃气空气掺混器,属于燃烧设备技术领域。The invention relates to a fully premixed surface burner gas-air blender and belongs to the technical field of combustion equipment.
背景技术Background technique
现有预混式燃烧器采用的燃气空气掺混结构大多都很简单,难以达到燃气空气均匀掺混的效果,因此导致燃烧器易回火,燃烧效率低,污染气体排放含量高等后果。Most of the gas-air mixing structures used in existing premixed burners are very simple, and it is difficult to achieve the effect of uniform mixing of gas and air. Therefore, the burner is prone to backfire, the combustion efficiency is low, and the pollutant gas emissions are high.
以下三种掺混结构形式为常见技术形式,对典型结构进行举例说明,如下:The following three blending structural forms are common technical forms. Examples of typical structures are given as follows:
1.旋流叶片/混风轮式1. Swirl blade/mixing wheel type
专利号:CN105546533APatent number: CN105546533A
燃气管的尾端端部依次置有多支燃气喷枪和多个旋流叶片;燃气分别经由燃气喷枪上的喷孔和燃气管上的燃气管孔均匀进入喉口;同时,助燃空气与所述燃气在喉口内对冲均匀混合,再由设置在燃气管端部旋流叶片的搅动下进一步促使均匀混合,混合距离缩短,有效避免了因燃气混合不均而产生火焰温度不均匀,从而降低了NOx排放。A plurality of gas nozzles and a plurality of swirl blades are arranged at the rear end of the gas pipe; the gas enters the throat evenly through the nozzle holes on the gas nozzle gun and the gas pipe holes on the gas pipe; at the same time, the combustion air and the The gas is mixed evenly in the throat, and then is further mixed evenly by the swirling blades installed at the end of the gas pipe. The mixing distance is shortened, which effectively avoids uneven flame temperature due to uneven mixing of the gas, thus reducing NOx. emission.
缺点:具有混合死区,越贴近于喉口内壁燃气/空气浓度组分越不均匀。Disadvantages: It has a mixing dead zone, and the closer it is to the inner wall of the throat, the more uneven the gas/air concentration components will be.
2.文丘里结构2. Venturi structure
专利号:WO2012007823A1Patent number: WO2012007823A1
文丘里通道型空气/气体混合器相对于气流(AF)设置在风扇的下游。混合器包括局部压力损失装置,在这种情况下由文丘里管道管构成。对空气/燃气比例调节主要是通过调节喷嘴尺寸(UGL)(UG2),其次为流量调节器的调整。放置在燃气阀和文丘里通道型空气/气体混合器之间的连接管上的流量调节器允许精确地调节所供给的气体量以具有用于燃烧头中的混合燃烧的最佳空气/气体比。A venturi channel type air/gas mixer is positioned downstream of the fan with respect to the air flow (AF). The mixer includes a local pressure loss device, in this case consisting of a venturi duct tube. The air/gas ratio is mainly adjusted by adjusting the nozzle size (UGL) (UG2), followed by the adjustment of the flow regulator. A flow regulator placed on the connecting pipe between the gas valve and the venturi channel type air/gas mixer allows precise adjustment of the supplied gas volume to have an optimal air/gas ratio for mixed combustion in the combustion head .
缺点:流道的特征尺寸减小,流速发生变化,空气侧压力突增,导致燃气/空气具有明显的压差,燃气喷射不充分,导致燃气/空气在径向混合不均匀。Disadvantages: The characteristic size of the flow channel is reduced, the flow rate changes, and the air side pressure suddenly increases, resulting in a significant pressure difference between gas/air, and insufficient gas injection, resulting in uneven radial mixing of gas/air.
3.孔板/丝网结构3. Orifice plate/wire mesh structure
专利号:US6834504B2Patent number: US6834504B2
旋流发生器具有轴向延伸的,至少近似旋转对称的腔室,燃烧通过入口狭缝优选地平行于纵向轴线流动。作为这些或多或少的狭缝形入口的切向取向的结果,燃烧空气经历强烈的切向速度分量,导致与朝向燃烧器口或出口的轴向分量相互作用,以涡流通过所述内部室。通过在燃烧空气入口狭缝附近的壳体罩上和/或经由燃烧器轴线中的中心供给装置的装置可选地或互补地进行燃料的富燃。在与燃料的燃烧空气的混合部分内的燃烧器的下游部分中布置网状结构。该网状结构由跨过流动横截面的至少一根丝网组成。The swirl generator has an axially extending, at least approximately rotationally symmetrical chamber, with combustion flowing through an inlet slit preferably parallel to the longitudinal axis. As a result of the tangential orientation of these more or less slit-shaped inlets, the combustion air experiences a strong tangential velocity component, causing interaction with an axial component towards the burner mouth or outlet to swirl through the internal chamber . Enrichment of the fuel is optionally or complementarily carried out by means on the housing hood in the vicinity of the combustion air inlet slit and/or via a central feed in the burner axis. A mesh structure is arranged in the downstream portion of the burner within the mixing portion of the combustion air with the fuel. The mesh structure consists of at least one wire mesh spanning the flow cross-section.
缺点:网状结构,其主要作用是使混合气体经过网状结构后加强湍流,进而加强混合,但是到网状结构空隙很小,会对流动产生较大阻力。Disadvantages: The main function of the mesh structure is to enhance the turbulence of the mixed gas after passing through the mesh structure, thereby enhancing the mixing. However, the gaps in the mesh structure are very small, which will cause greater resistance to the flow.
发明内容Contents of the invention
本发明的目的是提供一种全预混表面式燃烧器燃气空气掺混器,以解决上述问题。The object of the present invention is to provide a fully premixed surface burner gas-air blender to solve the above problems.
一种全预混表面式燃烧器燃气空气掺混器包括燃气空气预混室、上游旋流叶片、下游旋流叶片、文丘里环形燃气腔、主燃气管、内风道、外风道和固定法兰;A fully premixed surface burner gas air mixer includes a gas air premixing chamber, an upstream swirl blade, a downstream swirl blade, a Venturi annular gas cavity, a main gas pipe, an inner air duct, an outer air duct and a fixed flange;
文丘里环形燃气腔位于燃气空气预混室内且同轴设置,主燃气管的一端通过固定法兰固定在燃气空气预混室上,另一端穿过燃气空气预混室与文丘里环形燃气腔相连通,文丘里环形燃气腔内设有内风道,文丘里环形燃气腔与燃气空气预混室之间设有外风道,文丘里环形燃气腔的两端分别设有上游旋流叶片和下游旋流叶片,上游旋流叶片和下游旋流叶片与轴向均设有夹角。The Venturi annular gas chamber is located in the gas and air premixing chamber and is coaxially arranged. One end of the main gas pipe is fixed on the gas and air premixing chamber through a fixed flange, and the other end passes through the gas and air premixing chamber and is connected to the Venturi annular gas chamber. There is an inner air duct in the Venturi annular gas chamber, and an outer air duct is provided between the Venturi annular gas chamber and the gas air premixing chamber. The two ends of the Venturi annular gas chamber are respectively equipped with upstream swirl blades and downstream The swirl blades, the upstream swirl blades and the downstream swirl blades are all provided with an included angle with the axial direction.
优选的:燃气空气预混室为两端开口的圆筒,燃气空气预混室一端的端面上设有预混室风机法兰,另一端的端面上设有法兰,法兰的端面上开有螺栓孔。Preferably: the gas air premixing chamber is a cylinder with openings at both ends. The gas air premixing chamber is provided with a premixing chamber fan flange on the end face of one end, and a flange is provided on the end face of the other end. The end face of the flange is open. There are bolt holes.
优选的:文丘里环形燃气腔包括第一变径管、第二变径管、外文丘里管和内文丘里管;Preferably: the Venturi annular gas chamber includes a first reducing tube, a second reducing tube, an outer Venturi tube and an inner Venturi tube;
内文丘里管位于外文丘里管内,内文丘里管的左右两端分别通过第一变径管和第二变径管与外文丘里管的左右两端相连接,外文丘里管和内文丘里管的管壁上分别开有外文丘里环形腔燃气喷射孔和内文丘里环形腔燃气喷射孔,外文丘里环形腔燃气喷射孔和内文丘里环形腔燃气喷射孔等间距均布或错位分布或内外层管上疏密分布或不同孔径分布,且开孔方向与燃气空气预混室的中轴线相垂直,第一变径管和第二变径管小口径端的端面上均设有连接法兰,两个连接法兰分别通过上游旋流叶片固定法兰和下游旋流叶片固定法兰与上游旋流叶片和下游旋流叶片相连接。外文丘里管的底端设有内螺纹管接头,内螺纹管接头一端与文丘里环形燃气腔内部连通,另一端与主燃气管螺纹连接。The inner venturi tube is located in the outer venturi tube. The left and right ends of the inner venturi tube are connected to the left and right ends of the outer venturi tube through the first reducing tube and the second reducing tube respectively. The outer venturi tube and the inner venturi tube The outer venturi annular cavity gas injection holes and the inner venturi annular cavity gas injection holes are respectively opened on the wall of the inner pipe. The outer venturi annular cavity gas injection holes and the inner venturi annular cavity gas injection holes are equally spaced or misaligned. Distribution or dense distribution or different hole diameter distribution on the inner and outer tubes, and the opening direction is perpendicular to the central axis of the gas-air premixing chamber. There are connections on the end faces of the small diameter ends of the first reducer tube and the second reducer tube. Flange, the two connecting flanges are respectively connected to the upstream swirl blade and the downstream swirl blade through the upstream swirl blade fixed flange and the downstream swirl blade fixed flange. The bottom end of the outer venturi tube is provided with an internally threaded pipe joint. One end of the internally threaded pipe joint is connected to the inside of the venturi annular gas chamber, and the other end is threadedly connected to the main gas pipe.
优选的:圆筒的底端设有开口,主燃气管位于开口内,开口端部设有主燃气管固定接头,主燃气管固定接头与固定法兰通过第一螺栓相连接,主燃气管上与主燃气管固定接头相对位置处设有限位凸台,限位凸台下端面安装有密封圈。Preferably: the bottom end of the cylinder is provided with an opening, the main gas pipe is located in the opening, the opening end is provided with a main gas pipe fixed joint, the main gas pipe fixed joint and the fixed flange are connected through a first bolt, and the main gas pipe is A limiting boss is provided at a position opposite to the fixed joint of the main gas pipe, and a sealing ring is installed on the lower end of the limiting boss.
优选的:上游旋流叶片固定法兰和下游旋流叶片固定法兰分别设有多个上游旋流叶片安装孔和多个下游旋流叶片孔,上游旋流叶片和下游旋流叶片分别通过紧固螺栓安装在流叶片安装孔和下游旋流叶片孔上。Preferably: the upstream swirl blade fixed flange and the downstream swirl blade fixed flange are respectively provided with a plurality of upstream swirl blade mounting holes and a plurality of downstream swirl blade holes, and the upstream swirl blades and downstream swirl blades are respectively tightened. Install the fastening bolts on the flow blade mounting holes and the downstream swirl blade holes.
本发明与现有产品相比具有以下效果:由于特殊的环形燃气腔结构,空气经过风机抽入后经上游旋流叶片扰流后进入内风道和外风道,燃气通过文丘里环形燃气腔上的燃气喷射空进入内风道和外风道,并与空气混合,最后经过下游旋流叶片再次充分掺混,因而空气与燃气可以得到较充分的混合,空气和燃气在有限的预混距离内可以达到充分混合,从而实现燃气空气均匀掺混,进而改善燃烧。Compared with existing products, the present invention has the following effects: due to the special annular gas chamber structure, the air is sucked in by the fan and then turbulent by the upstream swirl blades before entering the inner air duct and the outer air duct, and the gas passes through the Venturi annular gas chamber. The gas jet air enters the inner air duct and the outer air duct, and mixes with the air. Finally, it is fully mixed again through the downstream swirl blades, so the air and gas can be fully mixed, and the air and gas are mixed within a limited premixing distance. Full mixing can be achieved within the system, thereby achieving uniform mixing of gas and air, thereby improving combustion.
附图说明Description of the drawings
图1是本发明所述的一种全预混表面式燃烧器燃气空气掺混器的结构示意图;Figure 1 is a schematic structural diagram of a fully premixed surface burner gas-air blender according to the present invention;
图2是旋流叶片的安装位置结构示意图;Figure 2 is a schematic structural diagram of the installation position of the swirl blade;
图3是文丘里环形燃气腔的结构示意图:Figure 3 is a schematic structural diagram of the Venturi annular gas chamber:
图4是主燃气管与燃气空气预混室的连接结构示意图。Figure 4 is a schematic diagram of the connection structure between the main gas pipe and the gas air premixing chamber.
图中:1-燃气空气预混室;2-上游旋流叶片;3-下游旋流叶片;4-文丘里环形燃气腔;5-主燃气管;51-内层水平管;52-外层水平管;53-第一变径管;54-第二变径管;6-内风道、7-外风道;8-风机;9-固定法兰;11-预混室风机法兰;12-法兰、13-主燃气管固定接头、21-上游旋流叶片固定法兰、31-下游旋流叶片固定法兰、41-第一变径管、42-第二变径管、43-外文丘里管、44-内文丘里管、45-外文丘里环形腔燃气喷射孔、46-内文丘里环形腔燃气喷射孔、47-内螺纹管接头、410-连接法兰、51-限位凸台、C1-密封圈。In the picture: 1-gas air premixing chamber; 2-upstream swirl blades; 3-downstream swirl blades; 4-Venturi annular gas chamber; 5-main gas pipe; 51-inner horizontal pipe; 52-outer layer Horizontal pipe; 53-first reducing pipe; 54-second reducing pipe; 6-inner air duct, 7-outer air duct; 8-fan; 9-fixed flange; 11-premix chamber fan flange; 12-flange, 13-main gas pipe fixed joint, 21-upstream swirl blade fixed flange, 31-downstream swirl blade fixed flange, 41-first reducing pipe, 42-second reducing pipe, 43 -Outer Venturi tube, 44-inner Venturi tube, 45-outer Venturi annular cavity gas injection hole, 46-inner Venturi annular cavity gas injection hole, 47-internal threaded pipe joint, 410-connecting flange, 51- Limiting boss, C1-sealing ring.
具体实施方式Detailed ways
下面根据附图详细阐述本发明优选的实施方式。Preferred embodiments of the present invention will be described in detail below with reference to the accompanying drawings.
如图1至图4所示,本发明所述的一种全预混表面式燃烧器燃气空气掺混器包括燃气空气预混室1、上游旋流叶片2、下游旋流叶片3、文丘里环形燃气腔4、主燃气管5、内风道6、外风道7和固定法兰9;As shown in Figures 1 to 4, a fully premixed surface burner gas air mixer according to the present invention includes a gas air premixing chamber 1, an upstream swirl blade 2, a downstream swirl blade 3, a venturi Annular gas chamber 4, main gas pipe 5, inner air duct 6, outer air duct 7 and fixed flange 9;
文丘里环形燃气腔4位于燃气空气预混室1内且同轴设置,主燃气管5的一端通过固定法兰9固定在燃气空气预混室1上,另一端穿过燃气空气预混室1与文丘里环形燃气腔4相连通,文丘里环形燃气腔4内设有内风道6,文丘里环形燃气腔4与燃气空气预混室1之间设有外风道7,文丘里环形燃气腔4的两端分别设有上游旋流叶片2和下游旋流叶片3,上游旋流叶片2和下游旋流叶片3与轴向均设有夹角。The Venturi annular gas chamber 4 is located in the gas and air premixing chamber 1 and is coaxially arranged. One end of the main gas pipe 5 is fixed on the gas and air premixing chamber 1 through a fixed flange 9, and the other end passes through the gas and air premixing chamber 1. It is connected with the Venturi annular gas chamber 4. The Venturi annular gas chamber 4 is provided with an inner air duct 6. There is an outer air duct 7 between the Venturi annular gas chamber 4 and the gas air premixing chamber 1. The Venturi annular gas chamber 4 is connected with the Venturi annular gas chamber 4. The two ends of the cavity 4 are respectively provided with upstream swirl blades 2 and downstream swirl blades 3, and the upstream swirl blades 2 and the downstream swirl blades 3 have an included angle with the axial direction.
进一步:燃气空气预混室1为两端开口的圆筒,燃气空气预混室1一端的端面上设有预混室风机法兰11,另一端的端面上设有法兰12,法兰12的端面上开有螺栓孔121。Further: the gas air premixing chamber 1 is a cylinder with openings at both ends. The gas air premixing chamber 1 is provided with a premixing chamber fan flange 11 on the end face of one end, and a flange 12 is provided on the end face of the other end. The flange 12 There are bolt holes 121 on the end face.
进一步:文丘里环形燃气腔4包括第一变径管41、第二变径管42、外文丘里管43和内文丘里管44;Further: the Venturi annular gas chamber 4 includes a first reducing tube 41, a second reducing tube 42, an outer Venturi tube 43 and an inner Venturi tube 44;
内文丘里管44位于外文丘里管43内,内文丘里管44的左右两端分别通过第一变径管41和第二变径管42与外文丘里管43的左右两端相连接,外文丘里管43和内文丘里管44的管壁上分别开有外文丘里环形腔燃气喷射孔45和内文丘里环形腔燃气喷射孔46,外文丘里环形腔燃气喷射孔45和内文丘里环形腔燃气喷射孔46等间距均布或错位分布或内外层管上疏密分布或不同孔径分布,且开孔方向与燃气空气预混室1的中轴线相垂直,第一变径管41和第二变径管42小口径端的端面上均设有连接法兰410,两个连接法兰410分别通过上游旋流叶片固定法兰21和下游旋流叶片固定法兰31与上游旋流叶片2和下游旋流叶片3相连接,外文丘里管43的底端设有内螺纹管接头47,内螺纹管接头47一端与文丘里环形燃气腔4内部连通,另一端与主燃气管5螺纹连接。The inner venturi tube 44 is located in the outer venturi tube 43. The left and right ends of the inner venturi tube 44 are connected to the left and right ends of the outer venturi tube 43 through the first reducing tube 41 and the second reducing tube 42 respectively. The outer venturi annular cavity gas injection hole 45 and the inner venturi annular cavity gas injection hole 46 are respectively opened on the tube walls of the outer venturi tube 43 and the inner venturi tube 44. The outer venturi annular cavity gas injection hole 45 and the inner venturi annular cavity gas injection hole 45 The gas injection holes 46 in the inner annular cavity are equally spaced or staggered, or are densely distributed or have different hole diameters on the inner and outer tubes, and the opening direction is perpendicular to the central axis of the gas-air premixing chamber 1. The first reducing tube 41 and the small-diameter end of the second reducer 42 are provided with connecting flanges 410. The two connecting flanges 410 are respectively connected to the upstream swirl blades through the upstream swirl blade fixed flange 21 and the downstream swirl blade fixed flange 31. 2 is connected to the downstream swirl blade 3. The bottom end of the outer venturi pipe 43 is provided with an internally threaded pipe joint 47. One end of the internally threaded pipe joint 47 is internally connected with the venturi annular gas chamber 4, and the other end is threaded with the main gas pipe 5 connect.
进一步:圆筒的底端设有开口,主燃气管5位于开口内,开口端部设有主燃气管固定接头13,主燃气管固定接头13与固定法兰9通过第一螺栓9131相连接,主燃气管5上与主燃气管固定接头13相对位置处设有限位凸台51,限位凸台51下端面安装有密封圈C1。Further: the bottom end of the cylinder is provided with an opening, the main gas pipe 5 is located in the opening, and the main gas pipe fixed joint 13 is provided at the end of the opening. The main gas pipe fixed joint 13 and the fixed flange 9 are connected through the first bolt 9131. The main gas pipe 5 is provided with a limiting boss 51 at a position opposite to the main gas pipe fixed joint 13, and a sealing ring C1 is installed on the lower end of the limiting boss 51.
进一步:上游旋流叶片固定法兰21和下游旋流叶片固定法兰31分别设有多个上游旋流叶片安装孔211和多个下游旋流叶片孔311,上游旋流叶片2和下游旋流叶片3分别通过紧固螺栓安装在流叶片安装孔211和下游旋流叶片孔311上。Further: the upstream swirl blade fixed flange 21 and the downstream swirl blade fixed flange 31 are respectively provided with a plurality of upstream swirl blade mounting holes 211 and a plurality of downstream swirl blade holes 311. The upstream swirl blade 2 and the downstream swirl blade The blades 3 are respectively installed on the flow blade mounting holes 211 and the downstream swirl blade holes 311 through fastening bolts.
工作原理:working principle:
全预混表面式燃烧器掺混器使用双旋流叶片、内外文丘里通道结构。风机8在新型燃气空气掺混结构上游抽入空气1F,在上游旋流叶片处形成外通路2F与内通路3F,2F通路内的空气进入文丘里环形腔4,3F通路内的空气经由上游旋流叶片扰流后进入外风道形成旋流空气4F;燃气由外部燃气管道沿通路5F供入,在文丘里环形燃气腔4中形成循环通路6F,一部分由外文丘里环形腔燃气喷射孔45流出形成燃气8F至外风道7;另一部分由内文丘里环形腔燃气喷孔46流出形成燃气7F至内风道6。经外风道4的燃气8F与旋流空气4F混合,并经过下游旋流叶片3加强掺混,形成均匀燃气空气掺混气10F;经内风道6的燃气7F与3F通路内的空气混合后形成混合气9F,最终内外风道混合气在高效燃气空气掺混结构下游汇流,形成均匀混合气11F。The fully premixed surface burner mixer uses double swirl blades and an inner and outer venturi channel structure. The fan 8 draws air 1F upstream of the new gas-air mixing structure, forming an outer passage 2F and an inner passage 3F at the upstream swirl blades. The air in the 2F passage enters the Venturi annular cavity 4, and the air in the 3F passage passes through the upstream swirl blade. After being disturbed by the flow blades, it enters the outer air duct to form swirling air 4F; the gas is supplied from the external gas pipe along the passage 5F, forming a circulation passage 6F in the venturi annular gas chamber 4, part of which is formed by the gas injection hole 45 of the outer venturi annular cavity The gas 8F flows out to the outer air duct 7; the other part flows out from the inner venturi annular cavity gas injection hole 46 to form the gas 7F to the inner air duct 6. The gas 8F passing through the outer air duct 4 is mixed with the swirling air 4F, and the mixing is enhanced by the downstream swirling blades 3 to form a uniform gas-air mixture 10F; the gas 7F passing through the inner air duct 6 is mixed with the air in the 3F passage Finally, the mixed gas 9F is formed, and finally the mixed gas in the inner and outer air ducts merges downstream of the high-efficiency gas air mixing structure to form a uniform mixed gas 11F.
本实施方式只是对本专利的示例性说明,并不限定它的保护范围,本领域技术人员还可以对其局部进行改变,只要没有超出本专利的精神实质,都在本专利的保护范围内。This embodiment is only an illustrative description of this patent and does not limit its protection scope. Those skilled in the art can also make partial changes to it. As long as the spirit and essence of this patent are not exceeded, they are all within the protection scope of this patent.
Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811020990.XA CN108844068B (en) | 2018-09-03 | 2018-09-03 | Full-premix surface type burner gas-air blender |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811020990.XA CN108844068B (en) | 2018-09-03 | 2018-09-03 | Full-premix surface type burner gas-air blender |
Publications (2)
Publication Number | Publication Date |
---|---|
CN108844068A CN108844068A (en) | 2018-11-20 |
CN108844068B true CN108844068B (en) | 2024-01-19 |
Family
ID=64233941
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201811020990.XA Active CN108844068B (en) | 2018-09-03 | 2018-09-03 | Full-premix surface type burner gas-air blender |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN108844068B (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111288448B (en) * | 2020-03-20 | 2022-03-29 | 东营富润智能科技有限公司 | Ultralow nitrogen burner for oil field heating furnace |
CN112316762B (en) * | 2020-10-28 | 2024-10-15 | 国电铜陵发电有限公司 | Double-stage rotational flow ammonia air mixing device based on Laval nozzle |
CN113417770A (en) * | 2021-05-31 | 2021-09-21 | 东风商用车有限公司 | Wall surface flow guiding type Venturi mixer |
CN113357058B (en) * | 2021-05-31 | 2022-11-01 | 东风商用车有限公司 | Central flow guide type venturi integrated mixer |
CN113417771B (en) * | 2021-05-31 | 2022-05-31 | 东风商用车有限公司 | Wall surface flow guide opposite impact type venturi integrated mixer |
CN113417769A (en) * | 2021-05-31 | 2021-09-21 | 东风商用车有限公司 | Turbulent flow type venturi integrated mixer |
CN113417768A (en) * | 2021-05-31 | 2021-09-21 | 东风商用车有限公司 | Central flow guiding type Venturi mixer |
CN113417775A (en) * | 2021-05-31 | 2021-09-21 | 东风商用车有限公司 | Turbulent flow type venturi mixer |
CN113417774B (en) * | 2021-05-31 | 2022-05-03 | 东风商用车有限公司 | Turbulent flow opposite impact type Venturi integrated mixer |
CN113417773A (en) * | 2021-05-31 | 2021-09-21 | 东风商用车有限公司 | Wall surface flow guide type venturi integrated mixer |
CN116162755B (en) * | 2023-04-04 | 2025-03-07 | 北京神科博斯热能工程技术有限公司 | A miniature hot air furnace |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA1289862C (en) * | 1988-05-16 | 1991-10-01 | David William Kramer | Gas burner construction |
DE10324706B3 (en) * | 2003-05-30 | 2004-12-02 | Hovalwerk Ag | Device for controlling the gas / air ratio for a premixing combustion device |
CN201412846Y (en) * | 2008-11-09 | 2010-02-24 | 覃洪波 | Gas burner |
CN102297429A (en) * | 2010-06-24 | 2011-12-28 | 通用电气公司 | Fuel nozzle assembly |
CN203240578U (en) * | 2012-07-15 | 2013-10-16 | 覃洪波 | Novel gas burner |
CN103776030A (en) * | 2014-02-28 | 2014-05-07 | 大连本源节能科技有限公司 | Mixed-flow burner provided with multiple centrally-symmetric tangential air channels |
CN105605579A (en) * | 2016-02-26 | 2016-05-25 | 上海诺特飞博燃烧设备有限公司 | Air-combustion full premixing device of metal fiber low-nitrogen combustion device |
CN205480979U (en) * | 2016-01-13 | 2016-08-17 | 哈尔滨工业大学 | High speed burner that jets of adaptation pluralities of fuel |
CN106196059A (en) * | 2016-08-26 | 2016-12-07 | 中能服能源科技股份有限公司 | A kind of low nitrogen oxide burner structure |
CN106705075A (en) * | 2016-12-12 | 2017-05-24 | 深圳智慧能源技术有限公司 | Torch with forced-cooling air film |
CN208720222U (en) * | 2018-09-03 | 2019-04-09 | 哈尔滨电气股份有限公司 | A fully premixed surface burner gas-air blender |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6238997B2 (en) * | 2012-11-07 | 2017-11-29 | エクスポネンシャル テクノロジーズ, インコーポレイテッドExponential Technologies, Inc. | Pressure gain combustion apparatus and method |
-
2018
- 2018-09-03 CN CN201811020990.XA patent/CN108844068B/en active Active
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA1289862C (en) * | 1988-05-16 | 1991-10-01 | David William Kramer | Gas burner construction |
DE10324706B3 (en) * | 2003-05-30 | 2004-12-02 | Hovalwerk Ag | Device for controlling the gas / air ratio for a premixing combustion device |
CN201412846Y (en) * | 2008-11-09 | 2010-02-24 | 覃洪波 | Gas burner |
CN102297429A (en) * | 2010-06-24 | 2011-12-28 | 通用电气公司 | Fuel nozzle assembly |
CN203240578U (en) * | 2012-07-15 | 2013-10-16 | 覃洪波 | Novel gas burner |
CN103776030A (en) * | 2014-02-28 | 2014-05-07 | 大连本源节能科技有限公司 | Mixed-flow burner provided with multiple centrally-symmetric tangential air channels |
CN205480979U (en) * | 2016-01-13 | 2016-08-17 | 哈尔滨工业大学 | High speed burner that jets of adaptation pluralities of fuel |
CN105605579A (en) * | 2016-02-26 | 2016-05-25 | 上海诺特飞博燃烧设备有限公司 | Air-combustion full premixing device of metal fiber low-nitrogen combustion device |
CN106196059A (en) * | 2016-08-26 | 2016-12-07 | 中能服能源科技股份有限公司 | A kind of low nitrogen oxide burner structure |
CN106705075A (en) * | 2016-12-12 | 2017-05-24 | 深圳智慧能源技术有限公司 | Torch with forced-cooling air film |
CN208720222U (en) * | 2018-09-03 | 2019-04-09 | 哈尔滨电气股份有限公司 | A fully premixed surface burner gas-air blender |
Also Published As
Publication number | Publication date |
---|---|
CN108844068A (en) | 2018-11-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN108844068B (en) | Full-premix surface type burner gas-air blender | |
JP3527280B2 (en) | Combustion chamber | |
JP3527278B2 (en) | Fuel supply system for combustion chamber | |
CN110631049B (en) | Gas Turbine Soft Combustor | |
US8113821B2 (en) | Premix lean burner | |
CN101158479A (en) | Liquid fuel enhancement for natural gas swirl stabilized nozzle and method | |
JPH0712313A (en) | Premixing burner | |
CN105157064B (en) | The method of premixing and the burner arrangement for executing this method | |
CN104896511B (en) | Fuel oil premixed apparatus for low emission combustion chamber | |
CN1137342C (en) | Burner for operating heat generator | |
CN110345475A (en) | A kind of premixed anti-backfire Flameless burner | |
CN103822229A (en) | Low swirl nozzle for combustion chamber of gas turbine | |
US6327860B1 (en) | Fuel injector for low emissions premixing gas turbine combustor | |
CN109028059B (en) | Full premix surface type burner with efficient gas-air mixing structure | |
CN116398880A (en) | Micro-scale pure hydrogen fuel premixing burner | |
CN109489070A (en) | A kind of gas-turbine combustion chamber cyclone and component | |
CN103822230B (en) | A kind of low swirl combustion chamber nozzle | |
CN106402856A (en) | High-temperature gas generating device and method capable of continuously, quickly and linearly adjusting temperature within large range | |
CN116066858A (en) | A low-emission hydrogen-fueled micromix combustor for gas turbines | |
CN208720222U (en) | A fully premixed surface burner gas-air blender | |
CN208764921U (en) | Fully premixed surface burner with high-efficiency gas-air blending structure | |
CN118463220A (en) | Gas premix combustion nozzle and burner | |
CN208817471U (en) | A fully premixed surface burner gas-air blender | |
CN112963832B (en) | A fully premixed low NOx burner with explosion-proof function | |
CN212618280U (en) | Low nitrogen gas burner |
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 |