CN206094062U - Strong efflux combustor that revolves - Google Patents

Strong efflux combustor that revolves Download PDF

Info

Publication number
CN206094062U
CN206094062U CN201620973541.7U CN201620973541U CN206094062U CN 206094062 U CN206094062 U CN 206094062U CN 201620973541 U CN201620973541 U CN 201620973541U CN 206094062 U CN206094062 U CN 206094062U
Authority
CN
China
Prior art keywords
bluff body
flame chamber
steady flame
strong
ventilating duct
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
CN201620973541.7U
Other languages
Chinese (zh)
Inventor
牛芳
尚庆雨
王乃继
罗伟
崔豫泓
刘增斌
刘建航
徐大宝
李小炯
张红顺
纪任山
刘振宇
刘羽
孟长芳
王乾
王实朴
姜思源
刘刚
梁兴
张鑫
杨石
刘力章
王永英
肖翠微
程晓磊
李婷
陈隆
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.)
Beijing Tiandi Sunac Technology Co ltd
Original Assignee
Energy Saving Technology 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 Energy Saving Technology Co Ltd filed Critical Energy Saving Technology Co Ltd
Priority to CN201620973541.7U priority Critical patent/CN206094062U/en
Application granted granted Critical
Publication of CN206094062U publication Critical patent/CN206094062U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The utility model relates to a strong efflux combustor that revolves, its characterized in that: it includes ventilating duct, steady flame chamber, acceleration nozzle, revolves generating device and supply of fuel device by force, strong revolve generating device set up in in the ventilating duct, the strong exit end that revolves generating device with the inlet connection in steady flame chamber, the exit end in steady flame chamber with acceleration nozzle's inlet connection, supply of fuel device axle arrangement in strong revolving in generating device and the steady flame chamber, the supply of fuel device includes fuel spout soft breeze tube cell, the entrance point of fuel spout is worn out the airtight end of middle guide duct, the exit end of fuel spout passes strong revolve generating device and with steady flame chamber intercommunication, the wind tube cell along steady flame chamber axle arrangement and with fuel spout detachably connects, the airtight end of middle ventilating duct is worn out to the entrance point of wind tube cell through the fuel spout.

Description

Strong swirl jet burner
Technical field
The utility model is related to a kind of strong swirl jet burner, belongs to industrial burning device technical field.
Background technology
The such as shortage of the non-renewable energy resources of coal, oil and natural gas, and discharge in use it is unburned Hydrocarbon and oxynitrides heavy damage natural environment is use up, therefore high-efficiency cleaning is to solve using non-renewable resources Existing energy shortage and the effective way of environmental pollution.In recent years, domestic industry boiler obtains the development of explosion type, using efficient The Industrial Boiler of environmental protection replaces the policy guidance that traditional mediumand smallscale industrial boilers are China.Industrial Boiler compares station boiler, deposits Fuel characteristic difference than it is larger, load regulation range is relatively wide the characteristics of, but at present the design of Industrial Boiler is substantially pin To a certain specific fuel, when changing fuel characteristic or relatively low duty ratio, efficiency of combustion decline is there is, pollutant emission is high Problem.
The content of the invention
For problem present in background technology, the purpose of this utility model is to provide one kind to improve fuel adaptation Property and low stain, efficient strong swirl jet burner.
For achieving the above object, the utility model is employed the following technical solutions:It includes ventilating duct, steady flame chamber, accelerates spray Mouth, strong rotation generating means and fuel supply device;The strong rotation generating means is arranged in the ventilating duct, and the strong rotation occurs The port of export of device is connected with the entrance point in the steady flame chamber, the port of export in the steady flame chamber and the entrance point of the accelerating jet Connection, the fuel supply device is axial arranged in the strong rotation generating means and the steady flame chamber;In the ventilating duct Outside is provided with middle ventilating duct, and one end of the middle ventilating duct is tightly connected with the side wall in the steady flame chamber, and the other end is Sealed end and leave spacing with the entrance point of the ventilating duct, the middle ventilating duct side wall near the steady flame chamber position The airduct being connected with for introducing outside combustion air is put, the fuel supply device includes fuel nozzle ports and wind powder pipe, described The entrance point of fuel nozzle ports passes the sealed end of the middle ventilating duct, and the port of export of the fuel nozzle ports is sent out through the strong rotation Generating apparatus and connect with the steady flame chamber;The wind powder pipe is axial arranged and detachable with the fuel nozzle ports along the steady flame chamber Ground connection, the entrance point of the wind powder pipe passes the sealed end of the middle ventilating duct by fuel nozzle ports.
The strong rotation generating means includes axial blade group and bluff body group, outside and the wind-guiding of the axial blade group The inner side of cylinder is fastenedly connected, and is fastenedly connected on the outside of the inner side of the axial blade group and the bluff body group.
The bluff body group is connected in series by multiple bluff bodies, is threaded connection between each bluff body.
The axial blade group includes multiple axial blades, and the number of the axial blade is less than the number of the bluff body Mesh;Each axial blade is connected by concaveconvex structure with a bluff body.
Also include igniter, the igniter is stretched in the steady flame chamber through the bluff body group.
The steady flame chamber is more than the steady flame chamber using cylindrical structure or the cone structure of flaring, the length in the steady flame chamber Maximum gauge.
The accelerating jet adopts cylindrical structure.
The accelerating jet adopts tapered cone structure.
The port of export of the accelerating jet is provided with the second bluff body.
Second bluff body using V-arrangement bluff body, circular cone bluff body, oval bluff body, sand dune shape bluff body and cylindrical bluff body it One.
The utility model due to taking above technical scheme, with advantages below:1st, the utility model is by changing strong rotation The divergence of the quantity of axial blade and bluff body in generating means, the different swirling number of acquisition and air-flow causes the combustion of different qualities Material is fully burnt, and reduces pollutant emission.2nd, the utility model due to axial blade, helically arrange in bluff body group by rule Row, therefore, it is possible to be formed with tangential velocity in steady flame chamber and the strong cyclone field without tangential velocity nested high temperature recirculation zone.3、 Each bluff body is threaded connection in the utility model bluff body group, thus can easily assembly and disassembly bluff body adapting to different fuel Combustion characteristics.4th, the utility model is fluted due to arranging on the outside of bluff body, relative set male structure in axial blade, therefore Axial blade and bluff body can pass through the convenient assembly and disassembly of concaveconvex structure.5th, the utility model is adopted for gas, liquid fuel Fuel nozzle ports, for solid fuel wind powder pipe is adopted, therefore this burner is suitable for gas, liquid, solid.6th, the utility model Because burner produces exteenal reflux area, therefore, it is possible to cool down burner, the water cooling plant of burner can be cancelled, reduction is produced into This.7th, the utility model accelerating jet can be added by the way of bluff body using cylinder, therefore burner hearth is internally formed by returning that bluff body is formed The toroidal recirculation pattern that stream area and flow area sudden expansion are formed so that temperature is uniform in burner hearth, flame stabilization, pollutant emission drop It is low.
Description of the drawings
Fig. 1 is the utility model overall structure diagram;
Fig. 2 is the utility model wind powder pipe and backflow cap schematic diagram;
Fig. 3 revolves by force generating means structural representation for the utility model;
Fig. 4 is the utility model bluff body structural representation;
Fig. 5 is the utility model axial blade group front view structural representation;
Fig. 6 is the utility model axial blade group left view figure structure schematic representation;
Fig. 7 is the utility model axial blade and bluff body attachment structure schematic diagram;
Fig. 8 is the steady flame chamber of the utility model and accelerating jet using schematic diagram during cylindrical structure.
Specific embodiment
The utility model is described in detail with reference to the accompanying drawings and examples.
As shown in figure 1, the utility model includes ventilating duct 1, steady flame chamber 2, accelerating jet 3, strong rotation generating means and fuel Feeding mechanism.Strong rotation generating means is arranged in ventilating duct 1, and it includes axial blade group 4 and bluff body group 5, wherein, axial blade The outside of group 4 is fastenedly connected with the inner side of ventilating duct 1, and inner side and the outside of bluff body group 5 of axial blade group 4 are fastenedly connected.Surely The entrance point in flame chamber 2 is connected with the port of export of strong rotation generating means, and the port of export in steady flame chamber 2 connects with the entrance point of accelerating jet 3 Connect.The outside of ventilating duct 1 is provided with middle ventilating duct 6, one end of middle ventilating duct 6 is tightly connected with the side wall in steady flame chamber 2, The other end is sealed end and leaves spacing with the entrance point of ventilating duct 1.Middle ventilating duct 6 side wall near steady flame chamber 2 position Put the airduct 7 being connected with for introducing outside combustion air.Fuel supply device includes fuel nozzle ports 8 and wind powder pipe 9, fuel spray The entrance point of mouth 8 passes the sealed end of middle ventilating duct 6, and the port of export of fuel nozzle ports 8 connects through bluff body group 5 and with steady flame chamber 2 Lead to, gas or liquid fuel can enter stable burning cavity 2 by fuel nozzle ports 8;Wind powder pipe 9 along steady flame chamber 2 it is axial arranged and with combustion Material spout 8 is detachably connected, and its port of export passes through fuel nozzle ports near steady flame chamber 2 and the interface of accelerating jet 3, entrance point 8 sealed ends for passing middle ventilating duct 6, solid fuel enters stable burning cavity 2 by wind powder pipe 9.
In above-described embodiment, as shown in Fig. 2 the port of export in wind powder pipe 9 is provided with backflow cap 13, backflow cap 13 can pass through Two pillars or built-in blade are connected with wind powder pipe 9, make breeze airflow adverse current direct-injection or adverse current rotation spray into steady flame chamber 2.
In above-described embodiment, as shown in figure 3, bluff body group 5 is connected in series by the bluff body 10 of multiple same types, it is each blunt It is threaded connection between body 10.Top surface and the bottom surface positioned at the bluff body 10 of end except the bluff body 10 positioned at head end, remaining The top surface of bluff body 10 is provided with external screw thread (as shown in Figure 4), and bottom surface is provided with internal thread.
In above-described embodiment, as shown in Fig. 5~Fig. 7, axial blade group 4 includes multiple axial blades 11, wherein, axial leaf The quantity of piece 11 is less than the quantity of bluff body 10, and each axial blade 11 is connected by concaveconvex structure with a bluff body 10.
In above-described embodiment, as shown in figure 1, the utility model also includes stretching into the igniting dress in steady flame chamber 2 through bluff body group 5 Put 12.
In above-described embodiment, using cylindrical structure or the cone structure of flaring, the length in steady flame chamber 2 is more than steady in steady flame chamber 2 The maximum gauge in flame chamber 2.
In above-described embodiment, accelerating jet 3 adopts cylindrical structure or tapered cone structure, if using cylindrical structure, Need to accelerating jet 3 port of export center arrange bluff body 14 (as shown in Figure 7), wherein, bluff body 14 can adopt V-arrangement bluff body, Circular cone bluff body, oval bluff body, sand dune shape bluff body, cylindrical bluff body or other shapes of any curves bluff bodies.
Operation principle of the present utility model is as follows:
Outside combustion air sequentially passes through airduct 7, middle ventilating duct 6, ventilating duct 1 and enters strong rotation generating means, Jing Guoqiang Air is become into swirling eddy into steady flame chamber 2 after rotation generating means, in two recirculating zones formed behind of swirling eddy, one It is the exteenal reflux area formed by air, it can be used to cool down the utility model burner, and another is the high temperature reflux of nested Area.
The utility model is suitable for for gas, liquid and solid fuel, and gas or liquid fuel are directly from fuel nozzle ports 8 Into steady flame chamber 2, in the port of export of strong rotation generating means, air stream is mixed with fuel, forms main flame;Solid fuel leads to The return flow line for crossing wind powder pipe 9 and the backflow composition of cap 13 enters steady flame chamber 2 against spirt, and solid fuel is carried out through high temperature recirculation zone After preheating, mixed in strong rotation generating means port of export air stream and fuel, formed main flame;The air-flow of burning is in this practicality Convolution in novel burner is burned, and reaches up to the intersection of steady flame chamber 2 and accelerating jet 3, there is about 40~60% herein Burning gases flow back, and remaining burning gases forms high-temperature injection flame and enters burner hearth through accelerating jet 3.
The utility model can by change axial blade 11 number and bluff body 10 number come adjust high temperature recirculation zone and The property in exteenal reflux area.Reducing the number of axial blade 11 can reduce swirling number, increase the thickness in exteenal reflux area, increase axial leaf The number of piece 11, can reduce the thickness in exteenal reflux area;The thickness in exteenal reflux area is excessive, can cause incomplete combustion, exteenal reflux area Thickness is too little, and burner wall surface temperature can be caused too high, damages burner, so swirling number control is between 0.5~1.5 Preferably.If the number of axial blade 11 is identical with the number of bluff body 10, high temperature recirculation zone is by rotating jet and flow area sudden expansion The nested recirculating zone that the recirculating zone and the recirculating zone without tangential velocity that have tangential velocity for being formed is done jointly;If axial blade 11 number is less than the number of bluff body 10, and swirling number is reduced, and high temperature recirculation zone is that the nested formed by rotating jet and bluff body is returned Stream area;The turbulence intensity of the nested recirculating zone that rotating jet and flow area sudden expansion are formed is formed more than rotating jet and bluff body Nested recirculating zone, for gaseous fuel, preferably using axial blade 11 and the equal numbers of mode of bluff body 10, and liquid or Solid fuel is preferably less than by the way of the number of bluff body 10 using the number for selecting axial blade 11.
The utility model is only illustrated with above-described embodiment, and the structure of each part, set location and its connection are all can It is all individual part is carried out according to the utility model principle on the basis of technical solutions of the utility model with what is be varied from Improvement and equivalents, should not exclude outside protection domain of the present utility model.

Claims (10)

1. a kind of strong swirl jet burner, it is characterised in that:It includes ventilating duct, steady flame chamber, accelerating jet, revolves generating means by force And fuel supply device;It is described it is strong rotation generating means be arranged in the ventilating duct, it is described it is strong rotation generating means the port of export with The entrance point connection in the steady flame chamber, the port of export in the steady flame chamber is connected with the entrance point of the accelerating jet, the fuel Feeding mechanism is axial arranged in the strong rotation generating means and the steady flame chamber;The outside of the ventilating duct is provided with centre Ventilating duct, one end of the middle ventilating duct is tightly connected with the side wall in the steady flame chamber, the other end be sealed end and with it is described The entrance point of ventilating duct leaves spacing, is connected with for drawing near the position in the steady flame chamber in the side wall of the middle ventilating duct Enter the airduct of outside combustion air, the fuel supply device includes fuel nozzle ports and wind powder pipe, the import of the fuel nozzle ports End passes the sealed end of the middle ventilating duct, the port of export of the fuel nozzle ports through the strong rotation generating means and with it is described Steady flame chamber connection;The wind powder pipe is axial arranged and detachably connected with the fuel nozzle ports along the steady flame chamber, the wind The entrance point of tube cell passes the sealed end of the middle ventilating duct by fuel nozzle ports.
2. strong swirl jet burner as claimed in claim 1, it is characterised in that:The strong rotation generating means includes axial blade Group and bluff body group, are fastenedly connected on the inside of the outside of the axial blade group and the ventilating duct, the axial blade group it is interior It is fastenedly connected on the outside of side and the bluff body group.
3. strong swirl jet burner as claimed in claim 2, it is characterised in that:The bluff body group is connected in series by multiple bluff bodies Form, be threaded connection between each bluff body.
4. strong swirl jet burner as claimed in claim 3, it is characterised in that:The axial blade group includes multiple axial leaves Piece, the number of the axial blade is less than the number of the bluff body;Each axial blade is by concaveconvex structure and one The bluff body connection.
5. strong swirl jet burner as claimed in claim 2, it is characterised in that:Also include igniter, the igniter Stretch in the steady flame chamber through the bluff body group.
6. strong swirl jet burner as claimed in claim 1, it is characterised in that:The steady flame chamber is using cylindrical structure or flaring Cone structure, the maximum gauge of the length in the steady flame chamber more than the steady flame chamber.
7. strong swirl jet burner as claimed in claim 1, it is characterised in that:The accelerating jet adopts cylindrical structure.
8. strong swirl jet burner as claimed in claim 1, it is characterised in that:The accelerating jet is tied using tapered taper Structure.
9. strong swirl jet burner as claimed in claim 7, it is characterised in that:It is provided with the port of export of the accelerating jet Second bluff body.
10. strong swirl jet burner as claimed in claim 9, it is characterised in that:Second bluff body adopts V-arrangement bluff body, circle One of cone bluff body, oval bluff body, sand dune shape bluff body and cylindrical bluff body.
CN201620973541.7U 2016-08-29 2016-08-29 Strong efflux combustor that revolves Active CN206094062U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620973541.7U CN206094062U (en) 2016-08-29 2016-08-29 Strong efflux combustor that revolves

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620973541.7U CN206094062U (en) 2016-08-29 2016-08-29 Strong efflux combustor that revolves

Publications (1)

Publication Number Publication Date
CN206094062U true CN206094062U (en) 2017-04-12

Family

ID=58473606

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620973541.7U Active CN206094062U (en) 2016-08-29 2016-08-29 Strong efflux combustor that revolves

Country Status (1)

Country Link
CN (1) CN206094062U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109000226A (en) * 2018-08-31 2018-12-14 煤科院节能技术有限公司 A kind of air-cooled burner

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109000226A (en) * 2018-08-31 2018-12-14 煤科院节能技术有限公司 A kind of air-cooled burner
CN109000226B (en) * 2018-08-31 2023-12-29 北京天地融创科技股份有限公司 Air-cooled burner

Similar Documents

Publication Publication Date Title
CN201680364U (en) Efficient low NOx pulverized coal burner for small and medium-sized industrial boilers
CN102062396B (en) Composite concentration triple-wind-regulating low-NOx cyclone pulverized-coal burner
CN103615717A (en) Novel oxygen enrichment tiny-oil ignition and ultralow load stable-combustion combustor
CN203099814U (en) Pulverized coal burner
CN103791494B (en) A kind of air-cooled coal dust low NO and using method thereof
CN106168378A (en) A kind of premix classification strong eddy flow low stain gas burner
CN207539904U (en) Ultralow nitrogen gas burner
CN102679337B (en) Cyclone combustor with adjustable flame shape and mixing strength
CN102353049A (en) Stable combustion device for pulverized coal ignition
CN106949471A (en) A kind of multistage premix burner of low emission cool flame
CN201203108Y (en) Micro-oil heat reinforced nozzle coal-powder combustor capable of swinging
CN108870383A (en) A kind of pulverized-coal fired boiler low NOx combustion system
CN206145669U (en) Swirling flow pulverized coal burner
CN208901372U (en) A kind of pulverized-coal fired boiler low NOx combustion system
CN107543160A (en) A kind of ultralow nitrogen gas burner
CN208025506U (en) A kind of coal burner
CN201606876U (en) Low-NOx coal burner
CN104154566B (en) gas turbine dual fuel nozzle structure
CN206094062U (en) Strong efflux combustor that revolves
CN106439801B (en) A kind of reverse spray type bluff body vortex burner
CN106196042B (en) A kind of strong swirl jet burner
CN208418701U (en) A kind of low-NOx combustor for biomass and combustion of natural gas
CN206257664U (en) Reverse spray type bluff body vortex burner
CN205825031U (en) A kind of new and effective ultra-low nitrogen body burner
CN205579553U (en) Ultralow NOx coal burner

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: 102606 No.5, Yulong Street, Caiyu Economic Development Zone, Caiyu Town, Daxing District, Beijing

Patentee after: Beijing Tiandi Sunac Technology Co.,Ltd.

Address before: 102606 No.5, Yulong Street, Caiyu Economic Development Zone, Caiyu Town, Daxing District, Beijing

Patentee before: CHINA COAL RESEARCH INSTITUTE (CCRI) ENERGY SAVING TECHNOLOGY CO.,LTD.