CN102242930B - Nozzle of burner - Google Patents
Nozzle of burner Download PDFInfo
- Publication number
- CN102242930B CN102242930B CN 201110196634 CN201110196634A CN102242930B CN 102242930 B CN102242930 B CN 102242930B CN 201110196634 CN201110196634 CN 201110196634 CN 201110196634 A CN201110196634 A CN 201110196634A CN 102242930 B CN102242930 B CN 102242930B
- Authority
- CN
- China
- Prior art keywords
- nozzle
- blade
- spout
- hole
- fuel
- 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
Images
Landscapes
- Nozzles (AREA)
Abstract
The invention discloses a nozzle of a burner. The nozzle provided by the invention is characterized in that a cylindrical nozzle base serves as a foundation, and a rotary vane, a regulating core and a nozzle cap are successively assembled on the nozzle of the burner; the front end of the nozzle base is provided with an annular fuel channel groove, and the nozzle cap is sleeved on the front end ofthe nozzle base; a spout is arranged on the top of the nozzle cap, and the regulating core is arranged in the spout; and the hammer-shaped lower part of the regulating core is in threaded connection with the inner wall of the rotary vane, and an air inlet channel and a fuel channel are arranged in the nozzle base and are communicated with a mixing swirl chamber which is communicated with the spout. The nozzle of the burner provided by the invention has the advantages of simple and compact structure, less parts, easiness in assembly and maintainence, and suitability for multiple-impurity high-particle liquid fuels with high temperature, corrosion and high viscosity; the oil gas mixing concentrated fine bubble transformation bursting atomization and the double-flow high-speed rotating 'tornado' tearing-type atomization can be formed by virtue of an inclined hole and an inclined guide groove which are arranged in the nozzle, thereby improving the oxygen supply and ensuring full burning; and the flame is transparent and bright and is high in temperature, the liquid-gas mixing is balanced, the heat efficiency and the heat use ratio are high, discharged materials are less, and the environmental friendliness and the economic benefit are better.
Description
Technical field
The present invention relates to a kind of burner nozzle, refer to a kind of burner nozzle that heavy and inferior fuel fully can be atomized especially.
Background technology
Burner is made up of fuel nozzle and air register.Burner nozzle is the critical component of industrial kiln burner, and fuel nozzle is placed on the air register axial line, and fuel fog is changed into thin dripping, and sprays in the combustion chamber with certain angle of flare (also claiming atomizing angle), and the air of sending into air register mixes the postignition burning mutually.Existing fuel nozzle mainly contains two kinds of pressure atomization and twins.The pressure atomization fuel nozzle is made up of splitter, spinning disk and atomizing piece.During use, fuel generally produces high speed rotary motion in spinning disk, through the centre bore ejection, is broken into thin dripping under action of centrifugal force, and the fuel droplet average diameter after atomizing is many below 100 microns.What pressure atomization was current is to adopt single fluid engine driven supercharging formula, progressively withdraws from the market because atomizing effect is difficult to meet the demands.The twin fuel nozzle then utilizes steam or compressed air as atomizing medium, utilizes the negative-pressure siphon of adjusting the flowing gas generation that fuel is accelerated and broken atomizing.As seen, twin namely obviously is better than single fluid engine driven supercharging formula on principle, wherein use steam as the bifurcation type fuel nozzle of atomizing medium, gain the name because steam channel becomes bifurcation shape oblique with fuel channel, it has the advantage that load regulation range is big, steam consumption is few.But market proves that also there is greatly room for improvement in twin.
Summary of the invention
The purpose of this invention is to provide a kind of two-fluid burner nozzle, the advantage of comprehensive single fluid engine driven supercharging formula and air-flow siphon and the explosion of double-current body fluid bubble transformation, produce double fluid and simultaneously around " cyclone " formula atomizing type of center high-speed rotary, with guarantee the fuel droplet diameter 30 microns following average diameters about 5 microns.
Designed a kind of burner nozzle according to above-mentioned purpose, comprise nozzle base, in this base, offer inlet channel and fuel channel with the axis parallel direction, described inlet channel and fuel channel be the sensible vortex chamber that mixes all, should mix vortex chamber and spout connection, described nozzle base is cylinder, has a counterbore at the front end edge axis of this nozzle base, and this counterbore is parallel with the fuel channel of straight-through front end and connect with inlet channel; In this counterbore, be shelved with a cross section and be the blade of T-shaped rotary body, the bottom of this blade is hollow tube, and the disc on blade top is shelved on counterbore along last and compressed and locate along the edge by the cap of spraying nozzle inwall, and the chamber that constitutes vertically between this blade and cap of spraying nozzle is described mixed vortex chamber; The described cap of spraying nozzle enclosure is at the front end of nozzle base, and spout is opened in the top of cap of spraying nozzle, is provided with one and regulates core in spout, is spirally connected in the tup shape bottom of this adjusting core and the inwall of blade.
Wherein, offer an annular fuel channel slot at the front end of described nozzle base, this fuel channel groove is vertical with fuel channel and directly be communicated with.On the disc on described blade top, have the through hole that mates and be communicated with the fuel channel groove vertically, also having the oblique hole that connects with described counterbore on disc, is matched in clearance between blade lower end and the counterbore, and the chamber that this gap constitutes is the inlet channel chamber that is communicated with inlet channel.Be evenly equipped with the groove that becomes 30～45 degree angles with circumferential normal direction on the disc upper surface of described blade top, this groove connects edge and the hollow hole of disc.Groove on the disc upper surface of described blade top is linear groove, and this groove arranges in pairs, and one is communicated with the fuel channel groove in edge, and adjacent another is communicated with oblique hole and the rest may be inferred in edge.Be provided with the clamp nut that carries out shutoff to along the lower port of axis hollow in the lower end of described blade, same week of the joint portion of this blade bottom and blade top disc upwards, also be provided with the cyclonic current through hole that runs through the blade lower sides equably.Described cyclonic current through hole is oblique hole, and this through hole becomes 30～45 degree angles with circumferential normal direction, and this through hole arranges in pairs.In addition, described spout is outside bell mouth shape, and the angle of bell-mouthed sidewall and bottom surface is 60～120 degree.The top that described adjusting core cooperates with spout is for also being the adjusting core top flat of T-shaped rotary body, and the bottom shape of the card of this T-shaped rotary body and described bell-mouthed shape adapt.
The present invention is simple in structure, compact, and parts are few, assemble, safeguard easily, and parts is metalwork, suitable hot environment, the high particle-liquid fuel of many impurity such as suitable corrosivity alcohol ether basic ring guarantor's liquid fuel and high viscosity environment protective emulsive heavy oil.During use, the inclined hole and the oblique slot that arrange by nozzle interior lead, band pressure gas stream and fuel stream is all sprayed from spout in rotary manner, the fluid of ejection is in the T-shaped rotary body guiding of regulating the core top and by the advantage of two-fluid siphon, axis before spout forms central negative pressure and double-current " cyclone " formula atomizing type that rotates at a high speed around the center simultaneously, under the pressure that forms at a high speed, make the intensive microbubble explosion in the gas-liquid DL stream, guaranteed that effectively the diameter of big footpath fuel droplet is below 30 even 10 microns, it is more abundant to make liquid fuel mix with combustion air, balanced, improve flammable liquid particulate and airborne oxygen contact area greatly, especially as jet-propelled sonic boom conflagration, substance combustion is thorough, the bright and limpid bright temperature height of flame, liquid gas mixed equilibrium, the thermal efficiency and heat utilization efficiency height, emission of substance is few, and environmental protection and economic benefit are splendid.
Description of drawings
The explanation of number in the figure acute pyogenic infection of finger tip, 1-nozzle base, 2-inlet channel, 3-air inlet guide hole, 4-cap of spraying nozzle, 5-counterbore are the inlet channel chamber, 6-cyclonic current through hole, and 8-mixes vortex chamber, 9-regulates core, and 91-regulates core top flat, 10-spout, the 11-blade, 111-disc, 112-through hole, the oblique hole of 113-, 114-groove, 115-hollow tube, 12-fuel channel groove, 13-clamp nut, 14-fuel channel.
The specific embodiment
Purport of the present invention provides a kind of two double-current method burner nozzle of pressing, and by small-sized " cyclone " that produces before nozzle, lives and the comminution of fuel fluid with powerful take-up roll, and the abundant atomizing that has realized fuel fluid is that the drop footpath is less than 30 microns.The invention will be further described below in conjunction with accompanying drawing.
Accompanying drawing 1～4 is given the design of having shown a kind of burner nozzle.Fig. 1 has shown that the present invention assembling has a look at configuration, and Fig. 4,2 and 3 has shown assembling and the annexation between each parts.As seen, this burner nozzle is based on nozzle base 1, and is equipped with blade 11 in regular turn, regulates core 9 and cap of spraying nozzle 4.Front end at nozzle base offers an annular fuel channel slot 12, and the cap of spraying nozzle enclosure is at the front end of nozzle base, and spout is opened in the top of cap of spraying nozzle, is provided with one and regulates core in spout, is spirally connected in the tup shape bottom of this adjusting core and the inwall of blade.
Fig. 5 has provided the partial rotation schematic diagram of the present invention's assembling by complete section.Comprehensive each figure as can be known, described base is a cylinder, in base, offer inlet channel 2 and fuel channel 15 with the axis parallel direction, front end edge axis at this nozzle base has a counterbore, the annular fuel channel slot is opened in the outside of counterbore and around one week of counterbore, this counterbore is parallel with the fuel channel of straight-through front end and connect with inlet channel, and the inlet channel mouth is positioned on the bottom of this counterbore, and the fuel channel groove is vertical with fuel channel and directly be communicated with.
In this counterbore, be shelved with a cross section and be the blade 11 of T-shaped rotary body, the bottom of this blade is hollow tube 115, the disc 111 on blade top is shelved on counterbore along last and compressed and locate along the edge by cap of spraying nozzle 4 inwalls, and the chamber that constitutes vertically between this blade and cap of spraying nozzle is described mixed vortex chamber.Described inlet channel and fuel channel be the sensible vortex chamber 8 that mixes all, and this mixed vortex chamber is communicated with spout 10.On the disc on described blade top, have the through hole 112 that mates and be communicated with the fuel channel groove vertically, on disc, also have the oblique hole 113 that connects with described counterbore, be matched in clearance between blade lower end and the counterbore, the chamber that this gap constitutes is the gas channel lumens 5 that is communicated with inlet channel.Be evenly equipped with the groove 114 that becomes 30～45 degree angles with circumferential normal direction at blade top disc upper surface, this groove connects edge and the hollow hole of disc; Groove on the blade top disc upper surface of stating is linear groove, and this groove arranges in pairs, and one is communicated with the fuel channel groove in edge, and adjacent another is communicated with oblique hole and the rest may be inferred in edge.Simultaneously, be provided with carry out the clamp nut 13 of shutoff along the lower port of axis hollow in the lower end of blade, same week of the joint portion of this blade bottom and blade top disc upwards, also be provided with the through hole 6 that runs through the blade lower sides equably, this through hole is oblique hole, this through hole becomes 30～45 degree angles with circumferential normal direction, and this through hole arranges in pairs.
Described spout is outside bell mouth shape, and the angle of bell-mouthed sidewall and bottom surface is 60～120 degree.The top that described adjusting core cooperates with spout is T-shaped rotary body 91, and the bottom shape of the card of this T-shaped rotary body and described bell-mouthed shape adapt.
In sum, the main body of nozzle of the present invention is made up of base, blade and clamp nut thereof, cap of spraying nozzle and adjusting core.Wherein be provided with two fluid gas channels and liquid paths in the base, and the oblique through hole on the blade hollow tube can be likened the one-level gas circuit to, the top cover of blade or the oblique slot on the disc surface then constitute secondary gas circuit and liquid road, by one, the rotating fluid that secondary gas circuit and liquid pass are led converges the back at mixed vortex chamber and forms three grades of gas-liquid mixture fluids, these three grades of gas-liquid mixture fluids have further been strengthened rotation under the guiding of regulating core and horn-like spout, and by illustrate as can be known the shape of spout be close up to the center earlier after again wide-angle diffuse to form the three swirler diffusing opening, mix in the vortex chamber and well-mixed gas-liquid mixture fluid one spout of gushing out so be compressed in, then fast rotational preshoot and decompression, pressure discharges and to make the quick-fried broken explosion of drop up hill and dale, so just produced maximum particle diameter less than 30 microns superfine drop gas-liquid binary mixture.
Claims (1)
1. burner nozzle, comprise nozzle base (1), offer inlet channel (2) and fuel channel (15) with the axis parallel direction in this base, described inlet channel and fuel channel be the sensible vortex chamber (8) that mixes all, should mix vortex chamber is communicated with spout (10)
Described nozzle base is cylinder, has a counterbore (5) at the front end edge axis of this nozzle base, and this counterbore is parallel with the fuel channel of straight-through front end and connect with inlet channel;
In this counterbore, be shelved with a cross section and be the blade (11) of T-shaped rotary body, the bottom of this blade is hollow tube (115), the disc on blade top (111) is shelved on counterbore along last and compressed and locate along the edge by cap of spraying nozzle (4) inwall, the chamber that constitutes vertically between this blade and cap of spraying nozzle is described mixed vortex chamber, it is characterized in that:
The described cap of spraying nozzle enclosure is at the front end of nozzle base, and spout is opened in the top of cap of spraying nozzle, is provided with one and regulates core (9) in spout, is spirally connected in the tup shape bottom of this adjusting core and the inwall of blade;
Front end at described nozzle base offers an annular fuel channel slot (12), and this fuel channel groove is vertical with fuel channel and directly be communicated with;
On the disc on described blade top, have the through hole (112) that mates and be communicated with the fuel channel groove vertically, on disc, also have the oblique hole (113) that connects with described counterbore, be matched in clearance between blade lower end and the counterbore, the chamber that this gap constitutes is the inlet channel chamber that is communicated with inlet channel;
Be evenly equipped with the groove (114) that becomes 30～45 degree angles with circumferential normal direction on the disc upper surface of described blade top, this groove connects the edge of disc and the hollow hole of blade;
Groove on the disc upper surface of described blade top is linear groove, and this groove arranges in pairs, and one is communicated with the fuel channel groove in edge by through hole, and adjacent another is communicated with oblique hole and the rest may be inferred in edge;
Be provided with in the lower end of described blade carrying out the clamp nut (13) of shutoff along the lower port of axis hollow, same week of the joint portion of this blade bottom and blade top disc upwards, also be provided with the cyclonic current through hole (6) that runs through the blade lower sides equably;
Described cyclonic current through hole is oblique hole, and this cyclonic current through hole becomes 30～45 degree angles with circumferential normal direction, and this cyclonic current through hole arranges in pairs;
Described spout is outside bell mouth shape, and the angle of bell-mouthed sidewall and bottom surface is 120 degree;
The top that described adjusting core cooperates with spout is for also being the adjusting core top flat (91) of T-shaped rotary body, and the bottom shape of the card of this T-shaped rotary body and described bell-mouthed shape adapt;
Thus, the inclined hole and the oblique slot that arrange by nozzle interior lead, band pressure gas stream and fuel stream is all sprayed from spout in rotary manner, the fluid of ejection is in the T-shaped rotary body guiding of regulating the core top and by the advantage of two-fluid siphon, axis before spout forms central negative pressure and double-current " cyclone " formula atomizing type that rotates at a high speed around the center simultaneously, under the pressure that forms at a high speed, make the intensive microbubble explosion in the gas-liquid DL stream, form single fluid engine driven supercharging formula and air-flow siphon and the explosion of double-current body fluid bubble transformation, produce double fluid and simultaneously around " cyclone " formula atomizing type of center high-speed rotary, make the fuel droplet diameter below 30 microns and average diameter at 5 microns, be suitable for corrosivity alcohol ether basic ring and protect liquid fuel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110196634 CN102242930B (en) | 2011-07-05 | 2011-07-05 | Nozzle of burner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110196634 CN102242930B (en) | 2011-07-05 | 2011-07-05 | Nozzle of burner |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102242930A CN102242930A (en) | 2011-11-16 |
| CN102242930B true CN102242930B (en) | 2013-09-18 |
Family
ID=44961111
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201110196634 Active CN102242930B (en) | 2011-07-05 | 2011-07-05 | Nozzle of burner |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102242930B (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105157058B (en) * | 2015-10-22 | 2018-05-01 | 耿烽 | A kind of extra quality combustor of methanol steam |
| CN107763615A (en) * | 2016-08-19 | 2018-03-06 | 河南汇金智能装备有限公司 | Oil gun |
| CN112984558A (en) * | 2021-03-17 | 2021-06-18 | 中国航发动力股份有限公司 | Natural gas nozzle of gas turbine |
| CN114229477B (en) * | 2021-12-24 | 2022-11-04 | 北京理工大学 | Stable powder supply method and device based on internal and external cyclone fluidized powder |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201045494Y (en) * | 2007-05-14 | 2008-04-09 | 青岛特利尔新能源有限责任公司 | Water coal slurry ring-shaped atomizing spray rod |
| CN201344531Y (en) * | 2008-10-24 | 2009-11-11 | 北京大学 | Self-priming swirl pneumatic atomizing nozzle |
| CN201866765U (en) * | 2010-11-29 | 2011-06-15 | 南京中船绿洲环保有限公司 | Microporous heavy oil spraying gun |
| CN202118905U (en) * | 2011-07-05 | 2012-01-18 | 清远市精旺环保设备有限公司 | Nozzle of burner |
-
2011
- 2011-07-05 CN CN 201110196634 patent/CN102242930B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN102242930A (en) | 2011-11-16 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101206029B (en) | Nozzle for minisize gas-turbine combustor | |
| CN102242930B (en) | Nozzle of burner | |
| CN103175219B (en) | Venturi tube device used for head portion of chemical regenerative cycle combustor | |
| CN101526233B (en) | Safe and energy-saving gas stove | |
| CN201672538U (en) | Whirlcone, pneumatic nebulization spray nozzle and gas turbine | |
| CN109737393A (en) | Big Pulverized Coal Concentration is than postponing hybrid vortex burner | |
| CN210751035U (en) | Portable fire extinguisher nozzle suitable for high boiling point gas fire extinguishing agent | |
| CN114046537A (en) | Combined premixing nozzle of microminiature gas turbine | |
| JPS6036811A (en) | Atomizer for liquid fuel burner | |
| CN113154444B (en) | Gas turbine combustion chamber head air inlet structure of whirl atomizing integration | |
| CN201832731U (en) | External mixing type double-fluid spray nozzle | |
| CN113294808A (en) | Air atomizing nozzle of combustion chamber of gas turbine | |
| CN109323258A (en) | One kind being based on polymorphic type jet-burner structure | |
| CN201367953Y (en) | Vortex ramjet engine | |
| CN202118905U (en) | Nozzle of burner | |
| CN202581309U (en) | Atomizing nozzle | |
| CN216010909U (en) | Fuel injection structure of combustion chamber of gas turbine | |
| CN112254125B (en) | Spiral-flow type pressure atomizing nozzle | |
| CN210022551U (en) | Double-fluid multistage atomizing nozzle | |
| CN201416922Y (en) | Safe and energy-saving gas stove | |
| CN102721053A (en) | Atomizing nozzle | |
| CN113464981A (en) | Air atomizing nozzle for enhancing atomizing effect | |
| CN208222510U (en) | A kind of double fuel air-swirl burner | |
| CN206973546U (en) | A kind of multistage atomizing oil gun | |
| CN219976409U (en) | Small-output mechanical atomization oil gun for power station boiler |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of invention: Nozzle of burner Effective date of registration: 20171106 Granted publication date: 20130918 Pledgee: Qingyuan Desheng Investment Group Co., Ltd. Pledgor: Qingyuan Jingwang Environmental Protection Equipment Co., Ltd. Registration number: 2017440000119 |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190808 Address after: 511517 Incubator Building 205, Qingyuan Senior Technical School, Chuangxing Avenue, 14 District, Qingyuan High-tech Zone, Guangdong Province Co-patentee after: Qingyuan High-tech Jingwang New Energy Research Institute Co., Ltd. Patentee after: Qingyuan Jingwang Environmental Protection Equipment Co., Ltd. Address before: 511500 No. 105, Commercial and Residential Building X6 and X7, Ping'an First Street, New Town, Longtang Town, Qingcheng District, Qingyuan City, Guangdong Province Patentee before: Qingyuan Jingwang Environmental Protection Equipment Co., Ltd. |