CN102889615A - Fuel oil atomizing device - Google Patents

Fuel oil atomizing device Download PDF

Info

Publication number
CN102889615A
CN102889615A CN201210410201XA CN201210410201A CN102889615A CN 102889615 A CN102889615 A CN 102889615A CN 201210410201X A CN201210410201X A CN 201210410201XA CN 201210410201 A CN201210410201 A CN 201210410201A CN 102889615 A CN102889615 A CN 102889615A
Authority
CN
China
Prior art keywords
cup
evaporation tube
fuel
air
fuel oil
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.)
Pending
Application number
CN201210410201XA
Other languages
Chinese (zh)
Inventor
姜山
李洪伏
王忠鹏
江红兵
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.)
AVIC Harbin Dongan Engine Group Co Ltd
Original Assignee
AVIC Harbin Dongan Engine Group 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 AVIC Harbin Dongan Engine Group Co Ltd filed Critical AVIC Harbin Dongan Engine Group Co Ltd
Priority to CN201210410201XA priority Critical patent/CN102889615A/en
Publication of CN102889615A publication Critical patent/CN102889615A/en
Pending legal-status Critical Current

Links

Images

Landscapes

  • Nozzles For Spraying Of Liquid Fuel (AREA)

Abstract

The invention relates to a fuel oil atomizing device which comprises an evaporation pipe, an air cup and an oil rotating device, wherein the evaporation pipe is formed by three sections of reversed-L-shaped pipes which form angles of 90 degrees; the oil rotating device is arranged at the inner part of a fuel oil outlet of the evaporation pipe; 4-6 spiral grooves are arranged on the outer surface of the oil rotating device; the air cup is mounted at the outer part of the evaporation pipe at the fuel oil inlet; a cup opening of the air cup is leveled with the fuel oil inlet of the evaporation pipe; and an air outlet is arranged on the side wall of the air cup. The fuel oil atomizing device disclosed by the invention realizes the aim of sufficiently atomizing under the condition of a very short oil mist range so that the evaporation rate is improved and good conditions are provided for stable and efficient combustion.

Description

Fuel atomization device
Technical field
The present invention relates to a kind of atomising device, especially a kind of fuel atomization device.
Background technology
Evaporation tubular type atomising device belongs to one of fuel atomizer, on large and small type combustion chamber, application is arranged all, operated by rotary motion is at engine main chamber burner inner liner head, Main Function has: the high-temperature fuel gas by the primary zone passes through the evaporation tube wall to fuel Heating in the evaporation tube, fuel oil in the evaporation tube is clashed into and heat by high temperature, high speed inlet air, to reach the effect of EVAP atomizing.Combustion gas by evaporation tubular type atomizer is the high-temperature oil gas gaseous mixture, and easier and primary zone air blending, burning are for efficient, stable burning provides good condition; Commonly used is T-shaped evaporation tube and Г type evaporation tube at present, is single tubular structure, and spray shapes is single direct-injection type cone structure, axial jet speed is large, and for some aero-engine, its burner inner liner compact conformation, head space is little, and mist of oil can be sprayed onto the burner inner liner wall; Because the combustion chamber fuel flow is large, take conventional evaporation tube atomizing effect to descend again.Therefore need good, the short-range atomizer of mist of oil of a kind of atomizing effect, conventional evaporation tube can't satisfy stable, the efficient burning requirement of this combustion chamber.
Summary of the invention
The purpose of this invention is to provide a kind of fuel atomization device, can realize that fuel oil atomizes fully, the short-range target of mist of oil, make flame stabilization, efficient burning, the combustion chamber reliable operation.
Concrete technical scheme of the present invention is: fuel atomization device comprises evaporation tube, air cup and revolve oily device, described evaporation tube is three sections of the Г type each other 90 ° pipes, be provided with in the inside at the fuel outlet place of evaporation tube and revolve oily device, the described outer surface that revolves oily device is provided with 4~6 helicla flutes, evaporation tube outside at the fuel filler place is equipped with the air cup, the rim of a cup of described air cup is concordant with the fuel filler of evaporation tube, sidewall at the air cup is provided with air outlet slit, the air outlet slit of the sidewall setting of described air cup is 6, and described spiral fluted quantity is preferably 5.The mounting means of described air cup and evaporation tube is welding.
The present invention in use, fuel oil and air enter evaporation tube through fuel nozzle, high temperature, high-speed air impact fuel oil, make airborne fuel oil be broken into granule, the heat of high temperature in primary zone is conducted heat by wall and is accelerated adherent EVAP simultaneously, ejects taper rotation gas mixture jet by revolving oily device at last.Simultaneously, portion of air can also enter the air cup, and the sidewall by the air cup enters the primary zone, participates in burning.
The inside at the fuel outlet place of evaporation tube of the present invention is provided with revolves oily device, increased the centrifugal atomizing effect, reduced the axial jet speed of evaporation tube outlet gas mixture, and increased the average area that fuel oil contacts with high-temperature wall surface, the condition that has realized very short mist of oil range has been issued to the sufficient purpose of atomizing, improve evaporation rate, for stable, efficient burning provide advantage, again because evaporation tube is in the primary zone of combustion chamber, operating ambient temperature is higher, this evaporation tube exit arranges the air cup, has realized preferably cooling.Because the air cup normally is welded on the evaporation tube, so effective cooling can also guarantee the reliability of welding.
Description of drawings
Fig. 1 is structural representation of the present invention;
Fig. 2 is the structural representation that revolves oily device.
The specific embodiment
As shown in the figure, fuel atomization device comprises evaporation tube 1, air cup 2 and revolves oily device 3, described evaporation tube 1 is three sections of the Г type each other 90 ° pipes, be provided with in the inside at the fuel outlet place of evaporation tube 1 and revolve oily device 3, the described outer surface that revolves oily device 3 is provided with 4~6 helicla flutes 4, evaporation tube 1 outside at the fuel filler place is equipped with air cup 2, and the rim of a cup of described air cup 2 is concordant with the fuel filler of evaporation tube 1, is provided with air outlet slit at the sidewall of air cup 2.The air outlet slit of the sidewall setting of described air cup is 6, and described spiral fluted quantity is preferably 5.The mounting means of described air cup and evaporation tube is welding.

Claims (4)

1. fuel atomization device, it is characterized in that, fuel atomization device comprises evaporation tube (1), air cup (2) and revolve oily device (3), described evaporation tube (1) is three sections of the Г type each other 90 ° pipes, be provided with in the inside at the fuel outlet place of evaporation tube (1) and revolve oily device (3), the described outer surface that revolves oily device (3) is provided with 4-6 helicla flute (4), evaporation tube (1) outside at the fuel filler place is equipped with air cup (2), the rim of a cup of described air cup (2) is concordant with the fuel filler of evaporation tube (1), and the sidewall of air cup (2) is provided with air outlet slit.
2. fuel atomization device as claimed in claim 1 is characterized in that, the helicla flute (4) that the described outer surface that revolves oily device (3) arranges is 5.
3. fuel atomization device as claimed in claim 1 is characterized in that, the sidewall of described air cup (2) is provided with 6 air outlet slits.
4. fuel atomization device as claimed in claim 1 is characterized in that, described air cup (2) is welding with the mounting means of evaporation tube (1).
CN201210410201XA 2012-10-24 2012-10-24 Fuel oil atomizing device Pending CN102889615A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210410201XA CN102889615A (en) 2012-10-24 2012-10-24 Fuel oil atomizing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210410201XA CN102889615A (en) 2012-10-24 2012-10-24 Fuel oil atomizing device

Publications (1)

Publication Number Publication Date
CN102889615A true CN102889615A (en) 2013-01-23

Family

ID=47533216

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210410201XA Pending CN102889615A (en) 2012-10-24 2012-10-24 Fuel oil atomizing device

Country Status (1)

Country Link
CN (1) CN102889615A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105627365A (en) * 2016-01-19 2016-06-01 西北工业大学 Micro combustion chamber punching type evaporation pipe
CN105952613A (en) * 2016-05-13 2016-09-21 蚌埠市金鹏燃气设备制造有限公司 Low-noise and small-friction gas compressor
CN108151063A (en) * 2017-12-14 2018-06-12 西北工业大学 A kind of tiny engine combustion chamber evaporation tube structure with cyclone
CN109931627A (en) * 2019-04-03 2019-06-25 山东建筑大学 A kind of Micro Turbine Jet Engine fuel oil choked flow atomizing nozzle structure

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1743735A (en) * 2005-09-29 2006-03-08 北京航空航天大学 Evaporation pipe type miniature-small-sized engine combustion chamber
CN202253629U (en) * 2011-08-15 2012-05-30 中国南方航空工业(集团)有限公司 Fuel oil atomizing nozzle and gas turbine with same
CN202852883U (en) * 2012-10-24 2013-04-03 哈尔滨东安发动机(集团)有限公司 Fuel atomization device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1743735A (en) * 2005-09-29 2006-03-08 北京航空航天大学 Evaporation pipe type miniature-small-sized engine combustion chamber
CN202253629U (en) * 2011-08-15 2012-05-30 中国南方航空工业(集团)有限公司 Fuel oil atomizing nozzle and gas turbine with same
CN202852883U (en) * 2012-10-24 2013-04-03 哈尔滨东安发动机(集团)有限公司 Fuel atomization device

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
孙跃中: "蒸发管喷嘴燃油雾化特性试验研究", 《航空动力学报》 *
沈福忱: "航空发动机燃烧室可燃混合气形成过程的数值模拟", 《中国优秀硕士学位论文全文数据库工程科技Ⅱ辑》 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105627365A (en) * 2016-01-19 2016-06-01 西北工业大学 Micro combustion chamber punching type evaporation pipe
CN105952613A (en) * 2016-05-13 2016-09-21 蚌埠市金鹏燃气设备制造有限公司 Low-noise and small-friction gas compressor
CN108151063A (en) * 2017-12-14 2018-06-12 西北工业大学 A kind of tiny engine combustion chamber evaporation tube structure with cyclone
CN109931627A (en) * 2019-04-03 2019-06-25 山东建筑大学 A kind of Micro Turbine Jet Engine fuel oil choked flow atomizing nozzle structure

Similar Documents

Publication Publication Date Title
CN202852883U (en) Fuel atomization device
CN101435585B (en) Gas turbine combined type fuel evaporating and atomizing combustion apparatus
CN102506446B (en) Fuel and air mixing device for low-pollution burning chamber of gas turbine
CN104406197B (en) Low-emission reverse flow combustor adopting radial swirl injection and fuel oil grading schemes
CN106461219B (en) Burner arrangement for a combustion device
US20090255258A1 (en) Pre-filming air-blast fuel injector having a reduced hydraulic spray angle
CN102261673A (en) Hybrid prefilming airblast, prevaporizing, lean-premixing dual-fuel nozzle for gas turbine combustor
CN101206029A (en) Nozzle for minisize gas-turbine combustor
CN102889615A (en) Fuel oil atomizing device
CN109047312A (en) A kind of soil sanitation apparatus and method for based on dystopy thermal desorption
CN108151069B (en) Main combustion zone radial flow combustion chamber and oil-gas mixing method
CN102384489A (en) Small-sized annular combustion chamber with high-capacity heat intensity
CN108151066A (en) Big extension atomization cone angle disc structure
CN109140501B (en) Double-oil-way double-nozzle centrifugal nozzle structure with double-layer air hood
CN102872994B (en) Long-distance air supply mist and smoke spraying machine
CN103175221A (en) Gas-assisted dual-fuel nozzle used for chemical regenerative cycle
CN104674156B (en) A kind of high-speed fuel gas fuel atomizer used for hot spraying
CN104566363A (en) Multi-mechanism composite atomized fuel nozzle structure
RU158820U1 (en) Gas oil burner
CN105783030A (en) Fuel nozzle cylinder spiral pulverization device for aerospace engine and pulverization method of fuel nozzle cylinder spiral pulverization device
CN110594743B (en) Mixed fuel burner for burning low-heat-value waste gas by using high-heat-value waste liquid
CN202715498U (en) Remote air supply mist and smoke spraying machine
CN202546753U (en) Controllable vortex flame diffusion cone
CN104595929A (en) Rotational flow water film cooling type combustion chamber
CN102889614A (en) Direct-flow spraying nozzle

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20130123