[go: up one dir, main page]

KR890004744Y1 - Via Burner's Crater - Google Patents

Via Burner's Crater Download PDF

Info

Publication number
KR890004744Y1
KR890004744Y1 KR2019850018143U KR850018143U KR890004744Y1 KR 890004744 Y1 KR890004744 Y1 KR 890004744Y1 KR 2019850018143 U KR2019850018143 U KR 2019850018143U KR 850018143 U KR850018143 U KR 850018143U KR 890004744 Y1 KR890004744 Y1 KR 890004744Y1
Authority
KR
South Korea
Prior art keywords
tank
tube
laser groove
literal
combustion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
KR2019850018143U
Other languages
Korean (ko)
Other versions
KR870010531U (en
Inventor
이동락
Original Assignee
대일공무 주식회사
이동락
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 대일공무 주식회사, 이동락 filed Critical 대일공무 주식회사
Priority to KR2019850018143U priority Critical patent/KR890004744Y1/en
Publication of KR870010531U publication Critical patent/KR870010531U/en
Application granted granted Critical
Publication of KR890004744Y1 publication Critical patent/KR890004744Y1/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/001—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space spraying nozzle combined with forced draft fan in one unit
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36—Details, e.g. burner cooling means, noise reduction means
    • F23D11/38—Nozzles; Cleaning devices therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2202/00—Liquid fuel burners

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Spray-Type Burners (AREA)

Abstract

내용 없음.No content.

Description

경유 버어너의 분화구Via Burner's Crater

제1도는 본 고안의 사용상태를 보인 정체 구성도.1 is a constitution configuration showing the state of use of the present invention.

제2도는 분무기 부분의 확대 단면도.2 is an enlarged cross-sectional view of the sprayer section.

제3도는 종래 노즐에 의한 연소 상태도.3 is a combustion state diagram by a conventional nozzle.

제4도는 본 고안의 분화구에 의한 연소 상태도.4 is a combustion state diagram by the crater of the present invention.

* 도면의 주요부분에 대한 부호의 설명* Explanation of symbols for main parts of the drawings

1 : 오일탱크 2 : 연료이송장치1: Oil tank 2: Fuel feeder

3 : 유출탱크 4 : 리터언관3: outflow tank 4: literian tube

5 : 유출관 6 : 리터언탱크5: outlet pipe 6: liter tank

10 : 분사구 11 : 레이저홈10: injection hole 11: laser groove

12 : 중공부 13 : 상부관12 hollow part 13 upper tube

14 : 하부리터언관 15 : 분출공14: lower literary tube 15: blowout

7 : 송풍장치 8 : 연소실7 blower 8 combustion chamber

8' : 연소공8 ': combustion ball

본 고안은 레이저홈을 타고 흐르는 경유를 압축공기로서 분무화시켜 소형난방 연소용으로 사용되는 경유버어너의 분화구에 관한 것이다.The present invention relates to a crater of diesel fuel burners used for compact heating combustion by atomizing diesel fuel flowing through a laser groove as compressed air.

종래의 오일버어너는 주로 오일을 노즐로서 분산시켰으므로 분출된 오일이 불규칙한 크기의 방울로 부숴져서 완전연소가 되지 않고 그을음이 나는 결점이 있었다.Conventional oil burners mainly disperse oil as nozzles, so that the ejected oil is broken into irregularly sized droplets so that it does not become completely burned and sooted.

본 고안에서는 이와 같은 결점을 개선하고져 경유를 미세한 압력으로 "D"형 분무기의 만곡진 전면의 사이틈에 형성된 레어저홈을 타고 흐르도록 하여 분무기의 중공부와 관통된 분출공의 압축공기로서 흐르는 오일막을 분무화시켜 분무기의 전부에 설치된 연소실에서 연소시킨뒤 연소실의 이중벽에서 공급되는 공기와 혼합되어 연소잔여물이 없이 완전 연소가 되는 것으로 도면에 의거 상세히 설명하면 다음과 같다.In the present invention, the defect is improved and the oil flows through the laser groove formed in the gap between the curved front face of the "D" type sprayer at a minute pressure so that the oil flows as the compressed air of the hollow part of the sprayer and the blown-out hole. Membrane is atomized and burned in the combustion chamber installed in the whole of the atomizer and then mixed with air supplied from the double wall of the combustion chamber to be completely burned without any combustion residues.

오일탱크 (1)에서 공지의 연료이송장치 (2)을 통해 경유가 하부로 공급되는 유출탱크 (3)의 하부유출관 (5)을 "D"형 분사기 (10)의 만곡진 전면의 이중사이틈에 형성된 레어저홈 (11)의 상부관 (13)과 연결시키고 유출탱크 상부의 리터언관 (4)과 레이저홈 하부의 리터언관 (14)을 하부의 리터언팅크 (6)로 연관시키고 공지의 송풍장치 (7)를 통해 공급되는 압축공기는 분사구의 중공부 (12)를 통한 레어저홈의 중앙분출공 (15)과 분사구의 전부에 부설된 연소실 (8)의 이중벽 내측으로 관통된 수개의 연소공 (8')으로 동시에 유출되도록 된 것이다.In the oil tank (1), the lower outlet pipe (5) of the outflow tank (3), through which the gas oil is supplied to the lower part through the known fuel transfer device (2), is placed between the double front of the curved front of the "D" type injector (10). It is connected to the upper tube 13 of the laser groove 11 formed in the gap, and the literal tube 4 of the upper portion of the outflow tank and the literal tube 14 of the lower laser groove are connected to the lower literal tin 6 and known. Compressed air supplied through the blower (7) is a plurality of combustion penetrated inside the double wall of the combustion chamber (8) attached to the central injection hole (15) of the laser groove through the hollow portion (12) of the injection hole and all the injection holes It is going to flow out to the ball 8 'at the same time.

이와 같은 구조로 된 본 고안은 오일탱크 (1)에서 경유를 공급받는 유출탱크 (3)가 상부에 리터언관 (4)이 연결되어 있으므로 탱크내의 일정한 용량으로 인해 경유가 일정하고 미세한 내부압으로 하부유출관 (5)을 통해 "D"형 분사기 (10)의 만곡 전면의 이중사이틈에 형성된 레이저홈 (11)을 타고 하향으로 흐르면 송풍장치 (7)에 의한 압축공기가 분사구의 중공부 (12)와 관통된 분출공 (15)을 통해 분출되면서 레어저홈을 타고 흐르는 경유막을 전부의 연소실 (8)로 분무화시켜 주므로 연소시 연소잔여물이 발생되지 않고 연소실에서 연소시에도 공급되는 압축공기의 일부가 연소실의 이중벽 내측에 관통된 수개의 연소공 (8')으로 동시에 공기를 공급시켜 주므로 충분한 산소공급으로 완전연소가 되고 레이저홈을 타고 흐르는 경유가 압축공기에 의해 분무화되지 않는 것은 레이저홈의 하부를 타고 흘러서 리터언관 (14)을 통해 리터언탱크 (6)로 유입되므로 연료의 낭비가 전혀 없는 것이다.The present invention has a structure such as the outflow tank (3) receiving the light oil from the oil tank (1) is connected to the upper literal tube (4) in the upper portion of the tank due to the constant capacity in the tank is a constant and fine internal pressure When the air flows downward through the outflow pipe 5 through the laser groove 11 formed in the double gap between the curved front surface of the “D” type injector 10, the compressed air by the blower 7 is opened at the hollow portion 12 of the injection hole. ) And through the blow-out hole (15) to spray the gas oil film flowing through the laser groove into all the combustion chamber (8), so that no combustion residues are generated during combustion, and the compressed air supplied during combustion in the combustion chamber Some of them simultaneously supply air to several combustion holes (8 ') penetrated inside the double wall of the combustion chamber, so they are completely burned by sufficient oxygen supply, and light oil flowing through the laser groove is atomized by compressed air. It will do so with no waste of fuel flowing into the frozen liter tank 6 through liter eongwan 14 flows riding the lower portion of the laser groove.

Claims (1)

오일탱크 (1)에서 공지의 연료이송장치 (2)을 통해 경유가 하부로 공급되는 유출탱크 (3)의 하부유출관 (5) "D"형 분사기 (10)의 만곡진 전면의 이중사이틈에 형성된 레이저홈 (11)의 상부관 (13)과 연결시키고 유출탱크 상부의 리터언관 (4)과 레이저홈 하부의 리터언관 (14)을 하부의 리터언탱크 (6)로 연관시키고 공지의 송풍장치 (8)을 통해 공급되는 압축공기는 분사구의 중공부 (12)를 통한 레어저홈의 중앙 분출공 (15)과 분사구의 전부에 부설된 연소실 (8)의 이중벽 내측으로 관통된 수개의 연소공 (8')으로 동시에 유출되도록 된 경유버어너의 분화구.In the oil tank 1, a double gap between the lower outflow pipe 5 of the outflow tank 3 in which the diesel oil is supplied to the lower portion through the known fuel transfer device 2 at the curved front of the “D” type injector 10. Connected to the upper tube 13 of the laser groove 11 formed in the upper part of the tank, and the literal tube 4 of the upper portion of the outflow tank and the literal tube 14 of the lower portion of the laser groove are connected to the lower literal tank 6 and a known blowing Compressed air supplied through the apparatus 8 is a plurality of combustion holes penetrating into the central wall 15 of the laser groove through the hollow portion 12 of the injection hole and inside the double wall of the combustion chamber 8 installed in all of the injection holes. A crater of diesel burners intended to flow out simultaneously with (8 ').
KR2019850018143U 1985-12-30 1985-12-30 Via Burner's Crater Expired KR890004744Y1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR2019850018143U KR890004744Y1 (en) 1985-12-30 1985-12-30 Via Burner's Crater

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR2019850018143U KR890004744Y1 (en) 1985-12-30 1985-12-30 Via Burner's Crater

Publications (2)

Publication Number Publication Date
KR870010531U KR870010531U (en) 1987-07-11
KR890004744Y1 true KR890004744Y1 (en) 1989-07-20

Family

ID=19247727

Family Applications (1)

Application Number Title Priority Date Filing Date
KR2019850018143U Expired KR890004744Y1 (en) 1985-12-30 1985-12-30 Via Burner's Crater

Country Status (1)

Country Link
KR (1) KR890004744Y1 (en)

Also Published As

Publication number Publication date
KR870010531U (en) 1987-07-11

Similar Documents

Publication Publication Date Title
KR890017492A (en) Fuel injection burner and combustion method
JP4260948B2 (en) Burners and combustion methods and methods for their use
KR100234572B1 (en) Narrow spray angle liquid fuel atomizers for combustion
US4222243A (en) Fuel burners for gas turbine engines
KR870000983B1 (en) Combustion device of liquid fuel
GB1445795A (en) Method of and apparatus for burning fuel
US2259011A (en) Atomizer for liquid fuels
JPH074619A (en) Oxygen - fuel burner mechanism and its operation
JP2003021309A (en) Multi-fluid spraying nozzle and combustion method with addition of water
US3739989A (en) Duct burner for operation with liquid or gaseous fuels
US4014639A (en) Recirculating vortex burner
GB1408021A (en) Incinerator
US4568019A (en) Internal burner type flame spray method and apparatus having material introduction into an overexpanded gas stream
US5449288A (en) Aspirated wick atomizer nozzle
US3693887A (en) Method and apparatus for gasifying liquid fuels and effecting a complete combustion thereof
RU2040731C1 (en) Fuel gasification burner
KR890004744Y1 (en) Via Burner's Crater
US4634370A (en) Flare
US4174201A (en) Burner heads for waste combustible gas
JPS62500118A (en) Burner and combustion method for liquid waste
US3610536A (en) Combination gas/oil burner
US5520535A (en) Burner apparatus
CA2156248A1 (en) Apparatus for the vaporization of fuels and supply of air for combustion
KR950019362A (en) Method and apparatus for combusting fluid fuel comprising solid particles
CN1158950A (en) Port burner structure of oil combustion equipment

Legal Events

Date Code Title Description
A201 Request for examination
UA0108 Application for utility model registration

Comment text: Application for Utility Model Registration

Patent event code: UA01011R08D

Patent event date: 19851230

UA0201 Request for examination

Patent event date: 19851230

Patent event code: UA02012R01D

Comment text: Request for Examination of Application

UG1501 Laying open of application
E902 Notification of reason for refusal
UE0902 Notice of grounds for rejection

Comment text: Notification of reason for refusal

Patent event code: UE09021S01D

Patent event date: 19890124

UG1604 Publication of application

Patent event code: UG16041S01I

Comment text: Decision on Publication of Application

Patent event date: 19890620

E701 Decision to grant or registration of patent right
UE0701 Decision of registration

Patent event date: 19891017

Comment text: Decision to Grant Registration

Patent event code: UE07011S01D

REGI Registration of establishment
UR0701 Registration of establishment

Patent event date: 19891130

Patent event code: UR07011E01D

Comment text: Registration of Establishment

UR1002 Payment of registration fee

Start annual number: 1

End annual number: 3

Payment date: 19891130

UR1001 Payment of annual fee

Payment date: 19930107

Start annual number: 4

End annual number: 5

UR1001 Payment of annual fee

Payment date: 19940113

Start annual number: 6

End annual number: 6

FPAY Annual fee payment

Payment date: 19950314

Year of fee payment: 8

UR1001 Payment of annual fee

Payment date: 19950314

Start annual number: 7

End annual number: 8

LAPS Lapse due to unpaid annual fee
UC1903 Unpaid annual fee