KR900016676A - 버너 설비 - Google Patents
버너 설비 Download PDFInfo
- Publication number
- KR900016676A KR900016676A KR1019900005601A KR900005601A KR900016676A KR 900016676 A KR900016676 A KR 900016676A KR 1019900005601 A KR1019900005601 A KR 1019900005601A KR 900005601 A KR900005601 A KR 900005601A KR 900016676 A KR900016676 A KR 900016676A
- Authority
- KR
- South Korea
- Prior art keywords
- burner
- nozzle
- discharge
- fuel
- flow rate
- Prior art date
Links
- 238000009434 installation Methods 0.000 claims description 5
- 238000002485 combustion reaction Methods 0.000 claims 3
- 239000000446 fuel Substances 0.000 claims 3
- 239000012530 fluid Substances 0.000 claims 2
- 239000007789 gas Substances 0.000 claims 1
- 239000007788 liquid Substances 0.000 claims 1
- 239000000203 mixture Substances 0.000 claims 1
- 230000000149 penetrating effect Effects 0.000 claims 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C5/00—Disposition of burners with respect to the combustion chamber or to one another; Mounting of burners in combustion apparatus
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
- F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
-
- 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
- F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
- F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
- F23D14/24—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other at least one of the fluids being submitted to a swirling motion
-
- 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
- F23D14/26—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid with provision for a retention flame
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
Abstract
내용 없음.
Description
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음
제1도는 본 발명에 따른 버너 설비를 통해 가장 간략한 부분을 도시하는 도이다.
Claims (6)
- 연료-공기 혼합물의 주공급 통로와, 연소실 내로 유량을 방출하도록 연결된 상기 통로와, 주공급 통로 (2)를 흐르는 과정에서 제공되며 선회베인(5)에 적합한 적어도 하나의 와류기와. 적어도 하나의 와류기를 관통하는 버너랜스(3)와, 주연료 통로(2)내로 유량을 배출하도록 연결되고 노즐(9)로서 구성된 연료 공급 출구를 갖는 버너 설비로서, 상기 노즐(9)은 적어도 하나의 노즐(9)이 이웃한 선회 베인(5)사이에 제공되는 방법을 사용하여 선회 베인(5) 사이의 영역으로 유량을 방출하도록 연결된 버너 설비에 있어서, 연소실(1)로 부터 막혀진 측부에서 선회 베인(5)은노즈(5a)로서 구성된 연장부를 가지며, 노즐(9)은 노즈(5a)의 영역내에서 방출하도록 연결됨을 특징으로 하는 버너 설비.
- 제1항에 있어서, 노즐(9)의 종축은 연소실(1) 방향으로 기울어져 있으며, 이와 관련하에 버너랜스(3)의 종축에 대해 90°내지 대략 45°범위의 각이 제공됨을 특징으로 하는 버너 설비.
- 제1항에 있어서, 그 제어범위는 적어도 하나의 보조 버너의 도움을 받아 확장됨을 특징으로 하는 버너 설비.
- 제1항에 있어서, 기체, 액체 또는 유체, 분말 연료로 동작될 수 있는 버너 설비.
- 제1항에 있어서, 노즐(9)은 버너 랜스(3)를 통해 공급됨을 특징으로 하는 버너 설비.
- 제1항에 있어서, 노즐(9)은 주 공급 파이프(2)의 외벽을 통해 유체를 방출함을 특징으로 하는 버너 설비.※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH150789 | 1989-04-20 | ||
CH150789-9 | 1989-04-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
KR900016676A true KR900016676A (ko) | 1990-11-14 |
Family
ID=4212057
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1019900005601A KR900016676A (ko) | 1989-04-20 | 1990-04-20 | 버너 설비 |
Country Status (6)
Country | Link |
---|---|
US (1) | US5101633A (ko) |
EP (1) | EP0393484B1 (ko) |
JP (1) | JP2834531B2 (ko) |
KR (1) | KR900016676A (ko) |
CA (1) | CA2014828C (ko) |
DE (1) | DE59000422D1 (ko) |
Families Citing this family (51)
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US5218824A (en) * | 1992-06-25 | 1993-06-15 | Solar Turbines Incorporated | Low emission combustion nozzle for use with a gas turbine engine |
US5407347A (en) * | 1993-07-16 | 1995-04-18 | Radian Corporation | Apparatus and method for reducing NOx, CO and hydrocarbon emissions when burning gaseous fuels |
US5470224A (en) * | 1993-07-16 | 1995-11-28 | Radian Corporation | Apparatus and method for reducing NOx , CO and hydrocarbon emissions when burning gaseous fuels |
WO1995002789A1 (en) * | 1993-07-16 | 1995-01-26 | Radian Corporation | APPARATUS AND METHOD FOR REDUCING NOx, CO AND HYDROCARBON EMISSIONS WHEN BURNING GASEOUS FUELS |
DE4326802A1 (de) * | 1993-08-10 | 1995-02-16 | Abb Management Ag | Brennstofflanze für flüssige und/oder gasförmige Brennstoffe sowie Verfahren zu deren Betrieb |
US5461865A (en) * | 1994-02-24 | 1995-10-31 | United Technologies Corporation | Tangential entry fuel nozzle |
GB9410233D0 (en) * | 1994-05-21 | 1994-07-06 | Rolls Royce Plc | A gas turbine engine combustion chamber |
US5943866A (en) * | 1994-10-03 | 1999-08-31 | General Electric Company | Dynamically uncoupled low NOx combustor having multiple premixers with axial staging |
US5664944A (en) * | 1994-12-05 | 1997-09-09 | The Babcock & Wilcox Company | Low pressure drop vanes for burners and NOX ports |
US5813232A (en) * | 1995-06-05 | 1998-09-29 | Allison Engine Company, Inc. | Dry low emission combustor for gas turbine engines |
US5678499A (en) * | 1995-07-03 | 1997-10-21 | Foster Wheeler Energy Corporation | System for preheating fuel |
JP3939756B2 (ja) * | 1995-09-22 | 2007-07-04 | シーメンス アクチエンゲゼルシヤフト | 特にガスタービン用のバーナ |
GB2305498B (en) * | 1995-09-25 | 2000-03-01 | Europ Gas Turbines Ltd | Fuel injector arrangement for a combustion apparatus |
US5749229A (en) * | 1995-10-13 | 1998-05-12 | General Electric Company | Thermal spreading combustor liner |
US5647215A (en) * | 1995-11-07 | 1997-07-15 | Westinghouse Electric Corporation | Gas turbine combustor with turbulence enhanced mixing fuel injectors |
JP2858104B2 (ja) * | 1996-02-05 | 1999-02-17 | 三菱重工業株式会社 | ガスタービン燃焼器 |
US5755567A (en) * | 1996-02-21 | 1998-05-26 | The Babcock & Wilcox Company | Low vortex spin vanes for burners and overfire air ports |
DE19618058B4 (de) * | 1996-05-06 | 2008-12-04 | Alstom | Brenner |
US5983642A (en) * | 1997-10-13 | 1999-11-16 | Siemens Westinghouse Power Corporation | Combustor with two stage primary fuel tube with concentric members and flow regulating |
US6176087B1 (en) * | 1997-12-15 | 2001-01-23 | United Technologies Corporation | Bluff body premixing fuel injector and method for premixing fuel and air |
US6109038A (en) * | 1998-01-21 | 2000-08-29 | Siemens Westinghouse Power Corporation | Combustor with two stage primary fuel assembly |
DE19905996A1 (de) * | 1999-02-15 | 2000-08-17 | Abb Alstom Power Ch Ag | Brennstofflanze zum Eindüsen von flüssigen und/oder gasförmigen Brennstoffen in eine Brennkammer |
US6820411B2 (en) * | 2002-09-13 | 2004-11-23 | The Boeing Company | Compact, lightweight high-performance lift thruster incorporating swirl-augmented oxidizer/fuel injection, mixing and combustion |
US7007477B2 (en) * | 2004-06-03 | 2006-03-07 | General Electric Company | Premixing burner with impingement cooled centerbody and method of cooling centerbody |
US20060191268A1 (en) * | 2005-02-25 | 2006-08-31 | General Electric Company | Method and apparatus for cooling gas turbine fuel nozzles |
US8062027B2 (en) * | 2005-08-11 | 2011-11-22 | Elster Gmbh | Industrial burner and method for operating an industrial burner |
US7536862B2 (en) * | 2005-09-01 | 2009-05-26 | General Electric Company | Fuel nozzle for gas turbine engines |
AU2007233890B2 (en) * | 2006-03-30 | 2010-07-01 | Ansaldo Energia Ip Uk Limited | Burner arrangement |
US7762077B2 (en) * | 2006-12-05 | 2010-07-27 | Pratt & Whitney Rocketdyne, Inc. | Single-stage hypersonic vehicle featuring advanced swirl combustion |
US20080128547A1 (en) * | 2006-12-05 | 2008-06-05 | Pratt & Whitney Rocketdyne, Inc. | Two-stage hypersonic vehicle featuring advanced swirl combustion |
US7762058B2 (en) * | 2007-04-17 | 2010-07-27 | Pratt & Whitney Rocketdyne, Inc. | Ultra-compact, high performance aerovortical rocket thruster |
US7690192B2 (en) * | 2007-04-17 | 2010-04-06 | Pratt & Whitney Rocketdyne, Inc. | Compact, high performance swirl combustion rocket engine |
CN100526720C (zh) * | 2007-08-20 | 2009-08-12 | 上海诺特飞博燃烧设备有限公司 | 一种确保工业燃烧器稳定燃烧的方法及其装置 |
US8485813B2 (en) * | 2008-01-11 | 2013-07-16 | Hauck Manufacturing Company | Three stage low NOx burner system with controlled stage air separation |
US8312722B2 (en) * | 2008-10-23 | 2012-11-20 | General Electric Company | Flame holding tolerant fuel and air premixer for a gas turbine combustor |
US8333075B2 (en) * | 2009-04-16 | 2012-12-18 | General Electric Company | Gas turbine premixer with internal cooling |
US8677760B2 (en) | 2010-01-06 | 2014-03-25 | General Electric Company | Fuel nozzle with integrated passages and method of operation |
US8919673B2 (en) * | 2010-04-14 | 2014-12-30 | General Electric Company | Apparatus and method for a fuel nozzle |
US8661825B2 (en) * | 2010-12-17 | 2014-03-04 | General Electric Company | Pegless secondary fuel nozzle including a unitary fuel injection manifold |
EP2685160B1 (en) * | 2012-07-10 | 2018-02-21 | Ansaldo Energia Switzerland AG | Premix burner of the multi-cone type for a gas turbine |
US9347378B2 (en) | 2013-05-13 | 2016-05-24 | Solar Turbines Incorporated | Outer premix barrel vent air sweep |
CN103267307B (zh) * | 2013-05-16 | 2015-09-09 | 上海诺特飞博燃烧设备有限公司 | 一种工业燃气燃烧器点火稳燃装置 |
CN105465786A (zh) * | 2015-12-08 | 2016-04-06 | 上海华之邦科技股份有限公司 | 一种适用各种低热值/低压力燃气的低NOx燃烧器 |
US10663171B2 (en) * | 2017-06-19 | 2020-05-26 | General Electric Company | Dual-fuel fuel nozzle with gas and liquid fuel capability |
US11149948B2 (en) * | 2017-08-21 | 2021-10-19 | General Electric Company | Fuel nozzle with angled main injection ports and radial main injection ports |
US11561008B2 (en) * | 2017-08-23 | 2023-01-24 | General Electric Company | Fuel nozzle assembly for high fuel/air ratio and reduced combustion dynamics |
US11480338B2 (en) * | 2017-08-23 | 2022-10-25 | General Electric Company | Combustor system for high fuel/air ratio and reduced combustion dynamics |
WO2020066999A1 (ja) * | 2018-09-25 | 2020-04-02 | 泰工技研工業株式会社 | 多流体気液噴出混合ノズル、バーナー、燃焼機器、ボイラー、内燃機関、動力機器および環境浄化殺菌農園ハウス |
KR102583223B1 (ko) * | 2022-01-28 | 2023-09-25 | 두산에너빌리티 주식회사 | 연소기용 노즐, 연소기 및 이를 포함하는 가스터빈 |
US20250109855A1 (en) * | 2022-02-03 | 2025-04-03 | Nuovo Pignone Tecnologie -S.R.L. | A fuel nozzle for a gas turbine, combustor including the fuel nozzle, and gas turbine |
CN114992640B (zh) * | 2022-05-23 | 2023-05-12 | 江西协成锂业有限公司 | 一种回转窑用多通道混合燃料燃烧器 |
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US2669296A (en) * | 1950-06-14 | 1954-02-16 | Eloise B Stillman | Burner throat with air inlet annulus defined by internally bladed cone |
US3013731A (en) * | 1958-08-06 | 1961-12-19 | Rolls Royce | Fuel injectors for gas turbine engines |
US3076497A (en) * | 1958-11-17 | 1963-02-05 | Gordon & Piatt Inc | Gas burner structure |
US3278125A (en) * | 1964-07-24 | 1966-10-11 | Texaco Inc | Oil burner structure |
US3409231A (en) * | 1967-01-23 | 1968-11-05 | Erwin L. Oehlerking | Swirler for use with burners of the gun type |
US3713588A (en) * | 1970-11-27 | 1973-01-30 | Gen Motors Corp | Liquid fuel spray nozzles with air atomization |
US3904119A (en) * | 1973-12-05 | 1975-09-09 | Avco Corp | Air-fuel spray nozzle |
JPS57187531A (en) * | 1981-05-12 | 1982-11-18 | Hitachi Ltd | Low nox gas turbine burner |
US4426841A (en) * | 1981-07-02 | 1984-01-24 | General Motors Corporation | Gas turbine combustor assembly |
CA1191443A (en) * | 1982-10-13 | 1985-08-06 | Denis Lefebvre | Flame retention head assembly for fuel burners |
EP0169431B1 (en) * | 1984-07-10 | 1990-04-11 | Hitachi, Ltd. | Gas turbine combustor |
CH672541A5 (ko) * | 1986-12-11 | 1989-11-30 | Bbc Brown Boveri & Cie | |
DE3860569D1 (de) * | 1987-01-26 | 1990-10-18 | Siemens Ag | Hybridbrenner fuer vormischbetrieb mit gas und/oder oel, insbesondere fuer gasturbinenanlagen. |
-
1990
- 1990-04-10 EP EP90106905A patent/EP0393484B1/de not_active Expired - Lifetime
- 1990-04-10 DE DE9090106905T patent/DE59000422D1/de not_active Expired - Lifetime
- 1990-04-16 US US07/509,352 patent/US5101633A/en not_active Expired - Fee Related
- 1990-04-18 CA CA002014828A patent/CA2014828C/en not_active Expired - Fee Related
- 1990-04-19 JP JP2101884A patent/JP2834531B2/ja not_active Expired - Lifetime
- 1990-04-20 KR KR1019900005601A patent/KR900016676A/ko not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
EP0393484A1 (de) | 1990-10-24 |
EP0393484B1 (de) | 1992-11-04 |
JP2834531B2 (ja) | 1998-12-09 |
CA2014828A1 (en) | 1990-10-20 |
CA2014828C (en) | 2000-08-01 |
JPH02293510A (ja) | 1990-12-04 |
US5101633A (en) | 1992-04-07 |
DE59000422D1 (de) | 1992-12-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PA0109 | Patent application |
Patent event code: PA01091R01D Comment text: Patent Application Patent event date: 19900420 |
|
PG1501 | Laying open of application | ||
PC1203 | Withdrawal of no request for examination | ||
WITN | Application deemed withdrawn, e.g. because no request for examination was filed or no examination fee was paid |