CN106461221A8 - 具有分级的沿轴向偏移的燃烧的燃烧器 - Google Patents
具有分级的沿轴向偏移的燃烧的燃烧器 Download PDFInfo
- Publication number
- CN106461221A8 CN106461221A8 CN201580017217.6A CN201580017217A CN106461221A8 CN 106461221 A8 CN106461221 A8 CN 106461221A8 CN 201580017217 A CN201580017217 A CN 201580017217A CN 106461221 A8 CN106461221 A8 CN 106461221A8
- Authority
- CN
- China
- Prior art keywords
- mixer
- burner
- burning
- classification
- 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.)
- Granted
Links
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
- F23R3/346—Feeding into different combustion zones for staged combustion
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- 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
-
- 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
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/10—Air inlet arrangements for primary air
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/26—Controlling the air flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/35—Combustors or associated equipment
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00015—Trapped vortex combustion chambers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Abstract
在一些方面中,一种燃气涡轮燃烧器组件围绕纵轴线布置。燃气涡轮燃烧器包括第一燃料/空气混合器组件,混合器组件包括第一燃料喷射器和多个第一混合器元件,各个混合器元件限定具有第一平面中的出口的穿过其的空气流通路。第二燃料/空气混合器组件包括第二燃料喷射器和多个第二混合器元件,并且各个第二混合器元件限定具有从第一平面沿纵向偏移的第二平面中的出口的穿过其的空气流通路。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/167,594 US9587833B2 (en) | 2014-01-29 | 2014-01-29 | Combustor with staged, axially offset combustion |
US14/167,594 | 2014-01-29 | ||
PCT/US2015/011419 WO2015116384A1 (en) | 2014-01-29 | 2015-01-14 | Combustor with staged, axially offset combustion |
Publications (3)
Publication Number | Publication Date |
---|---|
CN106461221A CN106461221A (zh) | 2017-02-22 |
CN106461221A8 true CN106461221A8 (zh) | 2017-06-30 |
CN106461221B CN106461221B (zh) | 2019-06-28 |
Family
ID=52432987
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201580017217.6A Active CN106461221B (zh) | 2014-01-29 | 2015-01-14 | 具有分级的沿轴向偏移的燃烧的燃烧器 |
Country Status (4)
Country | Link |
---|---|
US (2) | US9587833B2 (zh) |
EP (1) | EP3099979B1 (zh) |
CN (1) | CN106461221B (zh) |
WO (1) | WO2015116384A1 (zh) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105899878B (zh) | 2013-06-18 | 2018-11-13 | 伍德沃德有限公司 | 燃气涡轮燃烧室组件及发动机及相关联的操作方法 |
US9587833B2 (en) | 2014-01-29 | 2017-03-07 | Woodward, Inc. | Combustor with staged, axially offset combustion |
CN106796031B (zh) | 2014-08-18 | 2022-07-08 | 伍德沃德有限公司 | 火炬式点火器 |
US10364751B2 (en) * | 2015-08-03 | 2019-07-30 | Delavan Inc | Fuel staging |
US10859269B2 (en) | 2017-03-31 | 2020-12-08 | Delavan Inc. | Fuel injectors for multipoint arrays |
US10584877B2 (en) * | 2017-04-28 | 2020-03-10 | DOOSAN Heavy Industries Construction Co., LTD | Device to correct flow non-uniformity within a combustion system |
US11181274B2 (en) | 2017-08-21 | 2021-11-23 | General Electric Company | Combustion system and method for attenuation of combustion dynamics in a gas turbine engine |
US10724432B2 (en) | 2017-11-07 | 2020-07-28 | General Electric Company | Integrated fuel cell and engine combustor assembly |
US10935245B2 (en) | 2018-11-20 | 2021-03-02 | General Electric Company | Annular concentric fuel nozzle assembly with annular depression and radial inlet ports |
US11156360B2 (en) | 2019-02-18 | 2021-10-26 | General Electric Company | Fuel nozzle assembly |
US11421601B2 (en) | 2019-03-28 | 2022-08-23 | Woodward, Inc. | Second stage combustion for igniter |
US11174792B2 (en) | 2019-05-21 | 2021-11-16 | General Electric Company | System and method for high frequency acoustic dampers with baffles |
US11156164B2 (en) | 2019-05-21 | 2021-10-26 | General Electric Company | System and method for high frequency accoustic dampers with caps |
US11828465B2 (en) | 2022-01-21 | 2023-11-28 | General Electric Company | Combustor fuel assembly |
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US3905192A (en) | 1974-08-29 | 1975-09-16 | United Aircraft Corp | Combustor having staged premixing tubes |
US5749219A (en) | 1989-11-30 | 1998-05-12 | United Technologies Corporation | Combustor with first and second zones |
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JPH0579629A (ja) | 1991-09-19 | 1993-03-30 | Hitachi Ltd | 燃焼器およびその運転方法 |
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DE4228816C2 (de) | 1992-08-29 | 1998-08-06 | Mtu Muenchen Gmbh | Brenner für Gasturbinentriebwerke |
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-
2014
- 2014-01-29 US US14/167,594 patent/US9587833B2/en active Active
-
2015
- 2015-01-14 EP EP15701653.6A patent/EP3099979B1/en active Active
- 2015-01-14 WO PCT/US2015/011419 patent/WO2015116384A1/en active Application Filing
- 2015-01-14 CN CN201580017217.6A patent/CN106461221B/zh active Active
-
2017
- 2017-01-20 US US15/411,274 patent/US10006637B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US10006637B2 (en) | 2018-06-26 |
CN106461221A (zh) | 2017-02-22 |
CN106461221B (zh) | 2019-06-28 |
US20170328570A1 (en) | 2017-11-16 |
US20150211742A1 (en) | 2015-07-30 |
EP3099979B1 (en) | 2019-03-13 |
US9587833B2 (en) | 2017-03-07 |
WO2015116384A1 (en) | 2015-08-06 |
EP3099979A1 (en) | 2016-12-07 |
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Legal Events
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
CI01 | Publication of corrected invention patent application | ||
CI01 | Publication of corrected invention patent application |
Correction item: Priority Correct: 14/167,594 2014.01.29 US Number: 08 Volume: 33 |
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CI02 | Correction of invention patent application | ||
CI02 | Correction of invention patent application |
Correction item: Priority Correct: 14/167,594 2014.01.29 US Number: 08 Page: The title page Volume: 33 |
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GR01 | Patent grant |