AU593858B2 - Gas turbine engine augmentor - Google Patents
Gas turbine engine augmentor Download PDFInfo
- Publication number
- AU593858B2 AU593858B2 AU65626/86A AU6562686A AU593858B2 AU 593858 B2 AU593858 B2 AU 593858B2 AU 65626/86 A AU65626/86 A AU 65626/86A AU 6562686 A AU6562686 A AU 6562686A AU 593858 B2 AU593858 B2 AU 593858B2
- Authority
- AU
- Australia
- Prior art keywords
- pilot section
- annular
- section
- fuel
- gutters
- 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.)
- Ceased
Links
- 238000005516 engineering process Methods 0.000 claims description 3
- 239000000446 fuel Substances 0.000 description 28
- 239000000203 mixture Substances 0.000 description 11
- 238000002485 combustion reaction Methods 0.000 description 4
- 230000003134 recirculating effect Effects 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 description 1
- 230000037406 food intake Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
Classifications
-
- 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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
-
- 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
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
- F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
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)
- Testing Of Engines (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Control Of Combustion (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US80164285A | 1985-11-25 | 1985-11-25 | |
| US801642 | 1985-11-25 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| AU6562686A AU6562686A (en) | 1987-05-28 |
| AU593858B2 true AU593858B2 (en) | 1990-02-22 |
Family
ID=25181670
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AU65626/86A Ceased AU593858B2 (en) | 1985-11-25 | 1986-11-21 | Gas turbine engine augmentor |
Country Status (9)
| Country | Link |
|---|---|
| EP (1) | EP0224429B1 (enExample) |
| JP (1) | JPS62129528A (enExample) |
| KR (1) | KR940008267B1 (enExample) |
| CN (1) | CN1007640B (enExample) |
| AU (1) | AU593858B2 (enExample) |
| CA (1) | CA1281554C (enExample) |
| DE (1) | DE3675896D1 (enExample) |
| IL (1) | IL80634A (enExample) |
| YU (2) | YU201686A (enExample) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IL93630A0 (en) * | 1989-03-27 | 1990-12-23 | Gen Electric | Flameholder for gas turbine engine afterburner |
| JP5375433B2 (ja) * | 2009-08-21 | 2013-12-25 | 株式会社Ｉｈｉ | アフタバーナ及び航空機エンジン |
| US20110219776A1 (en) * | 2010-03-15 | 2011-09-15 | General Electric Company | Aerodynamic flame stabilizer |
| CN102200292B (zh) * | 2010-03-26 | 2015-01-21 | 北京航空航天大学 | 带凹腔的支板火焰稳定装置及火焰稳定方法 |
| JP2013181473A (ja) * | 2012-03-02 | 2013-09-12 | Ihi Corp | アフタバーナ及び航空機エンジン |
| CN103884024B (zh) * | 2014-04-03 | 2016-01-20 | 北京航空航天大学 | 一种能够组织燃烧并将火焰传导到外涵道气流的联焰装置 |
| CN105650642B (zh) * | 2016-02-04 | 2019-04-30 | 中国科学院工程热物理研究所 | 一种可形成低速区的喷嘴、喷嘴阵列和燃烧器 |
| CN105841191B (zh) * | 2016-03-30 | 2018-07-06 | 中国科学院工程热物理研究所 | 一种v型火焰稳定器尾缘结构 |
| CN106678877A (zh) * | 2016-11-15 | 2017-05-17 | 西北工业大学 | 一种加有v型槽环形火焰稳定器的一体化加力燃烧室 |
| CN110486148A (zh) * | 2017-08-29 | 2019-11-22 | 熵零技术逻辑工程院集团股份有限公司 | 一种加力燃烧室高负荷响应发动机 |
| CN109611887B (zh) * | 2018-11-01 | 2020-10-09 | 中国航发沈阳发动机研究所 | 一种燃烧装置 |
| CN114992674B (zh) * | 2022-06-20 | 2024-03-19 | 中国航发贵阳发动机设计研究所 | 一种外置式接力点火及起动供油装置 |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4423595A (en) * | 1982-05-27 | 1984-01-03 | United Technologies Corporation | Augmentor residual fuel drain apparatus |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB744178A (en) * | 1953-03-26 | 1956-02-01 | Rolls Royce | Improvements relating to combustion equipment of gas-turbine engines |
| FR1199822A (fr) * | 1958-07-11 | 1959-12-16 | Nord Aviat | Perfectionnements aux stabilisateurs de flammes dans les propulseurs à réaction |
| GB886700A (en) * | 1959-11-05 | 1962-01-10 | Rolls Royce | Reheat combustion equipment for jet propulsion engines |
| FR2429326A1 (fr) * | 1978-06-22 | 1980-01-18 | Snecma | Perfectionnements aux dispositifs accroche-flammes pour chambres de combustion, notamment pour canaux de post-combustion de turboreacteurs |
-
1986
- 1986-10-27 CA CA000521471A patent/CA1281554C/en not_active Expired - Lifetime
- 1986-11-14 IL IL80634A patent/IL80634A/xx not_active IP Right Cessation
- 1986-11-20 DE DE8686630174T patent/DE3675896D1/de not_active Expired - Lifetime
- 1986-11-20 EP EP86630174A patent/EP0224429B1/en not_active Expired - Lifetime
- 1986-11-21 AU AU65626/86A patent/AU593858B2/en not_active Ceased
- 1986-11-25 YU YU02016/86A patent/YU201686A/xx unknown
- 1986-11-25 CN CN86108062A patent/CN1007640B/zh not_active Expired
- 1986-11-25 JP JP61280537A patent/JPS62129528A/ja active Granted
- 1986-11-25 KR KR1019860009936A patent/KR940008267B1/ko not_active Expired - Lifetime
- 1986-11-28 YU YU02036/86A patent/YU203686A/xx unknown
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4423595A (en) * | 1982-05-27 | 1984-01-03 | United Technologies Corporation | Augmentor residual fuel drain apparatus |
Also Published As
| Publication number | Publication date |
|---|---|
| DE3675896D1 (de) | 1991-01-10 |
| EP0224429A3 (en) | 1988-09-14 |
| JPH0587654B2 (enExample) | 1993-12-17 |
| YU201686A (en) | 1990-06-30 |
| KR870005163A (ko) | 1987-06-05 |
| IL80634A0 (en) | 1987-02-27 |
| YU203686A (en) | 1990-06-30 |
| CN1007640B (zh) | 1990-04-18 |
| EP0224429B1 (en) | 1990-11-28 |
| KR940008267B1 (ko) | 1994-09-09 |
| JPS62129528A (ja) | 1987-06-11 |
| AU6562686A (en) | 1987-05-28 |
| EP0224429A2 (en) | 1987-06-03 |
| IL80634A (en) | 1991-12-15 |
| CA1281554C (en) | 1991-03-19 |
| CN86108062A (zh) | 1987-07-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3374624A (en) | Gas turbine engine combustion equipment | |
| US5123248A (en) | Low emissions combustor | |
| EP0153842B1 (en) | Combustion equipment | |
| US3299632A (en) | Combustion chamber for a gas turbine engine | |
| AU593858B2 (en) | Gas turbine engine augmentor | |
| US6968692B2 (en) | Fuel premixing module for gas turbine engine combustor | |
| US4271674A (en) | Premix combustor assembly | |
| US5396761A (en) | Gas turbine engine ignition flameholder with internal impingement cooling | |
| CA1319515C (en) | Gas-cooled flameholder assembly | |
| US5267851A (en) | Swirl gutters for isolating flow fields for combustion enhancement at non-baseload operating conditions | |
| GB1522826A (en) | Gas turbine engine afterburner flameholders | |
| GB1427146A (en) | Combustion apparatus for gas turbine engines | |
| JPS5826498B2 (ja) | ガスタ−ビンエンジン用燃焼装置 | |
| US6729141B2 (en) | Microturbine with auxiliary air tubes for NOx emission reduction | |
| US2977760A (en) | Annular combustion chambers for use with compressors capable of discharging combustion supporting medium with a rotary swirl through an annular outlet | |
| GB1180524A (en) | Gas Turbine Jet Engine of the By-Pass Type | |
| US4765136A (en) | Gas turbine engine augmentor | |
| US6141954A (en) | Premixing fuel injector with improved flame disgorgement capacity | |
| US4903492A (en) | Dilution air dispensing apparatus | |
| US4203285A (en) | Partial swirl augmentor for a turbofan engine | |
| US7568346B2 (en) | Method and apparatus for assembling a flameholder for an augmenter | |
| US4539811A (en) | Multi-port dump combustor | |
| US4179881A (en) | Premix combustor assembly | |
| US4170111A (en) | Thrust augmentor | |
| US4145879A (en) | Modified vorbix burner concept |