PL2671028T3 - Wtryskiwacz komory spalania turbiny gazowej z podwójnym obwodem paliwa i komora spalania wyposażona w co najmniej jeden taki wtryskiwacz - Google Patents
Wtryskiwacz komory spalania turbiny gazowej z podwójnym obwodem paliwa i komora spalania wyposażona w co najmniej jeden taki wtryskiwaczInfo
- Publication number
- PL2671028T3 PL2671028T3 PL12706638T PL12706638T PL2671028T3 PL 2671028 T3 PL2671028 T3 PL 2671028T3 PL 12706638 T PL12706638 T PL 12706638T PL 12706638 T PL12706638 T PL 12706638T PL 2671028 T3 PL2671028 T3 PL 2671028T3
- Authority
- PL
- Poland
- Prior art keywords
- injector
- combustion chamber
- gas turbine
- dual fuel
- fuel circuit
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title 2
- 230000009977 dual effect Effects 0.000 title 1
- 239000000446 fuel Substances 0.000 title 1
Classifications
-
- 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
-
- 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
-
- 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
- F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
- F23D11/101—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet
- F23D11/102—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet in an internal mixing chamber
- F23D11/103—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet in an internal mixing chamber with means creating a swirl inside the mixing chamber
-
- 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
- F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
- F23D11/106—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting at the burner outlet
- F23D11/107—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting at the burner outlet at least one of both being subjected to a swirling motion
-
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
- F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
- F23D2900/00014—Pilot burners specially adapted for ignition of main burners in furnaces or gas turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
- F23D2900/00015—Pilot burners specially adapted for low load or transient conditions, e.g. for increasing stability
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
- F23D2900/00016—Preventing or reducing deposit build-up on burner parts, e.g. from carbon
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
- Jet Pumps And Other Pumps (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1150807A FR2971039B1 (fr) | 2011-02-02 | 2011-02-02 | Injecteur de chambre de combustion de turbine a gaz a double circuit de carburant et chambre de combustion equipee d'au moins un tel injecteur |
| EP12706638.9A EP2671028B1 (fr) | 2011-02-02 | 2012-01-27 | Injecteur de chambre de combustion de turbine a gaz a double circuit de carburant et chambre de combustion equipee d'au moins un tel injecteur |
| PCT/FR2012/050177 WO2012104525A1 (fr) | 2011-02-02 | 2012-01-27 | Injecteur de chambre de combustion de turbine a gaz a double circuit de carburant et chambre de combustion equipee d'au moins un tel injecteur |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| PL2671028T3 true PL2671028T3 (pl) | 2018-11-30 |
Family
ID=45774260
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL12706638T PL2671028T3 (pl) | 2011-02-02 | 2012-01-27 | Wtryskiwacz komory spalania turbiny gazowej z podwójnym obwodem paliwa i komora spalania wyposażona w co najmniej jeden taki wtryskiwacz |
Country Status (11)
| Country | Link |
|---|---|
| US (1) | US9347667B2 (pl) |
| EP (1) | EP2671028B1 (pl) |
| JP (1) | JP5985514B2 (pl) |
| KR (1) | KR101877591B1 (pl) |
| CN (1) | CN103354890B (pl) |
| CA (1) | CA2825864C (pl) |
| ES (1) | ES2686560T3 (pl) |
| FR (1) | FR2971039B1 (pl) |
| PL (1) | PL2671028T3 (pl) |
| RU (1) | RU2584741C2 (pl) |
| WO (1) | WO2012104525A1 (pl) |
Families Citing this family (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2996288B1 (fr) * | 2012-10-01 | 2014-09-12 | Turbomeca | Injecteur a double circuit de chambre de combustion de turbomachine. |
| FR2996289B1 (fr) * | 2012-10-01 | 2018-10-12 | Turbomeca | Chambre de combustion comprenant un tube a flamme fixe au moyen de trois elements de centrage. |
| FR3001497B1 (fr) * | 2013-01-29 | 2016-05-13 | Turbomeca | Ensemble de combustion de turbomachine comprenant un circuit d alimentation de carburant ameliore |
| FR3001525B1 (fr) * | 2013-01-29 | 2016-12-09 | Turbomeca | Procede de gestion de la consommation de carburant d un ensemble bimoteur et ensemble associe |
| US20150354459A1 (en) * | 2013-02-01 | 2015-12-10 | Hamilton Sundstrand Corporation | Fuel injector for high altitude starting and operation of a gas turbine engine |
| US9404422B2 (en) * | 2013-05-23 | 2016-08-02 | Honeywell International Inc. | Gas turbine fuel injector having flow guide for receiving air flow |
| EP3022492A4 (en) * | 2013-07-15 | 2017-02-22 | Hamilton Sundstrand Corporation | Combustion system, apparatus and method |
| US9625156B2 (en) * | 2013-10-30 | 2017-04-18 | Honeywell International Inc. | Gas turbine engines having fuel injector shrouds with interior ribs |
| FR3017693B1 (fr) * | 2014-02-19 | 2019-07-26 | Safran Helicopter Engines | Chambre de combustion de turbomachine |
| CN104019475A (zh) * | 2014-06-23 | 2014-09-03 | 叶祖湘 | 一种装有燃烧机系统的大小灶具 |
| FR3050255B1 (fr) * | 2016-04-13 | 2019-10-25 | Safran Helicopter Engines | Injecteurs ameliores pour chambre de combustion de turbine a gaz |
| FR3059047B1 (fr) * | 2016-11-21 | 2020-08-28 | Safran Helicopter Engines | Injecteur de chambre de combustion pour une turbomachine et son procede de fabrication |
| FR3067444B1 (fr) * | 2017-06-12 | 2019-12-27 | Safran Helicopter Engines | Architecture de combustion de carburant de turbomachine comportant des moyens de deflexion |
| FR3068113B1 (fr) | 2017-06-27 | 2019-08-23 | Safran Helicopter Engines | Injecteur de carburant a jet plat pour une turbomachine d'aeronef |
| US10816211B2 (en) | 2017-08-25 | 2020-10-27 | Honeywell International Inc. | Axially staged rich quench lean combustion system |
| FR3081211B1 (fr) * | 2018-05-16 | 2021-02-26 | Safran Aircraft Engines | Ensemble pour une chambre de combustion de turbomachine |
| CN109185923B (zh) * | 2018-08-03 | 2023-09-12 | 新奥能源动力科技（上海）有限公司 | 一种燃烧室头部装置、燃烧室及燃气轮机 |
| CN109185924B (zh) * | 2018-08-03 | 2023-09-12 | 新奥能源动力科技（上海）有限公司 | 燃烧室的头部装置、燃烧室及燃气轮机 |
| FR3087250B1 (fr) | 2018-10-11 | 2020-09-25 | Safran Helicopter Engines | Injecteur de carburant monobloc a jet plat pour une turbomachine d'aeronef et son procede de fabrication |
| RU187491U1 (ru) * | 2018-11-15 | 2019-03-11 | Публичное Акционерное Общество "Одк-Сатурн" | Испарительная камера сгорания газотурбинного двигателя |
| FR3099231B1 (fr) | 2019-07-24 | 2022-08-12 | Safran Helicopter Engines | Injecteur de carburant a circuit de purge pour une turbomachine d’aeronef |
| US11988386B2 (en) * | 2021-12-03 | 2024-05-21 | Honeywell International Inc. | Gas turbine engine injector module with thermally coupled fuel lines having respective outlets |
| US12117174B2 (en) * | 2023-02-14 | 2024-10-15 | Collins Engine Nozzles, Inc. | Combustor section support structures |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4817389A (en) * | 1987-09-24 | 1989-04-04 | United Technologies Corporation | Fuel injection system |
| SU1560923A1 (ru) * | 1988-06-29 | 1990-04-30 | Войсковая часть 27177 | Камера сгорани газотурбинного двигател |
| US7513116B2 (en) * | 2004-11-09 | 2009-04-07 | Woodward Fst, Inc. | Gas turbine engine fuel injector having a fuel swirler |
| JP3958767B2 (ja) * | 2005-03-18 | 2007-08-15 | 川崎重工業株式会社 | ガスタービン燃焼器およびその着火方法 |
| US7624576B2 (en) * | 2005-07-18 | 2009-12-01 | Pratt & Whitney Canada Corporation | Low smoke and emissions fuel nozzle |
| FR2896030B1 (fr) * | 2006-01-09 | 2008-04-18 | Snecma Sa | Refroidissement d'un dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur |
| US20070193272A1 (en) * | 2006-02-21 | 2007-08-23 | Woodward Fst, Inc. | Gas turbine engine fuel injector |
| FR2906868B1 (fr) | 2006-10-06 | 2011-11-18 | Snecma | Injecteur de carburant pour chambre de combustion de moteur a turbine a gaz |
| US7908864B2 (en) * | 2006-10-06 | 2011-03-22 | General Electric Company | Combustor nozzle for a fuel-flexible combustion system |
| FR2911667B1 (fr) | 2007-01-23 | 2009-10-02 | Snecma Sa | Systeme d'injection de carburant a double injecteur. |
| US9513009B2 (en) * | 2009-02-18 | 2016-12-06 | Rolls-Royce Plc | Fuel nozzle having aerodynamically shaped helical turning vanes |
-
2011
- 2011-02-02 FR FR1150807A patent/FR2971039B1/fr active Active
-
2012
- 2012-01-27 WO PCT/FR2012/050177 patent/WO2012104525A1/fr active Application Filing
- 2012-01-27 PL PL12706638T patent/PL2671028T3/pl unknown
- 2012-01-27 CN CN201280007105.9A patent/CN103354890B/zh active Active
- 2012-01-27 KR KR1020137022157A patent/KR101877591B1/ko active Active
- 2012-01-27 JP JP2013552244A patent/JP5985514B2/ja not_active Expired - Fee Related
- 2012-01-27 ES ES12706638.9T patent/ES2686560T3/es active Active
- 2012-01-27 EP EP12706638.9A patent/EP2671028B1/fr active Active
- 2012-01-27 US US13/982,608 patent/US9347667B2/en active Active
- 2012-01-27 CA CA2825864A patent/CA2825864C/fr not_active Expired - Fee Related
- 2012-01-27 RU RU2013139354/06A patent/RU2584741C2/ru active
Also Published As
| Publication number | Publication date |
|---|---|
| JP5985514B2 (ja) | 2016-09-06 |
| CN103354890B (zh) | 2016-06-29 |
| FR2971039B1 (fr) | 2013-01-11 |
| KR101877591B1 (ko) | 2018-07-12 |
| EP2671028A1 (fr) | 2013-12-11 |
| RU2584741C2 (ru) | 2016-05-20 |
| CA2825864A1 (fr) | 2012-09-09 |
| EP2671028B1 (fr) | 2018-07-25 |
| FR2971039A1 (fr) | 2012-08-03 |
| ES2686560T3 (es) | 2018-10-18 |
| WO2012104525A1 (fr) | 2012-08-09 |
| JP2014504696A (ja) | 2014-02-24 |
| KR20140008350A (ko) | 2014-01-21 |
| US20130305726A1 (en) | 2013-11-21 |
| RU2013139354A (ru) | 2015-03-10 |
| CA2825864C (fr) | 2019-05-21 |
| US9347667B2 (en) | 2016-05-24 |
| CN103354890A (zh) | 2013-10-16 |
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