IN2015DN00981A - - Google Patents
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- Publication number
- IN2015DN00981A IN2015DN00981A IN981DEN2015A IN2015DN00981A IN 2015DN00981 A IN2015DN00981 A IN 2015DN00981A IN 981DEN2015 A IN981DEN2015 A IN 981DEN2015A IN 2015DN00981 A IN2015DN00981 A IN 2015DN00981A
- Authority
- IN
- India
- Prior art keywords
- tip
- injector
- tube
- dual connection
- transfer
- Prior art date
Links
- 230000009977 dual effect Effects 0.000 abstract 3
- 239000000446 fuel Substances 0.000 abstract 2
- 238000002347 injection Methods 0.000 abstract 2
- 239000007924 injection Substances 0.000 abstract 2
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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F02C7/228—Dividing fuel between various burners
-
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of 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
-
- 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
- F23R3/36—Supply of different fuels
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F02C7/222—Fuel flow conduits, e.g. manifolds
-
- 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
- F05D2270/00—Control
- F05D2270/30—Control parameters, e.g. input parameters
- F05D2270/31—Fuel schedule for stage combustors
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
- Feeding And Controlling Fuel (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1257622A FR2994217B1 (fr) | 2012-08-06 | 2012-08-06 | Rampe d'injection modulaire a double circuit |
| PCT/FR2013/051822 WO2014023892A1 (fr) | 2012-08-06 | 2013-07-29 | Rampe d'injection modulaire a double circuit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IN2015DN00981A true IN2015DN00981A (h) | 2015-06-12 |
Family
ID=47427360
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IN981DEN2015 IN2015DN00981A (h) | 2012-08-06 | 2013-07-29 |
Country Status (12)
| Country | Link |
|---|---|
| US (1) | US9689313B2 (h) |
| EP (1) | EP2880285B8 (h) |
| JP (1) | JP6147857B2 (h) |
| KR (1) | KR102077358B1 (h) |
| CN (1) | CN104583564B (h) |
| CA (1) | CA2880859C (h) |
| ES (1) | ES2612164T3 (h) |
| FR (1) | FR2994217B1 (h) |
| IN (1) | IN2015DN00981A (h) |
| PL (1) | PL2880285T3 (h) |
| RU (1) | RU2630053C2 (h) |
| WO (1) | WO2014023892A1 (h) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2910752B1 (en) * | 2014-02-19 | 2018-04-25 | United Technologies Corporation | Fuel manifold fitting with integral support for a gas turbine engine and method of mounting a fuel supply manifold assembly |
| WO2016001301A1 (en) * | 2014-07-02 | 2016-01-07 | Nuovo Pignone Srl | Fuel distribution device, gas turbine engine and mounting method |
| US10508600B2 (en) * | 2016-05-27 | 2019-12-17 | Pratt & Whitney Canada Corp. | Fire shield integrated to fuel nozzle retaining bracket |
| US10526972B2 (en) * | 2016-12-07 | 2020-01-07 | Rolls-Royce Corporation | Segmented fuel delivery system |
| US11306660B2 (en) | 2017-04-20 | 2022-04-19 | Pratt & Whitney Canada Corp. | Transfer tube manifold with integrated plugs |
| US11137144B2 (en) * | 2017-12-11 | 2021-10-05 | General Electric Company | Axial fuel staging system for gas turbine combustors |
| US11156162B2 (en) * | 2018-05-23 | 2021-10-26 | General Electric Company | Fluid manifold damper for gas turbine engine |
| US11060460B1 (en) | 2019-04-01 | 2021-07-13 | Marine Turbine Technologies, LLC | Fuel distribution system for gas turbine engine |
| US11578661B2 (en) | 2019-09-19 | 2023-02-14 | Pratt & Whitney Canada Corp. | Systems and methods for starting a gas turbine engine |
| CN113969837A (zh) * | 2020-07-24 | 2022-01-25 | 通用电气公司 | 改善的燃料分配歧管 |
| US11629641B2 (en) | 2020-09-29 | 2023-04-18 | General Electric Company | Fuel distribution manifold |
| US11867125B2 (en) * | 2021-06-30 | 2024-01-09 | Pratt & Whitney Canada Corp. | Fuel manifold adapter |
| US12241416B2 (en) | 2022-07-04 | 2025-03-04 | Pratt & Whitney Canada Corp. | Adaptor for a fuel system of an aircraft engine |
| US11939922B2 (en) * | 2022-08-19 | 2024-03-26 | Pratt & Whitney Canada Corp. | Fuel assembly for a gas turbine engine |
| US20250283601A1 (en) * | 2024-03-07 | 2025-09-11 | Rtx Corporation | Continuous flow fuel system |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3793838A (en) * | 1972-09-05 | 1974-02-26 | Gen Electric | Augmenter fuel injection mounting system |
| GB2036296B (en) * | 1978-11-20 | 1982-12-01 | Rolls Royce | Gas turbine |
| US4402184A (en) * | 1980-12-08 | 1983-09-06 | International Harvester Company | Gas turbine engines |
| US4467610A (en) * | 1981-04-17 | 1984-08-28 | General Electric Company | Gas turbine fuel system |
| CA1170844A (en) * | 1982-06-25 | 1984-07-17 | Carl E. Pearson | Gas turbine fuel system |
| US5031407A (en) * | 1989-06-06 | 1991-07-16 | Allied-Signal Inc. | Apparatus for use in a fuel delivery system for a gas turbine engine |
| US5257502A (en) * | 1991-08-12 | 1993-11-02 | General Electric Company | Fuel delivery system for dual annular combustor |
| US5211005A (en) * | 1992-04-16 | 1993-05-18 | Avco Corporation | High density fuel injection manifold |
| US5263314A (en) * | 1992-09-28 | 1993-11-23 | General Motors Corporation | Fuel leakage protection system for gas turbine engine |
| US6339924B1 (en) * | 1999-12-20 | 2002-01-22 | General Electric Company | Method and apparatus for encapsulating gas turbine engine fuel connections |
| US6672145B2 (en) * | 2001-09-21 | 2004-01-06 | Honeywell International, Inc. | Apparatus and method for testing jet engine fuel manifold flow distribution |
| US6786049B2 (en) * | 2002-05-22 | 2004-09-07 | Hamilton Sundstrand | Fuel supply control for a gas turbine including multiple solenoid valves |
| EP1906091A2 (en) * | 2006-09-26 | 2008-04-02 | United Technologies Corporation | Flow divider valve |
| GB2461503A (en) * | 2008-06-30 | 2010-01-06 | Rolls Royce Plc | A sliding joint for a gas turbine engine fuel manifold |
| US8091362B2 (en) * | 2008-08-20 | 2012-01-10 | Woodward, Inc. | Fuel injector sans support/stem |
| US8037690B2 (en) * | 2008-12-17 | 2011-10-18 | Pratt & Whitney Canada Corp. | Fuel manifold for gas turbine engine |
| RU2447304C2 (ru) * | 2010-03-19 | 2012-04-10 | Общество с ограниченной ответственностью Финансово-промышленная компания "Космос-Нефть-Газ" | Газотурбинная установка |
-
2012
- 2012-08-06 FR FR1257622A patent/FR2994217B1/fr active Active
-
2013
- 2013-07-29 ES ES13756616.2T patent/ES2612164T3/es active Active
- 2013-07-29 CN CN201380044538.6A patent/CN104583564B/zh active Active
- 2013-07-29 EP EP13756616.2A patent/EP2880285B8/fr active Active
- 2013-07-29 CA CA2880859A patent/CA2880859C/fr active Active
- 2013-07-29 JP JP2015525921A patent/JP6147857B2/ja not_active Expired - Fee Related
- 2013-07-29 WO PCT/FR2013/051822 patent/WO2014023892A1/fr active Application Filing
- 2013-07-29 IN IN981DEN2015 patent/IN2015DN00981A/en unknown
- 2013-07-29 US US14/419,741 patent/US9689313B2/en active Active
- 2013-07-29 KR KR1020157004096A patent/KR102077358B1/ko not_active Expired - Fee Related
- 2013-07-29 PL PL13756616T patent/PL2880285T3/pl unknown
- 2013-07-29 RU RU2015107807A patent/RU2630053C2/ru active
Also Published As
| Publication number | Publication date |
|---|---|
| CA2880859C (fr) | 2020-07-07 |
| KR102077358B1 (ko) | 2020-02-13 |
| JP6147857B2 (ja) | 2017-06-14 |
| PL2880285T3 (pl) | 2017-07-31 |
| KR20150038109A (ko) | 2015-04-08 |
| EP2880285B1 (fr) | 2016-10-19 |
| JP2015524912A (ja) | 2015-08-27 |
| WO2014023892A1 (fr) | 2014-02-13 |
| CN104583564A (zh) | 2015-04-29 |
| RU2015107807A (ru) | 2016-09-27 |
| EP2880285B8 (fr) | 2016-12-28 |
| ES2612164T3 (es) | 2017-05-12 |
| US20150176496A1 (en) | 2015-06-25 |
| RU2630053C2 (ru) | 2017-09-05 |
| CN104583564B (zh) | 2017-02-22 |
| FR2994217B1 (fr) | 2018-05-04 |
| FR2994217A1 (fr) | 2014-02-07 |
| CA2880859A1 (fr) | 2014-02-13 |
| EP2880285A1 (fr) | 2015-06-10 |
| US9689313B2 (en) | 2017-06-27 |
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