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
Application number
Other languages
English (en)
Inventor
Cédric Roger Zordan
Xavier Francez
Original Assignee
Turbomeca
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Turbomeca filed Critical Turbomeca
Publication of IN2015DN00981A publication Critical patent/IN2015DN00981A/en

Links

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)
IN981DEN2015 2012-08-06 2013-07-29 IN2015DN00981A (fr)

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 (fr) 2015-06-12

Family

ID=47427360

Family Applications (1)

Application Number Title Priority Date Filing Date
IN981DEN2015 IN2015DN00981A (fr) 2012-08-06 2013-07-29

Country Status (12)

Country Link
US (1) US9689313B2 (fr)
EP (1) EP2880285B8 (fr)
JP (1) JP6147857B2 (fr)
KR (1) KR102077358B1 (fr)
CN (1) CN104583564B (fr)
CA (1) CA2880859C (fr)
ES (1) ES2612164T3 (fr)
FR (1) FR2994217B1 (fr)
IN (1) IN2015DN00981A (fr)
PL (1) PL2880285T3 (fr)
RU (1) RU2630053C2 (fr)
WO (1) WO2014023892A1 (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10550769B2 (en) 2014-02-19 2020-02-04 United Technologies Corporation Fuel manifold fitting with integral support for a gas turbine engine
JP2017524094A (ja) * 2014-07-02 2017-08-24 ヌオーヴォ ピニォーネ ソチエタ レスポンサビリタ リミタータＮｕｏｖｏ Ｐｉｇｎｏｎｅ Ｓ．Ｒ．Ｌ． 燃料分配装置、ガスタービンエンジン、および取り付け方法
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
US20240003298A1 (en) * 2022-07-04 2024-01-04 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

Family Cites Families (17)

* Cited by examiner, † Cited by third party
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 (fr) * 1982-06-25 1984-07-17 Carl E. Pearson Systeme de carburant pour turbine a gaz
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 (fr) * 2006-09-26 2008-04-02 United Technologies Corporation Vanne de répartition de débit
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

Also Published As

Publication number Publication date
JP6147857B2 (ja) 2017-06-14
EP2880285B8 (fr) 2016-12-28
ES2612164T3 (es) 2017-05-12
KR20150038109A (ko) 2015-04-08
US20150176496A1 (en) 2015-06-25
US9689313B2 (en) 2017-06-27
PL2880285T3 (pl) 2017-07-31
FR2994217A1 (fr) 2014-02-07
KR102077358B1 (ko) 2020-02-13
CN104583564B (zh) 2017-02-22
RU2630053C2 (ru) 2017-09-05
WO2014023892A1 (fr) 2014-02-13
CN104583564A (zh) 2015-04-29
CA2880859C (fr) 2020-07-07
JP2015524912A (ja) 2015-08-27
CA2880859A1 (fr) 2014-02-13
EP2880285A1 (fr) 2015-06-10
EP2880285B1 (fr) 2016-10-19
FR2994217B1 (fr) 2018-05-04
RU2015107807A (ru) 2016-09-27

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