FR3001790B1 - Chambre de combustion a volume variable avec systeme d'injection de combustible en amont des injecteurs - Google Patents

Chambre de combustion a volume variable avec systeme d'injection de combustible en amont des injecteurs Download PDF

Info

Publication number
FR3001790B1
FR3001790B1 FR1450905A FR1450905A FR3001790B1 FR 3001790 B1 FR3001790 B1 FR 3001790B1 FR 1450905 A FR1450905 A FR 1450905A FR 1450905 A FR1450905 A FR 1450905A FR 3001790 B1 FR3001790 B1 FR 3001790B1
Authority
FR
France
Prior art keywords
injectors
combustion chamber
injection system
fuel injection
variable volume
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.)
Expired - Fee Related
Application number
FR1450905A
Other languages
English (en)
French (fr)
Other versions
FR3001790A1 (fr
Inventor
Christopher Paul Keener
Thomas Edward Johnson
Johnie Franklin Mcconnaughhay
Heath Michael Ostebee
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR3001790A1 publication Critical patent/FR3001790A1/fr
Application granted granted Critical
Publication of FR3001790B1 publication Critical patent/FR3001790B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • 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
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C5/00—Disposition of burners with respect to the combustion chamber or to one another; Mounting of burners in combustion apparatus
    • F23C5/02—Structural details of mounting
    • F23C5/06—Provision for adjustment of burner position during operation
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
FR1450905A 2013-02-06 2014-02-06 Chambre de combustion a volume variable avec systeme d'injection de combustible en amont des injecteurs Expired - Fee Related FR3001790B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13/760,091 US9435539B2 (en) 2013-02-06 2013-02-06 Variable volume combustor with pre-nozzle fuel injection system

Publications (2)

Publication Number Publication Date
FR3001790A1 FR3001790A1 (fr) 2014-08-08
FR3001790B1 true FR3001790B1 (fr) 2020-07-31

Family

ID=51214850

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1450905A Expired - Fee Related FR3001790B1 (fr) 2013-02-06 2014-02-06 Chambre de combustion a volume variable avec systeme d'injection de combustible en amont des injecteurs

Country Status (4)

Country Link
US (1) US9435539B2 (enExample)
JP (1) JP6397193B2 (enExample)
CH (1) CH707574A2 (enExample)
FR (1) FR3001790B1 (enExample)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10041681B2 (en) 2014-08-06 2018-08-07 General Electric Company Multi-stage combustor with a linear actuator controlling a variable air bypass
JP6551820B2 (ja) 2014-09-29 2019-07-31 三菱日立パワーシステムズ株式会社 燃焼器、及びこれを備えているガスタービン
US10655541B2 (en) * 2016-03-25 2020-05-19 General Electric Company Segmented annular combustion system
JP6941576B2 (ja) * 2018-03-26 2021-09-29 三菱パワー株式会社 燃焼器及びそれを備えるガスタービン
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages
FR3145795A1 (fr) * 2023-02-13 2024-08-16 Safran Aircraft Engines Ensemble pour turbomachine et turbomachine associee
US12339007B2 (en) 2023-12-01 2025-06-24 Doosan Enerbility Co., Ltd. Combustor nozzle, combustor and gas turbine including same
US12379107B2 (en) 2023-12-01 2025-08-05 Doosan Enerbility Co., Ltd. Combustor nozzle, combustor and gas turbine including same

Family Cites Families (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3738106A (en) 1971-10-26 1973-06-12 Avco Corp Variable geometry combustors
US3745766A (en) 1971-10-26 1973-07-17 Avco Corp Variable geometry for controlling the flow of air to a combustor
US3742703A (en) 1971-10-26 1973-07-03 Avco Corp Variable geometry combustor construction
US4044553A (en) 1976-08-16 1977-08-30 General Motors Corporation Variable geometry swirler
US4417846A (en) 1977-12-09 1983-11-29 Hydra-Rig, Inc. Traveling block elevator latch assembly
US4365910A (en) 1980-05-15 1982-12-28 Steelcraft Corporation Strut support apparatus
US4532762A (en) 1982-07-22 1985-08-06 The Garrett Corporation Gas turbine engine variable geometry combustor apparatus
US4545196A (en) 1982-07-22 1985-10-08 The Garrett Corporation Variable geometry combustor apparatus
US4497170A (en) 1982-07-22 1985-02-05 The Garrett Corporation Actuation system for a variable geometry combustor
US4844649A (en) 1987-04-20 1989-07-04 Vandenboom James J Bracket assembly for geodesic dome
US5231747A (en) 1990-12-21 1993-08-03 The Boeing Company Drill/rivet device
US5195853A (en) 1991-04-15 1993-03-23 Cincinnati Milacron Inc. Quill feed and spindle drive assembly
US5257499A (en) * 1991-09-23 1993-11-02 General Electric Company Air staged premixed dry low NOx combustor with venturi modulated flow split
EP0534685A1 (en) * 1991-09-23 1993-03-31 General Electric Company Air staged premixed dry low NOx combustor
US5287697A (en) 1992-01-02 1994-02-22 General Electric Company Variable area bypass injector seal
US5444982A (en) 1994-01-12 1995-08-29 General Electric Company Cyclonic prechamber with a centerbody
EP0686812B1 (en) * 1994-06-10 2000-03-29 General Electric Company Operating a combustor of a gas turbine
DE4446842B4 (de) 1994-12-27 2006-08-10 Alstom Verfahren und Vorrichtung zum Zuleiten eines gasförmigen Brennstoffs in einen Vormischbrenner
GB2299399A (en) 1995-03-25 1996-10-02 Rolls Royce Plc Variable geometry air-fuel injector
US5813232A (en) * 1995-06-05 1998-09-29 Allison Engine Company, Inc. Dry low emission combustor for gas turbine engines
GB2351343A (en) 1999-06-22 2000-12-27 Alstom Gas Turbines Ltd Telescopically-moveable combustion chamber
US6438959B1 (en) 2000-12-28 2002-08-27 General Electric Company Combustion cap with integral air diffuser and related method
US7093445B2 (en) 2002-05-31 2006-08-22 Catalytica Energy Systems, Inc. Fuel-air premixing system for a catalytic combustor
GB0319329D0 (en) 2003-08-16 2003-09-17 Rolls Royce Plc Variable geometry combustor
ITTO20031013A1 (it) 2003-12-16 2005-06-17 Ansaldo Energia Spa Sistema di smorzamento di instabilita' termoacustiche in un dispositivo combustore per una turbina a gas.
DE102005039279B4 (de) 2005-08-19 2007-06-14 Mtu Aero Engines Gmbh Linearführung
KR100820233B1 (ko) * 2006-10-31 2008-04-08 한국전력공사 연소기 및 이를 포함하는 멀티 연소기, 그리고 연소방법
US20100175380A1 (en) 2009-01-13 2010-07-15 General Electric Company Traversing fuel nozzles in cap-less combustor assembly
US8616002B2 (en) * 2009-07-23 2013-12-31 General Electric Company Gas turbine premixing systems
US8276391B2 (en) 2010-04-19 2012-10-02 General Electric Company Combustor liner cooling at transition duct interface and related method
US8991187B2 (en) 2010-10-11 2015-03-31 General Electric Company Combustor with a lean pre-nozzle fuel injection system
US8322143B2 (en) * 2011-01-18 2012-12-04 General Electric Company System and method for injecting fuel
US8875516B2 (en) 2011-02-04 2014-11-04 General Electric Company Turbine combustor configured for high-frequency dynamics mitigation and related method

Also Published As

Publication number Publication date
CH707574A2 (de) 2014-08-15
FR3001790A1 (fr) 2014-08-08
JP6397193B2 (ja) 2018-09-26
JP2014153052A (ja) 2014-08-25
US9435539B2 (en) 2016-09-06
US20140216049A1 (en) 2014-08-07

Similar Documents

Publication Publication Date Title
FR3001790B1 (fr) Chambre de combustion a volume variable avec systeme d'injection de combustible en amont des injecteurs
MX389948B (es) Sistema y metodo para mejorar el funcionamiento de motores de combustion que emplean combustibles primarios y secundarios.
GB2573853B (en) Fuel injector assembly for gas turbine engine
EP2631459A4 (en) FUEL SUPPLY SYSTEM FOR A GAS ENGINE
EP2977584A4 (en) FUEL FEED CONTROL DEVICE FOR VORKAMMERGASMOTOREN
FR2986856B1 (fr) Dispositif d'injection d'air et de carburant pour une chambre de combustion d'une turbomachine
FR3012522B1 (fr) Moteur a combustion a injection directe de combustible a allumage par compression et procede d'injection de combustible pour un tel moteur.
EP3060851A4 (en) COMPREHENSIVE AND AXIAL STAGED FLAME TUBE FOR GAS TURBINE MOTOR
GB2570035B (en) A Lean Burn Fuel Injector for a Gas Turbine Engine Combustion Chamber
EA201490839A1 (ru) Двигатель, использующий несколько видов топлива, и соответствующий способ
EP3666636A4 (en) EVAPORATIVE LOSS REFLAKING SYSTEM, METHOD OF DISPENSING LUBRICATING OIL IN EVAPORATIVE LOSS REFLAKING SYSTEM, AND ENGINE FUEL SUPPLY METHOD
GB201108766D0 (en) Internal combustion engines
EP2806217A3 (en) Gas turbine engines with fuel injector assemblies
FR2988813B1 (fr) Dispositif d'injection d'un melange d'air et de carburant dans une chambre de combustion de turbomachine
EP3361070A4 (en) FUEL INJECTION NOZZLE FOR VEHICLE ENGINE AND CLEANING DEVICE FOR COMBUSTION CHAMBER CARBON
EP4050261A4 (en) LIQUID FUEL INJECTOR
FR3011317B1 (fr) Chambre de combustion pour turbomachine a admission d'air homogene au travers de systemes d'injection
EP3535529A4 (en) Premix fuel nozzle for a gas turbine and combustor
EA201992531A1 (ru) Система для адаптации двигателя внутреннего сгорания к питанию газообразным топливом в газовой фазе и газообразным топливом в жидкой фазе
SE0700380L (sv) Arrangemang och förfarande hos en förbränningsmotor
DK201270034A (en) An internal combustion engine with a combined fuel oil and fuel gas operation mode
PL407361A1 (pl) Układ zasilający silniki spalinowe w paliwo
FI20115212A0 (fi) Mäntäpolttomoottorin polttoaineensyöttöjärjestelmä ja menetelmä sen käyttämiseksi
CL2016001433A1 (es) Sistema de combustible para vehículos
PH12014501645A1 (en) Fuel injection device for internal combustion engine

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLSC Publication of the preliminary search report

Effective date: 20180330

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

ST Notification of lapse

Effective date: 20221005