[go: up one dir, main page]

CH531643A - Chambre de combustion pour turbine à gaz - Google Patents

Chambre de combustion pour turbine à gaz

Info

Publication number
CH531643A
CH531643A CH1558369A CH1558369A CH531643A CH 531643 A CH531643 A CH 531643A CH 1558369 A CH1558369 A CH 1558369A CH 1558369 A CH1558369 A CH 1558369A CH 531643 A CH531643 A CH 531643A
Authority
CH
Switzerland
Prior art keywords
combustion chamber
chamber according
nozzle
valve
air
Prior art date
Application number
CH1558369A
Other languages
English (en)
French (fr)
Inventor
Guillot Jack
Original Assignee
Bennes Marrel Sa
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 Bennes Marrel Sa filed Critical Bennes Marrel Sa
Publication of CH531643A publication Critical patent/CH531643A/fr

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • F23R3/48Flame tube interconnectors, e.g. cross-over tubes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/22Fuel supply systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26Control of fuel supply
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54Reverse-flow combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Spray-Type Burners (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
CH1558369A 1968-10-18 1969-10-17 Chambre de combustion pour turbine à gaz CH531643A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR69050513 1968-10-18

Publications (1)

Publication Number Publication Date
CH531643A true CH531643A (fr) 1972-12-15

Family

ID=9695675

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1558369A CH531643A (fr) 1968-10-18 1969-10-17 Chambre de combustion pour turbine à gaz

Country Status (11)

Country Link
US (1) US3650106A (de)
AT (2) AT279483B (de)
BR (1) BR6913235D0 (de)
CA (1) CA917933A (de)
CH (1) CH531643A (de)
DE (3) DE1966661A1 (de)
ES (1) ES372250A1 (de)
FR (1) FR1592591A (de)
GB (1) GB1251749A (de)
NL (1) NL6915497A (de)
SE (1) SE356332B (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5089708A (de) * 1973-12-14 1975-07-18
CH586375A5 (de) * 1975-06-25 1977-03-31 Bbc Brown Boveri & Cie
JPS5242907U (de) * 1975-09-22 1977-03-26
US4129985A (en) * 1975-11-17 1978-12-19 Kawasaki Jukogyo Kabushiki Kaisha Combustor device of gas turbine engine
US4900246A (en) * 1977-05-25 1990-02-13 Phillips Petroleum Company Apparatus for burning nitrogen-containing fuels
GB2040031B (en) * 1979-01-12 1983-02-09 Gen Electric Dual stage-dual mode low emission gas turbine combustion system
US4393651A (en) * 1980-09-02 1983-07-19 Chandler Evans Inc. Fuel control method and apparatus
GB9108235D0 (en) * 1991-04-17 1991-06-05 Rolls Royce Plc A combustion chamber assembly
US5361577A (en) * 1991-07-15 1994-11-08 General Electric Company Spring loaded cross-fire tube
EP2157286A1 (de) * 2008-08-21 2010-02-24 Siemens Aktiengesellschaft Gasturbine mit angewinkeltem Mischgehäuse und Verfahren zur Turbinenanströmung
US20110091829A1 (en) * 2009-10-20 2011-04-21 Vinayak Barve Multi-fuel combustion system
US9388738B2 (en) * 2011-10-04 2016-07-12 Siemens Energy, Inc. Casing for a gas turbine engine
US9328925B2 (en) * 2012-11-15 2016-05-03 General Electric Company Cross-fire tube purging arrangement and method of purging a cross-fire tube
US20140137536A1 (en) * 2012-11-21 2014-05-22 General Electric Company Super telescoping cross-fire tube and method of assembling a combustor structure
US9353952B2 (en) * 2012-11-29 2016-05-31 General Electric Company Crossfire tube assembly with tube bias between adjacent combustors
JP2015135212A (ja) * 2014-01-17 2015-07-27 ヤンマー株式会社 ガスタービンエンジン
US10161635B2 (en) * 2014-06-13 2018-12-25 Rolls-Royce Corporation Combustor with spring-loaded crossover tubes
JP6325930B2 (ja) * 2014-07-24 2018-05-16 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器
US10473117B2 (en) * 2015-07-22 2019-11-12 United Technologies Corporation Diffuser case for a gas powered turbine
CN115727354B (zh) * 2022-11-11 2025-02-14 中国航发哈尔滨东安发动机有限公司 一种飞行器用涡扇发动机火焰筒结构

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2638745A (en) * 1943-04-01 1953-05-19 Power Jets Res & Dev Ltd Gas turbine combustor having tangential air inlets for primary and secondary air
US3172257A (en) * 1962-08-30 1965-03-09 Ingersoll Rand Co Hot gas power plant arrangement
GB998371A (en) * 1964-05-04 1965-07-14 Rolls Royce Ignition means for a continuous flow engine
CH434875A (de) * 1966-06-21 1967-04-30 Huber Robert Brennstoff-Einspritzventil mit elektromagnetischer Betätigung

Also Published As

Publication number Publication date
DE1966661A1 (de) 1973-07-12
DE1966660A1 (de) 1973-07-12
DE1946905A1 (de) 1970-05-06
FR1592591A (de) 1970-05-19
DE1946905B2 (de) 1973-09-13
AT279483B (de) 1970-03-10
ES372250A1 (es) 1971-10-16
AT301271B (de) 1972-07-15
US3650106A (en) 1972-03-21
SE356332B (de) 1973-05-21
GB1251749A (de) 1971-10-27
NL6915497A (de) 1970-04-21
BR6913235D0 (pt) 1973-01-02
CA917933A (en) 1973-01-02

Similar Documents

Publication Publication Date Title
CH531643A (fr) Chambre de combustion pour turbine à gaz
FR2536465A1 (fr) Ensemble d'injecteur de combustible a air souffle
EP2643579B1 (de) Kombination aus einem turboluftstrahltriebwerk und staustrahltriebwerk
EP0214003B1 (de) Kraftstoffdüse mit vergrössertem Luftleitblech für die Brennkammer einer Gasturbine
EP1770333B1 (de) Anti-Verkokungsinjektorarm
FR2629868A1 (fr) Dispositif de controle de jeu
FR2736708A1 (fr) Chambre de combustion annulaire pour moteur de turbine a gaz
FR2708338A1 (fr) Brûleur de turbine à gaz.
FR2462556A1 (fr) Injecteur de carburants perfectionne pour moteur a turbine a gaz
FR2931203A1 (fr) Injecteur de carburant pour turbine a gaz et son procede de fabrication
CA2848629C (fr) Chambre annulaire de combustion d'une turbomachine
FR2601069A1 (fr) Turbine.
CA2899508C (fr) Ensemble de combustion de turbomachine comprenant un circuit d'alimentation de carburant ameliore
CA2634615C (fr) Chambre de combustion de turbomachine a circulation helicoidale de l'air
CA2646959A1 (fr) Systeme d'injection d'un melange d'air et de carburant dans une chambre de combustion de turbomachine
FR2616886A1 (fr) Chambre de combustion annulaire pour une turbine a gaz
EP0359662A1 (de) Heissgaszapfvorrichtung in einer Raketenbrennkammer und Einspritzkopf, versehen mit einer solchen Vorrichtung
EP3530908B1 (de) Brennkammer, die zwei typen von injektoren umfasst, in denen die dichtungsorgane eine unterschiedliche öffnungsschwelle besitzen
FR2476230A1 (fr) Systeme d'injection de carburant pour augmentateur de poussee de moteur a turbine a gaz
FR2510657A1 (fr) Dispositif de demarrage pour une turbine a gaz
FR2695460A1 (fr) Chambre de combustion de turbomachine à plusieurs injecteurs.
WO1989001090A1 (fr) Chambre de combustion auxiliaire pour moteurs a combustion interne suralimentes
FR2660416A1 (fr) Chambre de combustion comportant une tuyere pour un propulseur hypersonique.
FR3038363A1 (fr) Chambre annulaire de combustion a diaphragme fixe, pour une turbine a gaz
FR2982010A1 (fr) Chambre de combustion annulaire dans une turbomachine

Legal Events

Date Code Title Description
PL Patent ceased