BE812506A - Perfectionnements aux systemes de combustion pour moteurs a turbinea gaz - Google Patents

Perfectionnements aux systemes de combustion pour moteurs a turbinea gaz

Info

Publication number
BE812506A
BE812506A BE142170A BE142170A BE812506A BE 812506 A BE812506 A BE 812506A BE 142170 A BE142170 A BE 142170A BE 142170 A BE142170 A BE 142170A BE 812506 A BE812506 A BE 812506A
Authority
BE
Belgium
Prior art keywords
gas turbine
turbine engines
combustion systems
combustion
systems
Prior art date
Application number
BE142170A
Other languages
English (en)
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 filed Critical
Publication of BE812506A publication Critical patent/BE812506A/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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • 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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
  • Air Supply (AREA)
  • Gas Burners (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
BE142170A 1973-03-20 1974-03-19 Perfectionnements aux systemes de combustion pour moteurs a turbinea gaz BE812506A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1327473A GB1429677A (en) 1973-03-20 1973-03-20 Gas turbine engine combustion equipment

Publications (1)

Publication Number Publication Date
BE812506A true BE812506A (fr) 1974-07-15

Family

ID=10020003

Family Applications (1)

Application Number Title Priority Date Filing Date
BE142170A BE812506A (fr) 1973-03-20 1974-03-19 Perfectionnements aux systemes de combustion pour moteurs a turbinea gaz

Country Status (13)

Country Link
US (1) US3952503A (fr)
JP (1) JPS5313723B2 (fr)
AU (1) AU6681474A (fr)
BE (1) BE812506A (fr)
CA (1) CA987918A (fr)
DE (1) DE2412604C3 (fr)
DK (1) DK138463B (fr)
FR (1) FR2222535B1 (fr)
GB (1) GB1429677A (fr)
IE (1) IE39341B1 (fr)
LU (1) LU69649A1 (fr)
NL (1) NL7403662A (fr)
SE (1) SE390051B (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1552132A (en) * 1975-11-29 1979-09-12 Rolls Royce Combustion chambers for gas turbine engines
GB1571213A (en) * 1977-01-28 1980-07-09 Kainov G Combustion chamber for gas turbine engine
FR2410138A2 (fr) * 1977-11-29 1979-06-22 Snecma Perfectionnements aux chambres de combustion pour moteur a turbine a gaz
USRE30925E (en) * 1977-12-14 1982-05-11 Caterpillar Tractor Co. Fuel vaporizing combustor tube
US4188782A (en) * 1977-12-14 1980-02-19 Caterpillar Tractor Co. Fuel vaporizing combustor tube
EP0019417B1 (fr) * 1979-05-18 1983-01-12 Rolls-Royce Plc Appareil de combustion pour turbines à gaz
US5142871A (en) * 1991-01-22 1992-09-01 General Electric Company Combustor dome plate support having uniform thickness arcuate apex with circumferentially spaced coolant apertures
US5289686A (en) * 1992-11-12 1994-03-01 General Motors Corporation Low nox gas turbine combustor liner with elliptical apertures for air swirling
JP3197103B2 (ja) * 1993-03-08 2001-08-13 三菱重工業株式会社 予混合気の燃焼方法
US6286317B1 (en) * 1998-12-18 2001-09-11 General Electric Company Cooling nugget for a liner of a gas turbine engine combustor having trapped vortex cavity
US7624576B2 (en) * 2005-07-18 2009-12-01 Pratt & Whitney Canada Corporation Low smoke and emissions fuel nozzle
US8196410B2 (en) * 2007-05-18 2012-06-12 Pratt & Whitney Canada Corp. Stress reduction feature to improve fuel nozzle sheath durability
US7931124B2 (en) * 2007-12-12 2011-04-26 United Technologies Corporation On-demand lubrication system and method for improved flow management and containment
US10767865B2 (en) * 2016-06-13 2020-09-08 Rolls-Royce North American Technologies Inc. Swirl stabilized vaporizer combustor
CN108758689B (zh) * 2018-07-09 2024-04-09 西安空天能源动力智能制造研究院有限公司 一种微型涡轮发动机燃烧室
CN111964097B (zh) * 2020-08-21 2022-05-10 江苏科技大学 一种具有贫油预混预蒸发功能的组合分级燃烧室供油装置及其工作方法
CN113154453B (zh) * 2021-05-06 2022-07-08 中国航发湖南动力机械研究所 一种切向倾斜式环膜发散冷却结构
US11885495B2 (en) * 2021-06-07 2024-01-30 General Electric Company Combustor for a gas turbine engine including a liner having a looped feature
US20230144971A1 (en) * 2021-11-11 2023-05-11 General Electric Company Combustion liner

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2541900A (en) * 1948-12-24 1951-02-13 A V Roe Canada Ltd Multiple fuel jet burner and torch igniter unit with fuel vaporizing tubes
GB676640A (en) * 1949-06-29 1952-07-30 Ronald Guerin Meschino Vapourizing system for a gas turbine engine
US2930192A (en) * 1953-12-07 1960-03-29 Gen Electric Reverse vortex combustion chamber
US2973624A (en) * 1955-10-26 1961-03-07 Gen Electric Cowled dome liners
US2974485A (en) * 1958-06-02 1961-03-14 Gen Electric Combustor for fluid fuels
US3121996A (en) * 1961-10-02 1964-02-25 Lucas Industries Ltd Liquid fuel combustion apparatus
GB1136543A (en) * 1966-02-21 1968-12-11 Rolls Royce Liquid fuel combustion apparatus for gas turbine engines
FR1569142A (fr) * 1968-05-07 1969-05-30
US3498055A (en) * 1968-10-16 1970-03-03 United Aircraft Corp Smoke reduction combustion chamber
US3579983A (en) * 1969-05-05 1971-05-25 Snecma Improvements in or relating to combustion chambers
GB1320482A (en) * 1971-01-25 1973-06-13 Secr Defence Cooling of hot fluid ducts
FR2155835B1 (fr) * 1971-10-08 1974-05-31 Snecma

Also Published As

Publication number Publication date
IE39341L (en) 1974-09-20
IE39341B1 (en) 1978-09-13
NL7403662A (fr) 1974-09-24
LU69649A1 (fr) 1974-07-10
JPS5025917A (fr) 1975-03-18
FR2222535A1 (fr) 1974-10-18
JPS5313723B2 (fr) 1978-05-12
AU6681474A (en) 1975-09-25
SE390051B (sv) 1976-11-29
US3952503A (en) 1976-04-27
DE2412604C3 (de) 1981-04-23
DK138463C (fr) 1979-03-26
CA987918A (en) 1976-04-27
GB1429677A (en) 1976-03-24
DK138463B (da) 1978-09-11
DE2412604A1 (de) 1974-09-26
FR2222535B1 (fr) 1979-01-12
DE2412604B2 (de) 1980-08-28

Similar Documents

Publication Publication Date Title
FR2290350A1 (fr) Nacelle pour moteur a turbine a gaz
BE810901A (fr) Moteur a turbine a gaz
FR2312654A1 (fr) Perfectionnements aux chambres de combustion pour moteurs a turbine a gaz
BE812506A (fr) Perfectionnements aux systemes de combustion pour moteurs a turbinea gaz
FR2579724B1 (fr) Construction de chambre de combustion pour un moteur a turbine a gaz
BE804375A (fr) Systeme distributeur du carburant pour l'augmentateur d'un moteur a turbine a gaz
BE787374A (fr) Systeme de drainage de combustible pour moteur a turbine a gaz
CA1013153A (en) Combustion apparatus for a gas turbine engine
BE773357A (fr) Systeme de combustion a fente annulaire pour moteurs a turbine a gaz
FR2336554A1 (fr) Systeme de combustion pour turbines a gaz
FR2333964A1 (fr) Tuyere de propulsion pour moteur a turbine a gaz
BE766536A (fr) Systeme de refroidissement pour moteurs a turbine a gaz
BE818151A (fr) Moteur a gaz comprime
BE804376A (fr) Systeme de distribution du carburant d'un moteur a turbine a gaz
FR2335701A1 (fr) Rotor en ceramique pour moteur a turbine a gaz
BE822925A (fr) Perfectionnements apportes aux chambres de combustion pour systemes de suralimentation aux moteurs a combustion interne
CA1031972A (fr) Regulateur de combustion pour moteur de turbine a gaz
BE777521A (fr) Rotor pour turbomachine, notamment pour moteur a turbine a gaz
BE790239A (fr) Systeme de distribution de combustible a valve a vortex pour des moteurs a turbine a gaz
FR2333956A1 (fr) Injecteur de carburant pour moteur a turbine a gaz
FR1419665A (fr) Perfectionnements apportés aux chambres de combustion annulaires pour moteurs à tubine à gaz
FR2333947A1 (fr) Aube refrigeree pour moteur a turbine a gaz
FR2287585A1 (fr) Injecteur de carburant pour moteur a turbine a gaz
FR2341742A1 (fr) Chambre de combustion pour moteurs a reaction a turbines a gaz
SE427130B (sv) Forgasare for forbrenningsmotorer