FR2203023A1 - - Google Patents

Info

Publication number
FR2203023A1
FR2203023A1 FR7236272A FR7236272A FR2203023A1 FR 2203023 A1 FR2203023 A1 FR 2203023A1 FR 7236272 A FR7236272 A FR 7236272A FR 7236272 A FR7236272 A FR 7236272A FR 2203023 A1 FR2203023 A1 FR 2203023A1
Authority
FR
France
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.)
Granted
Application number
FR7236272A
Other languages
French (fr)
Other versions
FR2203023B1 (en
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.)
Office National dEtudes et de Recherches Aerospatiales ONERA
Original Assignee
Office National dEtudes et de Recherches Aerospatiales ONERA
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 Office National dEtudes et de Recherches Aerospatiales ONERA filed Critical Office National dEtudes et de Recherches Aerospatiales ONERA
Priority to FR7236272A priority Critical patent/FR2203023B1/fr
Publication of FR2203023A1 publication Critical patent/FR2203023A1/fr
Application granted granted Critical
Publication of FR2203023B1 publication Critical patent/FR2203023B1/fr
Expired legal-status Critical Current

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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR7236272A 1972-10-13 1972-10-13 Expired FR2203023B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7236272A FR2203023B1 (en) 1972-10-13 1972-10-13

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7236272A FR2203023B1 (en) 1972-10-13 1972-10-13

Publications (2)

Publication Number Publication Date
FR2203023A1 true FR2203023A1 (en) 1974-05-10
FR2203023B1 FR2203023B1 (en) 1976-08-20

Family

ID=9105591

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7236272A Expired FR2203023B1 (en) 1972-10-13 1972-10-13

Country Status (1)

Country Link
FR (1) FR2203023B1 (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0019022A1 (en) * 1979-05-18 1980-11-26 Robert Storey Babington Liquid fuel burners
EP0252315A1 (en) * 1986-07-08 1988-01-13 BBC Brown Boveri AG Combustion chamber device with a precombustion chamber for an understoichiometric combustion
EP0349635A1 (en) * 1987-12-28 1990-01-10 Sundstrand Corp Turbine combustor with tangential fuel injection and bender jets.
WO1991008421A1 (en) * 1989-12-05 1991-06-13 Allied-Signal Inc. Combustion apparatus and method for a turbine engine
EP0540162A1 (en) * 1991-09-23 1993-05-05 General Electric Company Aero-slinger combustor
US5265425A (en) * 1991-09-23 1993-11-30 General Electric Company Aero-slinger combustor
US5277022A (en) * 1990-06-22 1994-01-11 Sundstrand Corporation Air blast fuel injecton system
WO1996008699A1 (en) * 1994-09-14 1996-03-21 Nyfotek A.S Method for measuring sound velocity and sample holder
WO1996008680A1 (en) * 1994-09-16 1996-03-21 Sundstrand Corporation Combustor for a gas turbine engine
EP1766292A2 (en) * 2004-06-10 2007-03-28 Georgia Technology Research Corporation Stagnation point reverse flow combustor for a combustion system
JP2008185253A (en) * 2007-01-30 2008-08-14 General Electric Co <Ge> System having reverse flow injection mechanism, and method of injecting fuel and air
WO2016126986A3 (en) * 2015-02-04 2016-10-06 Exxonmobil Upstream Research Company Systems and methods for high volumetric oxidant flow in gas turbine engine with exhaust gas recirculation

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB899213A (en) * 1959-12-24 1962-06-20 Havilland Engine Co Ltd Combustion chambers
GB1150226A (en) * 1965-05-27 1969-04-30 Lucas Industries Ltd Flame Tubes for Gas Turbine Engines.

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB899213A (en) * 1959-12-24 1962-06-20 Havilland Engine Co Ltd Combustion chambers
GB1150226A (en) * 1965-05-27 1969-04-30 Lucas Industries Ltd Flame Tubes for Gas Turbine Engines.

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0019022A1 (en) * 1979-05-18 1980-11-26 Robert Storey Babington Liquid fuel burners
EP0252315A1 (en) * 1986-07-08 1988-01-13 BBC Brown Boveri AG Combustion chamber device with a precombustion chamber for an understoichiometric combustion
CH671449A5 (en) * 1986-07-08 1989-08-31 Bbc Brown Boveri & Cie
US4894005A (en) * 1986-07-08 1990-01-16 Bbc Brown Boveri Ag Combustion chamber arrangement with a pre-combustion chamber for substoichiometric combustion
EP0349635A1 (en) * 1987-12-28 1990-01-10 Sundstrand Corp Turbine combustor with tangential fuel injection and bender jets.
EP0349635A4 (en) * 1987-12-28 1990-05-14 Sundstrand Corp Turbine combustor with tangential fuel injection and bender jets.
WO1991008421A1 (en) * 1989-12-05 1991-06-13 Allied-Signal Inc. Combustion apparatus and method for a turbine engine
US5109671A (en) * 1989-12-05 1992-05-05 Allied-Signal Inc. Combustion apparatus and method for a turbine engine
US5277022A (en) * 1990-06-22 1994-01-11 Sundstrand Corporation Air blast fuel injecton system
EP0540162A1 (en) * 1991-09-23 1993-05-05 General Electric Company Aero-slinger combustor
US5265425A (en) * 1991-09-23 1993-11-30 General Electric Company Aero-slinger combustor
WO1996008699A1 (en) * 1994-09-14 1996-03-21 Nyfotek A.S Method for measuring sound velocity and sample holder
WO1996008680A1 (en) * 1994-09-16 1996-03-21 Sundstrand Corporation Combustor for a gas turbine engine
US5746048A (en) * 1994-09-16 1998-05-05 Sundstrand Corporation Combustor for a gas turbine engine
EP1766292A2 (en) * 2004-06-10 2007-03-28 Georgia Technology Research Corporation Stagnation point reverse flow combustor for a combustion system
EP1766292A4 (en) * 2004-06-10 2011-07-27 Georgia Tech Res Inst Stagnation point reverse flow combustor for a combustion system
JP2008185253A (en) * 2007-01-30 2008-08-14 General Electric Co <Ge> System having reverse flow injection mechanism, and method of injecting fuel and air
WO2016126986A3 (en) * 2015-02-04 2016-10-06 Exxonmobil Upstream Research Company Systems and methods for high volumetric oxidant flow in gas turbine engine with exhaust gas recirculation
US10094566B2 (en) 2015-02-04 2018-10-09 General Electric Company Systems and methods for high volumetric oxidant flow in gas turbine engine with exhaust gas recirculation

Also Published As

Publication number Publication date
FR2203023B1 (en) 1976-08-20

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Legal Events

Date Code Title Description
CL Concession to grant licenses
ST Notification of lapse