FR1500110A - Perfectionnements aux turbo-réacteurs - Google Patents

Perfectionnements aux turbo-réacteurs

Info

Publication number
FR1500110A
FR1500110A FR68838A FR68838A FR1500110A FR 1500110 A FR1500110 A FR 1500110A FR 68838 A FR68838 A FR 68838A FR 68838 A FR68838 A FR 68838A FR 1500110 A FR1500110 A FR 1500110A
Authority
FR
France
Prior art keywords
turbo
reactors
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
Application number
FR68838A
Other languages
English (en)
Inventor
Herve Alain Quillevere
Jacques Emile Jules Caruel
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR68838A priority Critical patent/FR1500110A/fr
Priority to GB30388/67A priority patent/GB1194684A/en
Priority to US651308A priority patent/US3440818A/en
Application granted granted Critical
Publication of FR1500110A publication Critical patent/FR1500110A/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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient 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)
  • Investigating, Analyzing Materials By Fluorescence Or Luminescence (AREA)
  • Spray-Type Burners (AREA)
FR68838A 1966-07-08 1966-07-08 Perfectionnements aux turbo-réacteurs Expired FR1500110A (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR68838A FR1500110A (fr) 1966-07-08 1966-07-08 Perfectionnements aux turbo-réacteurs
GB30388/67A GB1194684A (en) 1966-07-08 1967-06-30 Improvements in or relating to Gas Turbine Engines
US651308A US3440818A (en) 1966-07-08 1967-07-05 Combustion and cooling air control in turbojet engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR68838A FR1500110A (fr) 1966-07-08 1966-07-08 Perfectionnements aux turbo-réacteurs

Publications (1)

Publication Number Publication Date
FR1500110A true FR1500110A (fr) 1967-11-03

Family

ID=8612906

Family Applications (1)

Application Number Title Priority Date Filing Date
FR68838A Expired FR1500110A (fr) 1966-07-08 1966-07-08 Perfectionnements aux turbo-réacteurs

Country Status (3)

Country Link
US (1) US3440818A (fr)
FR (1) FR1500110A (fr)
GB (1) GB1194684A (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2221621B1 (fr) * 1973-03-13 1976-09-10 Snecma
US3899882A (en) * 1974-03-27 1975-08-19 Westinghouse Electric Corp Gas turbine combustor basket cooling
US4073137A (en) * 1976-06-02 1978-02-14 United Technologies Corporation Convectively cooled flameholder for premixed burner
US4852355A (en) * 1980-12-22 1989-08-01 General Electric Company Dispensing arrangement for pressurized air
US4840226A (en) * 1987-08-10 1989-06-20 The United States Of America As Represented By The United States Department Of Energy Corrosive resistant heat exchanger
IT1236408B (it) * 1989-05-09 1993-02-26 Machler Urs Verona Procedimento per realizzare archi per violino od altri strumenti ad arco e prodotto con lo stesso ottenuto
US5323605A (en) * 1990-10-01 1994-06-28 General Electric Company Double dome arched combustor
US5581996A (en) * 1995-08-16 1996-12-10 General Electric Company Method and apparatus for turbine cooling
US6536201B2 (en) * 2000-12-11 2003-03-25 Pratt & Whitney Canada Corp. Combustor turbine successive dual cooling
US7509809B2 (en) * 2005-06-10 2009-03-31 Pratt & Whitney Canada Corp. Gas turbine engine combustor with improved cooling
FR2970666B1 (fr) * 2011-01-24 2013-01-18 Snecma Procede de perforation d'au moins une paroi d'une chambre de combustion
GB201116608D0 (en) * 2011-09-27 2011-11-09 Rolls Royce Plc A method of operating a combustion chamber

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2609040A (en) * 1950-03-14 1952-09-02 Elliott Co Combustion apparatus using compressed air
US2958194A (en) * 1951-09-24 1960-11-01 Power Jets Res & Dev Ltd Cooled flame tube
US2987873A (en) * 1955-05-13 1961-06-13 Phillips Petroleum Co Method and apparatus for using ammonia to increase the air specific impulse of a two-stage compressor turbojet engine
FR1094871A (fr) * 1959-01-22 1955-05-25 Thomson Houston Comp Francaise Perfectionnements aux appareils de combustion à combustible injecté
US3134229A (en) * 1961-10-02 1964-05-26 Gen Electric Combustion chamber
US3184918A (en) * 1963-06-18 1965-05-25 United Aircraft Corp Cooling arrangement for crossover tubes

Also Published As

Publication number Publication date
US3440818A (en) 1969-04-29
GB1194684A (en) 1970-06-10

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