FR1408812A - Perfectionnement apporté aux chambres de combustion de propulseurs - Google Patents

Perfectionnement apporté aux chambres de combustion de propulseurs

Info

Publication number
FR1408812A
FR1408812A FR980889A FR980889A FR1408812A FR 1408812 A FR1408812 A FR 1408812A FR 980889 A FR980889 A FR 980889A FR 980889 A FR980889 A FR 980889A FR 1408812 A FR1408812 A FR 1408812A
Authority
FR
France
Prior art keywords
combustion chambers
thruster combustion
thruster
chambers
combustion
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
FR980889A
Other languages
English (en)
Inventor
Maurice Ravel
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.)
NORD AVIAT
Original Assignee
NORD AVIAT
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 NORD AVIAT filed Critical NORD AVIAT
Priority to FR980889A priority Critical patent/FR1408812A/fr
Priority to DEN26049A priority patent/DE1297941B/de
Priority to GB2602/65A priority patent/GB1093781A/en
Priority to US428181A priority patent/US3274776A/en
Application granted granted Critical
Publication of FR1408812A publication Critical patent/FR1408812A/fr
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16Composite ram-jet/turbo-jet engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • 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
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • 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)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
FR980889A 1964-07-06 1964-07-06 Perfectionnement apporté aux chambres de combustion de propulseurs Expired FR1408812A (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR980889A FR1408812A (fr) 1964-07-06 1964-07-06 Perfectionnement apporté aux chambres de combustion de propulseurs
DEN26049A DE1297941B (de) 1964-07-06 1965-01-08 Brennkammer fuer Turbostaustrahltriebwerke
GB2602/65A GB1093781A (en) 1964-07-06 1965-01-20 Improvements in combustion chambers of ram-jets
US428181A US3274776A (en) 1964-07-06 1965-01-26 Combustion chambers of reaction propulsion units

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR980889A FR1408812A (fr) 1964-07-06 1964-07-06 Perfectionnement apporté aux chambres de combustion de propulseurs

Publications (1)

Publication Number Publication Date
FR1408812A true FR1408812A (fr) 1965-08-20

Family

ID=8834036

Family Applications (1)

Application Number Title Priority Date Filing Date
FR980889A Expired FR1408812A (fr) 1964-07-06 1964-07-06 Perfectionnement apporté aux chambres de combustion de propulseurs

Country Status (4)

Country Link
US (1) US3274776A (fr)
DE (1) DE1297941B (fr)
FR (1) FR1408812A (fr)
GB (1) GB1093781A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2297327A1 (fr) * 1975-01-08 1976-08-06 Gen Electric Stabilisateur de flamme pour turbo-reacteur

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3800527A (en) * 1971-03-18 1974-04-02 United Aircraft Corp Piloted flameholder construction
DE3935313C1 (fr) * 1989-10-24 1991-06-06 Mtu Muenchen Gmbh

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2720754A (en) * 1950-09-29 1955-10-18 Mcdonnell Aircraft Corp Flameholder for ram jet engine
GB719301A (en) * 1951-04-25 1954-12-01 Rolls Royce Improvements relating to gas turbine engines
US2872785A (en) * 1951-06-06 1959-02-10 Curtiss Wright Corp Jet engine burner apparatus having means for spreading the pilot flame
DE957003C (de) * 1951-11-20 1957-01-24 Hiller Helicopters Kontinuierlich arbeitendes Staustrahltriebwerk fuer Rotorfluegel von Hubschraubern
FR1109594A (fr) * 1954-08-03 1956-01-31 Snecma Propulseur à réaction combiné
DE1051071B (de) * 1955-07-13 1959-02-19 Sud Aviation Verbrennungsvorrichtung fuer UEberschall-Staustrahltriebwerke
DE1167594B (de) * 1960-04-25 1964-04-09 Rolls Royce Kreisringfoermige Brennkammer fuer Gasturbinenstrahltriebwerke
FR1325056A (fr) * 1962-03-15 1963-04-26 Nord Aviation Perfectionnements aux combinés turboréacteur-statoréacteur

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2297327A1 (fr) * 1975-01-08 1976-08-06 Gen Electric Stabilisateur de flamme pour turbo-reacteur

Also Published As

Publication number Publication date
DE1297941B (de) 1969-06-19
US3274776A (en) 1966-09-27
GB1093781A (en) 1967-12-06

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