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FR1150640A - Improvements to combustion chambers, in particular for aircraft - Google Patents

Improvements to combustion chambers, in particular for aircraft

Info

Publication number
FR1150640A
FR1150640A FR1150640DA FR1150640A FR 1150640 A FR1150640 A FR 1150640A FR 1150640D A FR1150640D A FR 1150640DA FR 1150640 A FR1150640 A FR 1150640A
Authority
FR
France
Prior art keywords
aircraft
combustion chambers
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
Other languages
French (fr)
Inventor
Rene Leduc
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
Application granted granted Critical
Publication of FR1150640A publication Critical patent/FR1150640A/en
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
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants 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
    • F02K7/10—Plants 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
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F23R3/346—Feeding into different combustion zones for staged combustion
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or 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)
FR1150640D 1956-05-18 1956-05-18 Improvements to combustion chambers, in particular for aircraft Expired FR1150640A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1150640T 1956-05-18

Publications (1)

Publication Number Publication Date
FR1150640A true FR1150640A (en) 1958-01-16

Family

ID=9647489

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1150640D Expired FR1150640A (en) 1956-05-18 1956-05-18 Improvements to combustion chambers, in particular for aircraft

Country Status (2)

Country Link
FR (1) FR1150640A (en)
GB (1) GB812317A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2124141A1 (en) * 1971-02-09 1972-09-22 Snecma
FR2587414A1 (en) * 1985-09-17 1987-03-20 Aerospatiale Ramjet with guidance of the air/fuel mixture and missile provided with such a ramjet

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5341640A (en) * 1993-03-30 1994-08-30 Faulkner Robie L Turbojet engine with afterburner and thrust augmentation ejectors
EP2107310A1 (en) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Burner
EP2107312A1 (en) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Pilot combustor in a burner
EP2107309A1 (en) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Quarls in a burner
EP2107313A1 (en) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Fuel staging in a burner
EP2107311A1 (en) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Size scaling of a burner

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2124141A1 (en) * 1971-02-09 1972-09-22 Snecma
FR2587414A1 (en) * 1985-09-17 1987-03-20 Aerospatiale Ramjet with guidance of the air/fuel mixture and missile provided with such a ramjet

Also Published As

Publication number Publication date
GB812317A (en) 1959-04-22

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