FR1166520A - Pilot burner for reactors - Google Patents

Pilot burner for reactors

Info

Publication number
FR1166520A
FR1166520A FR1166520DA FR1166520A FR 1166520 A FR1166520 A FR 1166520A FR 1166520D A FR1166520D A FR 1166520DA FR 1166520 A FR1166520 A FR 1166520A
Authority
FR
France
Prior art keywords
reactors
pilot burner
burner
pilot
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)
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.)
Continental Aviation and Engineering Corp
Original Assignee
Continental Aviation and Engineering Corp
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
Priority claimed from GB3543456A external-priority patent/GB812209A/en
Application filed by Continental Aviation and Engineering Corp filed Critical Continental Aviation and Engineering Corp
Application granted granted Critical
Publication of FR1166520A publication Critical patent/FR1166520A/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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous 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
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • 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
    • F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1166520D 1956-11-20 1956-12-12 Pilot burner for reactors Expired FR1166520A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3543456A GB812209A (en) 1956-11-20 Pilot burner for jet engines

Publications (1)

Publication Number Publication Date
FR1166520A true FR1166520A (en) 1958-11-12

Family

ID=10377674

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1166520D Expired FR1166520A (en) 1956-11-20 1956-12-12 Pilot burner for reactors

Country Status (1)

Country Link
FR (1) FR1166520A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2402077A1 (en) * 1975-06-30 1979-03-30 Gen Electric MANEUVERABLE IN-FLIGHT EJECTION DEVICE FOR A GAS TURBINE ENGINE
EP0059490A1 (en) * 1981-03-04 1982-09-08 BBC Aktiengesellschaft Brown, Boveri & Cie. Annular combustion chamber with an annular burner for gas turbines
FR2706588A1 (en) * 1993-06-16 1994-12-23 Snecma Fuel injection system for combustion chamber

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2402077A1 (en) * 1975-06-30 1979-03-30 Gen Electric MANEUVERABLE IN-FLIGHT EJECTION DEVICE FOR A GAS TURBINE ENGINE
EP0059490A1 (en) * 1981-03-04 1982-09-08 BBC Aktiengesellschaft Brown, Boveri & Cie. Annular combustion chamber with an annular burner for gas turbines
FR2706588A1 (en) * 1993-06-16 1994-12-23 Snecma Fuel injection system for combustion chamber
US5437159A (en) * 1993-06-16 1995-08-01 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (S.N.E.C.M.A.) Fuel injection system for a gas turbine combustor including radial fuel spray arms and V-gutter flameholders

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