GB751098A - Improvements in combustion devices particularly applicable to aircraft jet propulsion units - Google Patents

Improvements in combustion devices particularly applicable to aircraft jet propulsion units

Info

Publication number
GB751098A
GB751098A GB16800/55A GB1680055A GB751098A GB 751098 A GB751098 A GB 751098A GB 16800/55 A GB16800/55 A GB 16800/55A GB 1680055 A GB1680055 A GB 1680055A GB 751098 A GB751098 A GB 751098A
Authority
GB
United Kingdom
Prior art keywords
nozzle
gas
fuel
disposed
gaseous
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
GB16800/55A
Other languages
English (en)
Inventor
Gilbert Racine
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
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 filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of GB751098A publication Critical patent/GB751098A/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
    • F23R3/02—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
    • F23R3/24—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants of the fluid-screen type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D1/00—Burners for combustion of pulverulent fuel
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Testing Of Engines (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
GB16800/55A 1953-06-27 1953-09-16 Improvements in combustion devices particularly applicable to aircraft jet propulsion units Expired GB751098A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR270653X 1953-06-27
FR1063505T 1953-06-27

Publications (1)

Publication Number Publication Date
GB751098A true GB751098A (en) 1956-06-27

Family

ID=26214381

Family Applications (2)

Application Number Title Priority Date Filing Date
GB25628/53A Expired GB751013A (en) 1953-06-27 1953-09-16 Improvements in combustion devices particularly applicable to aircraft jet propulsion units
GB16800/55A Expired GB751098A (en) 1953-06-27 1953-09-16 Improvements in combustion devices particularly applicable to aircraft jet propulsion units

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB25628/53A Expired GB751013A (en) 1953-06-27 1953-09-16 Improvements in combustion devices particularly applicable to aircraft jet propulsion units

Country Status (5)

Country Link
CH (1) CH323717A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE1049640B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR1063505A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
GB (2) GB751013A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
NL (1) NL105199C (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2948117A (en) * 1956-10-01 1960-08-09 Gen Electric Afterburner flameholder
EP0750164A1 (en) * 1995-06-21 1996-12-27 United Technologies Corporation Method for distributing fuel within an augmentor

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1084980B (de) * 1954-08-03 1960-07-07 Snecma Rueckstossantrieb
DE1138588B (de) * 1960-03-01 1962-10-25 Entwicklungsbau Pirna Veb Ringbrennkammer mit einer rotierenden Kraftstoffeinspritzeinrichtung, insbesondere fuer Kleingasturbinen
DE1235670B (de) * 1962-11-06 1967-03-02 Deutsche Forsch Luft Raumfahrt Vorrichtung zur Flammenstabilisierung in Gleichdruck-Brennkammern
DE1301338B (de) * 1963-08-24 1969-08-21 Hans Dipl Ing Vorrichtung zum Nachverbrennen von Abgasen aus Verbrennungsmotoren
GB1139004A (en) * 1966-02-28 1969-01-08 Mini Of Technology Improvements in or relating to combustion devices
US4137712A (en) * 1976-07-06 1979-02-06 The United States Of America As Represented By The Secretary Of The Navy Fluidic combustion control of a solid fuel ramjet
US6125627A (en) * 1998-08-11 2000-10-03 Allison Advanced Development Company Method and apparatus for spraying fuel within a gas turbine engine
US20110219776A1 (en) * 2010-03-15 2011-09-15 General Electric Company Aerodynamic flame stabilizer
CN113551262B (zh) * 2021-07-19 2022-06-14 南昌航空大学 一种带新月沙丘型面的支板火焰稳定器

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2948117A (en) * 1956-10-01 1960-08-09 Gen Electric Afterburner flameholder
EP0750164A1 (en) * 1995-06-21 1996-12-27 United Technologies Corporation Method for distributing fuel within an augmentor

Also Published As

Publication number Publication date
CH323717A (fr) 1957-08-15
FR1063505A (fr) 1954-05-04
GB751013A (en) 1956-06-27
NL105199C (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE1049640B (de) 1959-01-29

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