FR1515329A - Dispositif de combustion - Google Patents

Dispositif de combustion

Info

Publication number
FR1515329A
FR1515329A FR96673A FR96673A FR1515329A FR 1515329 A FR1515329 A FR 1515329A FR 96673 A FR96673 A FR 96673A FR 96673 A FR96673 A FR 96673A FR 1515329 A FR1515329 A FR 1515329A
Authority
FR
France
Prior art keywords
combustion device
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
FR96673A
Other languages
English (en)
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.)
MINI OF TECHNOLOGY
Original Assignee
MINI OF TECHNOLOGY
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 MINI OF TECHNOLOGY filed Critical MINI OF TECHNOLOGY
Application granted granted Critical
Publication of FR1515329A publication Critical patent/FR1515329A/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
    • F23R3/16—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
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/108—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel intersecting downstream of the burner outlet
FR96673A 1966-02-28 1967-02-27 Dispositif de combustion Expired FR1515329A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8649/66A GB1139004A (en) 1966-02-28 1966-02-28 Improvements in or relating to combustion devices

Publications (1)

Publication Number Publication Date
FR1515329A true FR1515329A (fr) 1968-03-01

Family

ID=9856548

Family Applications (1)

Application Number Title Priority Date Filing Date
FR96673A Expired FR1515329A (fr) 1966-02-28 1967-02-27 Dispositif de combustion

Country Status (4)

Country Link
US (1) US3455108A (fr)
DE (1) DE1601610A1 (fr)
FR (1) FR1515329A (fr)
GB (1) GB1139004A (fr)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1184379A (en) * 1967-08-10 1970-03-18 Mini Of Technology London Improvements in or relat ing to Combustion Devices
US3913319A (en) * 1972-02-02 1975-10-21 Us Navy Low drag flameholder
DE2255306C3 (de) * 1972-11-11 1975-06-12 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Aerodynamische Flammenhalterung für luftatmende Strahltriebwerke
US4170110A (en) * 1976-07-19 1979-10-09 Edward Radin Combustion process
DE3819899C1 (en) * 1988-06-11 1989-11-30 Daimler-Benz Aktiengesellschaft, 7000 Stuttgart, De Apparatus for generating a homogeneous mixture from a first and second medium
DE3942042A1 (de) * 1989-12-20 1991-06-27 Bmw Rolls Royce Gmbh Brennkammer fuer eine gasturbine mit luftunterstuetzten brennstoffzerstaeuberduesen
DE59104727D1 (de) * 1991-12-23 1995-03-30 Asea Brown Boveri Vorrichtung für die Vermischung zweier gasförmiger Komponenten und Brenner, in welchem diese Vorrichtung eingesetzt wird.
US5647215A (en) * 1995-11-07 1997-07-15 Westinghouse Electric Corporation Gas turbine combustor with turbulence enhanced mixing fuel injectors
US6339925B1 (en) * 1998-11-02 2002-01-22 General Electric Company Hybrid catalytic combustor
US7003961B2 (en) * 2001-07-23 2006-02-28 Ramgen Power Systems, Inc. Trapped vortex combustor
US7603841B2 (en) * 2001-07-23 2009-10-20 Ramgen Power Systems, Llc Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel
US6694743B2 (en) 2001-07-23 2004-02-24 Ramgen Power Systems, Inc. Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall
ITMI20012780A1 (it) * 2001-12-21 2003-06-21 Nuovo Pignone Spa Dispositivo di iniezione principale di combustibile liquido per camera di combustione singola dotata di camera di pre-miscelamento di una tu
US6968694B2 (en) * 2003-03-13 2005-11-29 United Technologies Corporation Augmentor
US6971239B2 (en) * 2003-05-13 2005-12-06 United Technologies Corporation Augmentor pilot nozzle
US20080196414A1 (en) * 2005-03-22 2008-08-21 Andreadis Dean E Strut cavity pilot and fuel injector assembly
EP1821035A1 (fr) * 2006-02-15 2007-08-22 Siemens Aktiengesellschaft Brûleur de turbine à gaz et procédé pour mélanger le carburant et l'air dans une zone de tourbillonage d'un brûleur de turbine à gaz
EP1918638A1 (fr) * 2006-10-25 2008-05-07 Siemens AG Brûleur, en particulier pour une turbine à gaz
EP2107301B1 (fr) * 2008-04-01 2016-01-06 Siemens Aktiengesellschaft Injection de gaz dans un brûleur
US8291705B2 (en) * 2008-08-13 2012-10-23 General Electric Company Ultra low injection angle fuel holes in a combustor fuel nozzle
US8851402B2 (en) * 2009-02-12 2014-10-07 General Electric Company Fuel injection for gas turbine combustors
CN101551120B (zh) * 2009-05-11 2010-09-08 哈尔滨工业大学 带有驻涡结构的涡轮冷却叶栅
FR2958015B1 (fr) * 2010-03-24 2013-07-05 Snecma Systeme d'injection pour chambre de combustion de turbomachine, comprenant des moyens d'injection de carburant entre deux flux d'air coaxiaux
US8572981B2 (en) * 2010-11-08 2013-11-05 General Electric Company Self-oscillating fuel injection jets
US20120167550A1 (en) * 2010-12-30 2012-07-05 Victor Lewis Oechsle Thrust augmented gas turbine engine
EP2743588A1 (fr) * 2012-12-11 2014-06-18 Siemens Aktiengesellschaft Positionnement d'injecteur de carburant en retrait
EP2743581A1 (fr) * 2012-12-11 2014-06-18 Siemens Aktiengesellschaft Injection de carburant à air dirigé
US10393020B2 (en) * 2015-08-26 2019-08-27 Rohr, Inc. Injector nozzle configuration for swirl anti-icing system
US10941938B2 (en) * 2018-02-22 2021-03-09 Delavan Inc. Fuel injectors including gas fuel injection

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1049640B (de) * 1953-06-27 1959-01-29 Sociote Nationale cFEtude et de Construction de Moteurs d'Aviation, Paris Einrichtung zum Verbrennen eines Brennstoffes in einem gasförmigen, mit hoher Geschwindigkeit strömenden Verbrennungsmedium
US2979899A (en) * 1953-06-27 1961-04-18 Snecma Flame spreading device for combustion equipments
US2948117A (en) * 1956-10-01 1960-08-09 Gen Electric Afterburner flameholder
US3328958A (en) * 1963-06-05 1967-07-04 United Aircraft Corp Aerodynamic-type flameholder

Also Published As

Publication number Publication date
DE1601610A1 (de) 1971-01-07
US3455108A (en) 1969-07-15
GB1139004A (en) 1969-01-08

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