DE2153085A1 - Brennkammer, insbesondere Ringbrenn kammer - Google Patents

Brennkammer, insbesondere Ringbrenn kammer

Info

Publication number
DE2153085A1
DE2153085A1 DE19712153085 DE2153085A DE2153085A1 DE 2153085 A1 DE2153085 A1 DE 2153085A1 DE 19712153085 DE19712153085 DE 19712153085 DE 2153085 A DE2153085 A DE 2153085A DE 2153085 A1 DE2153085 A1 DE 2153085A1
Authority
DE
Germany
Prior art keywords
combustion chamber
combustion
flow
fuel
chamber according
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.)
Ceased
Application number
DE19712153085
Other languages
German (de)
English (en)
Inventor
Stanley Joseph East Hart ford Conn Markowski (V St A) F02c 9-04
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.)
RTX Corp
Original Assignee
United Aircraft 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
Application filed by United Aircraft Corp filed Critical United Aircraft Corp
Publication of DE2153085A1 publication Critical patent/DE2153085A1/de
Ceased 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
    • F23R3/34—Feeding into different combustion zones
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38—Introducing air inside the jet
    • F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G2243/00—Stirling type engines having closed regenerative thermodynamic cycles with flow controlled by volume changes
    • F02G2243/30—Stirling type engines having closed regenerative thermodynamic cycles with flow controlled by volume changes having their pistons and displacers each in separate cylinders
    • F02G2243/50—Stirling type engines having closed regenerative thermodynamic cycles with flow controlled by volume changes having their pistons and displacers each in separate cylinders having resonance tubes
    • F02G2243/52—Stirling type engines having closed regenerative thermodynamic cycles with flow controlled by volume changes having their pistons and displacers each in separate cylinders having resonance tubes acoustic
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient 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)
  • Spray-Type Burners (AREA)
DE19712153085 1970-10-26 1971-10-25 Brennkammer, insbesondere Ringbrenn kammer Ceased DE2153085A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US8408670A 1970-10-26 1970-10-26

Publications (1)

Publication Number Publication Date
DE2153085A1 true DE2153085A1 (de) 1972-04-27

Family

ID=22182799

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19712153085 Ceased DE2153085A1 (de) 1970-10-26 1971-10-25 Brennkammer, insbesondere Ringbrenn kammer

Country Status (7)

Country Link
US (1) US3788065A (OSRAM)
AU (1) AU451788B2 (OSRAM)
CA (1) CA954313A (OSRAM)
DE (1) DE2153085A1 (OSRAM)
FR (1) FR2112339B1 (OSRAM)
GB (1) GB1314970A (OSRAM)
SE (1) SE389893B (OSRAM)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2412120A1 (de) * 1973-03-13 1974-09-19 Snecma Umweltfreundliche brennkammer fuer gasturbinen
DE2449084A1 (de) * 1973-10-15 1975-04-17 United Aircraft Corp Wirbelbrennkammer mit turbulenter verbrennung und vermischung
CN112762435A (zh) * 2019-10-21 2021-05-07 王春明 一种燃烧器

Families Citing this family (46)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3999378A (en) * 1974-01-02 1976-12-28 General Electric Company Bypass augmentation burner arrangement for a gas turbine engine
US3974646A (en) * 1974-06-11 1976-08-17 United Technologies Corporation Turbofan engine with augmented combustion chamber using vorbix principle
US4058977A (en) * 1974-12-18 1977-11-22 United Technologies Corporation Low emission combustion chamber
US4045956A (en) * 1974-12-18 1977-09-06 United Technologies Corporation Low emission combustion chamber
US3973390A (en) * 1974-12-18 1976-08-10 United Technologies Corporation Combustor employing serially staged pilot combustion, fuel vaporization, and primary combustion zones
US3973395A (en) * 1974-12-18 1976-08-10 United Technologies Corporation Low emission combustion chamber
US3937008A (en) * 1974-12-18 1976-02-10 United Technologies Corporation Low emission combustion chamber
US3931707A (en) * 1975-01-08 1976-01-13 General Electric Company Augmentor flameholding apparatus
US3993449A (en) * 1975-04-07 1976-11-23 City Of North Olmsted Apparatus for pollution abatement
FR2312653A2 (fr) * 1975-05-30 1976-12-24 Snecma Chambre de combustion anti-pollution pour turbine a gaz
US4012904A (en) * 1975-07-17 1977-03-22 Chrysler Corporation Gas turbine burner
US4204402A (en) * 1976-05-07 1980-05-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Reduction of nitric oxide emissions from a combustor
US4149373A (en) * 1977-08-29 1979-04-17 United Technologies Corporation Combustion chamber stress reducing means
US4194358A (en) * 1977-12-15 1980-03-25 General Electric Company Double annular combustor configuration
US4226083A (en) * 1978-01-19 1980-10-07 United Technologies Corporation Method and apparatus for reducing nitrous oxide emissions from combustors
US4389848A (en) * 1981-01-12 1983-06-28 United Technologies Corporation Burner construction for gas turbines
US4928479A (en) * 1987-12-28 1990-05-29 Sundstrand Corporation Annular combustor with tangential cooling air injection
US5076053A (en) * 1989-08-10 1991-12-31 United Technologies Corporation Mechanism for accelerating heat release of combusting flows
US5207064A (en) * 1990-11-21 1993-05-04 General Electric Company Staged, mixed combustor assembly having low emissions
US5197278A (en) * 1990-12-17 1993-03-30 General Electric Company Double dome combustor and method of operation
US5406799A (en) * 1992-06-12 1995-04-18 United Technologies Corporation Combustion chamber
FR2694624B1 (fr) * 1992-08-05 1994-09-23 Snecma Chambre de combustion à plusieurs injecteurs de carburant.
US5335501A (en) * 1992-11-16 1994-08-09 General Electric Company Flow spreading diffuser
US5470224A (en) * 1993-07-16 1995-11-28 Radian Corporation Apparatus and method for reducing NOx , CO and hydrocarbon emissions when burning gaseous fuels
US5407347A (en) * 1993-07-16 1995-04-18 Radian Corporation Apparatus and method for reducing NOx, CO and hydrocarbon emissions when burning gaseous fuels
JPH08270950A (ja) * 1995-02-01 1996-10-18 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器
EP0813670B1 (de) * 1995-03-08 2000-06-28 Rolls-Royce Deutschland GmbH Axial gestufte doppelring-brennkammer einer gasturbine
US6125627A (en) * 1998-08-11 2000-10-03 Allison Advanced Development Company Method and apparatus for spraying fuel within a gas turbine engine
DE59812944D1 (de) * 1998-09-16 2005-08-25 Alstom Technology Ltd Baden Verfahren zur Verhinderung von Strömungsinstabilitäten in einem Brenner
MX354577B (es) * 2002-10-10 2018-03-12 Lpp Comb Llc Sistema para la evaporación de combustibles líquidos para la combustión y método de uso.
NZ555544A (en) * 2004-12-08 2011-05-27 Lpp Comb Llc Fuel conditioning unit comprising at least one nozzle mounted on the end wall of the vaporization chamber
US8529646B2 (en) * 2006-05-01 2013-09-10 Lpp Combustion Llc Integrated system and method for production and vaporization of liquid hydrocarbon fuels for combustion
US7827797B2 (en) * 2006-09-05 2010-11-09 General Electric Company Injection assembly for a combustor
EP2006606A1 (de) * 2007-06-21 2008-12-24 Siemens Aktiengesellschaft Drallfreie Stabilisierung der Flamme eines Vormischbrenners
US7775791B2 (en) * 2008-02-25 2010-08-17 General Electric Company Method and apparatus for staged combustion of air and fuel
FR2941742B1 (fr) * 2009-02-05 2011-08-19 Snecma Ensemble diffuseur-redresseur pour une turbomachine
RU2534189C2 (ru) * 2010-02-16 2014-11-27 Дженерал Электрик Компани Камера сгорания для газовой турбины(варианты) и способ эксплуатации газовой турбины
ES2488404T3 (es) * 2011-03-07 2014-08-27 Eads Construcciones Aeronáuticas, S.A. Sistema de evacuación de flujo para un motor de aeronave
EP2500640A1 (en) * 2011-03-16 2012-09-19 L'AIR LIQUIDE, Société Anonyme pour l'Etude et l'Exploitation des Procédés Georges Claude Low NOx combustion process and burner therefor
CA2844693A1 (en) * 2011-08-11 2013-02-14 Beckett Gas, Inc. Combustor
US8943832B2 (en) * 2011-10-26 2015-02-03 General Electric Company Fuel nozzle assembly for use in turbine engines and methods of assembling same
EP2644997A1 (en) * 2012-03-26 2013-10-02 Alstom Technology Ltd Mixing arrangement for mixing fuel with a stream of oxygen containing gas
US9677766B2 (en) * 2012-11-28 2017-06-13 General Electric Company Fuel nozzle for use in a turbine engine and method of assembly
EP2837771A1 (de) * 2013-08-16 2015-02-18 Siemens Aktiengesellschaft Auslegung eines Axialdiffusors unter Berücksichtigung von Einbauten
US10876407B2 (en) * 2017-02-16 2020-12-29 General Electric Company Thermal structure for outer diameter mounted turbine blades
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2477683A (en) * 1942-09-30 1949-08-02 Turbo Engineering Corp Compressed air and combustion gas flow in turbine power plant
DE847091C (de) * 1944-05-13 1952-08-21 Daimler Benz Ag Heissluftstrahltriebwerk
US2720750A (en) * 1947-11-04 1955-10-18 Helmut R Schelp Revolving fuel injection system for jet engines and gas turbines
US2627720A (en) * 1948-10-08 1953-02-10 Packard Motor Car Co Circumferentially arranged combustion chamber with arcuate walls defining an air flow path between chambers
US2773350A (en) * 1950-01-31 1956-12-11 Hillard E Barrett Combustion chamber assembly for ram jet fuel burner
BE502037A (OSRAM) * 1950-03-21
US3002351A (en) * 1951-01-26 1961-10-03 David H Sloan Ramjet device
US3088281A (en) * 1956-04-03 1963-05-07 Bristol Siddeley Engines Ltd Combustion chambers for use with swirling combustion supporting medium
US2945349A (en) * 1957-11-12 1960-07-19 Lear Inc Miniature gas turbine
US3034297A (en) * 1958-12-15 1962-05-15 Bristol Siddeley Engines Ltd Combustion chambers
FR1094871A (fr) * 1959-01-22 1955-05-25 Thomson Houston Comp Francaise Perfectionnements aux appareils de combustion à combustible injecté
US3078672A (en) * 1959-03-28 1963-02-26 Maschf Augsburg Nuernberg Ag Process and apparatus for operating a continuous or intermittent combustion engine
US3373562A (en) * 1966-03-17 1968-03-19 Wingaersheek Turbine Co Inc Combustion chamber for gas turbines and the like having improved flame holder
GB1170255A (en) * 1966-07-01 1969-11-12 Rolls Royce Combustion Apparatus.
US3393516A (en) * 1966-12-05 1968-07-23 United Aircraft Corp Curved exhaust deflector

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2412120A1 (de) * 1973-03-13 1974-09-19 Snecma Umweltfreundliche brennkammer fuer gasturbinen
DE2449084A1 (de) * 1973-10-15 1975-04-17 United Aircraft Corp Wirbelbrennkammer mit turbulenter verbrennung und vermischung
CN112762435A (zh) * 2019-10-21 2021-05-07 王春明 一种燃烧器

Also Published As

Publication number Publication date
FR2112339B1 (OSRAM) 1976-03-26
CA954313A (en) 1974-09-10
AU451788B2 (en) 1974-08-15
US3788065A (en) 1974-01-29
SE7401957L (OSRAM) 1974-02-14
FR2112339A1 (OSRAM) 1972-06-16
SE389893B (sv) 1976-11-22
AU3177971A (en) 1973-02-01
GB1314970A (en) 1973-04-26

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Legal Events

Date Code Title Description
OGA New person/name/address of the applicant
OD Request for examination
8131 Rejection