DE2460740C3 - Brennkammer für Gasturbinentriebwerke - Google Patents

Brennkammer für Gasturbinentriebwerke

Info

Publication number
DE2460740C3
DE2460740C3 DE2460740A DE2460740A DE2460740C3 DE 2460740 C3 DE2460740 C3 DE 2460740C3 DE 2460740 A DE2460740 A DE 2460740A DE 2460740 A DE2460740 A DE 2460740A DE 2460740 C3 DE2460740 C3 DE 2460740C3
Authority
DE
Germany
Prior art keywords
fuel
combustion
flame tube
combustion chamber
air
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
DE2460740A
Other languages
German (de)
English (en)
Other versions
DE2460740B2 (de
DE2460740A1 (de
Inventor
Adolf 8091 Pfaffing Fehler
Guenter 8000 Muenchen Kirschey
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Priority to DE2460740A priority Critical patent/DE2460740C3/de
Priority to GB49017/75A priority patent/GB1516868A/en
Priority to US05/641,086 priority patent/US4062182A/en
Priority to FR7539272A priority patent/FR2295237A1/fr
Publication of DE2460740A1 publication Critical patent/DE2460740A1/de
Publication of DE2460740B2 publication Critical patent/DE2460740B2/de
Application granted granted Critical
Publication of DE2460740C3 publication Critical patent/DE2460740C3/de
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
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
DE2460740A 1974-12-21 1974-12-21 Brennkammer für Gasturbinentriebwerke Expired DE2460740C3 (de)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE2460740A DE2460740C3 (de) 1974-12-21 1974-12-21 Brennkammer für Gasturbinentriebwerke
GB49017/75A GB1516868A (en) 1974-12-21 1975-11-28 Combustion chamber for gas turbine engines
US05/641,086 US4062182A (en) 1974-12-21 1975-12-15 Combustion chamber for gas turbine engines
FR7539272A FR2295237A1 (fr) 1974-12-21 1975-12-22 Chambre de combustion pour groupes propulseurs a turbine a gaz

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2460740A DE2460740C3 (de) 1974-12-21 1974-12-21 Brennkammer für Gasturbinentriebwerke

Publications (3)

Publication Number Publication Date
DE2460740A1 DE2460740A1 (de) 1976-07-01
DE2460740B2 DE2460740B2 (de) 1980-01-24
DE2460740C3 true DE2460740C3 (de) 1980-09-18

Family

ID=5934175

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2460740A Expired DE2460740C3 (de) 1974-12-21 1974-12-21 Brennkammer für Gasturbinentriebwerke

Country Status (4)

Country Link
US (1) US4062182A (cg-RX-API-DMAC10.html)
DE (1) DE2460740C3 (cg-RX-API-DMAC10.html)
FR (1) FR2295237A1 (cg-RX-API-DMAC10.html)
GB (1) GB1516868A (cg-RX-API-DMAC10.html)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0587580B2 (en) † 1991-06-07 2001-02-07 ROLLS-ROYCE plc Gas turbine engine combustor

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
GB1575410A (en) * 1976-09-04 1980-09-24 Rolls Royce Combustion apparatus for use in gas turbine engines
GB1581531A (en) * 1976-09-09 1980-12-17 Rolls Royce Control of airflow in combustion chambers by variable rate diffuser
US4380895A (en) * 1976-09-09 1983-04-26 Rolls-Royce Limited Combustion chamber for a gas turbine engine having a variable rate diffuser upstream of air inlet means
US4253301A (en) 1978-10-13 1981-03-03 General Electric Company Fuel injection staged sectoral combustor for burning low-BTU fuel gas
US4265615A (en) * 1978-12-11 1981-05-05 United Technologies Corporation Fuel injection system for low emission burners
US4265085A (en) * 1979-05-30 1981-05-05 United Technologies Corporation Radially staged low emission can-annular combustor
DE2937631A1 (de) * 1979-09-18 1981-04-02 Daimler-Benz Ag, 7000 Stuttgart Brennkammer fuer gasturbinen
US4343147A (en) * 1980-03-07 1982-08-10 Solar Turbines Incorporated Combustors and combustion systems
GB2161914B (en) * 1980-12-10 1986-06-11 Rolls Royce Combustion equipment for a gas turbine engine
US4835960A (en) * 1982-07-22 1989-06-06 Skoczkowski Andzej M High compression gas turbine engine
DE3241162A1 (de) * 1982-11-08 1984-05-10 Kraftwerk Union AG, 4330 Mülheim Vormischbrenner mit integriertem diffusionsbrenner
US4765136A (en) * 1985-11-25 1988-08-23 United Technologies Corporation Gas turbine engine augmentor
JP2852110B2 (ja) * 1990-08-20 1999-01-27 株式会社日立製作所 燃焼装置及びガスタービン装置
US5408825A (en) * 1993-12-03 1995-04-25 Westinghouse Electric Corporation Dual fuel gas turbine combustor
DE19614001A1 (de) * 1996-04-09 1997-10-16 Abb Research Ltd Brennkammer
US5867980A (en) * 1996-12-17 1999-02-09 General Electric Company Turbofan engine with a low pressure turbine driven supercharger in a bypass duct operated by a fuel rich combustor and an afterburner
US6826913B2 (en) 2002-10-31 2004-12-07 Honeywell International Inc. Airflow modulation technique for low emissions combustors
EP1950494A1 (de) * 2007-01-29 2008-07-30 Siemens Aktiengesellschaft Brennkammer für eine Gasturbine
EP2107311A1 (en) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Size scaling of a burner
FR3039254B1 (fr) * 2015-07-24 2021-10-08 Snecma Chambre de combustion comportant des dispositifs d'injection additionnels debouchant directement dans les zones de recirculation de coin, turbomachine la comprenant, et procede d'alimentation en carburant de celle-ci
DE102016201452A1 (de) 2016-02-01 2017-08-03 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit Wandkonturierung
RU2757705C1 (ru) 2021-01-13 2021-10-20 Роман Лазирович Илиев Горелка с двухслойным вихревым противоточным течением
US11566790B1 (en) * 2021-10-28 2023-01-31 General Electric Company Methods of operating a turbomachine combustor on hydrogen
US11940151B2 (en) 2022-01-12 2024-03-26 General Electric Company Combustor with baffle
US12018839B2 (en) 2022-10-20 2024-06-25 General Electric Company Gas turbine engine combustor with dilution passages
US12158270B2 (en) 2022-12-20 2024-12-03 General Electric Company Gas turbine engine combustor with a set of dilution passages

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2931174A (en) * 1952-12-20 1960-04-05 Armstrong Siddeley Motors Ltd Vaporizer for liquid fuel
DE1074920B (de) * 1955-07-07 1960-02-04 Ing habil Fritz A F Schmidt Murnau Dr (Obb) Verfahren und \ orrichtung zur Regelung von Gas turbmenbrennkammern mit unterteilter Verbrennung und mehreren Druckstufen
FR1166154A (fr) * 1957-02-01 1958-11-04 Snecma Brûleur à semi-vaporisation
GB854135A (en) * 1958-03-05 1960-11-16 Rolls Royce Improvements in or relating to combustion equipment
GB1357533A (en) * 1970-09-11 1974-06-26 Lucas Industries Ltd Combustion equipment for gas turbine engines
US3811277A (en) * 1970-10-26 1974-05-21 United Aircraft Corp Annular combustion chamber for dissimilar fluids in swirling flow relationship
US3729285A (en) * 1972-05-22 1973-04-24 G Schwedersky Burner and method of operating it to control the production of nitrogen oxides
FR2221621B1 (cg-RX-API-DMAC10.html) * 1973-03-13 1976-09-10 Snecma
US3925002A (en) * 1974-11-11 1975-12-09 Gen Motors Corp Air preheating combustion apparatus
US3946553A (en) * 1975-03-10 1976-03-30 United Technologies Corporation Two-stage premixed combustor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0587580B2 (en) † 1991-06-07 2001-02-07 ROLLS-ROYCE plc Gas turbine engine combustor

Also Published As

Publication number Publication date
DE2460740B2 (de) 1980-01-24
DE2460740A1 (de) 1976-07-01
FR2295237A1 (fr) 1976-07-16
FR2295237B1 (cg-RX-API-DMAC10.html) 1982-09-17
US4062182A (en) 1977-12-13
GB1516868A (en) 1978-07-05

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Legal Events

Date Code Title Description
OGA New person/name/address of the applicant
C3 Grant after two publication steps (3rd publication)
8339 Ceased/non-payment of the annual fee