DE2232025A1 - Gasturbinenanlage, insbesondere triebwerk mit gleichraumverbrennung - Google Patents

Gasturbinenanlage, insbesondere triebwerk mit gleichraumverbrennung

Info

Publication number
DE2232025A1
DE2232025A1 DE2232025A DE2232025A DE2232025A1 DE 2232025 A1 DE2232025 A1 DE 2232025A1 DE 2232025 A DE2232025 A DE 2232025A DE 2232025 A DE2232025 A DE 2232025A DE 2232025 A1 DE2232025 A1 DE 2232025A1
Authority
DE
Germany
Prior art keywords
gas turbine
plant according
combustion chamber
compressor
turbine plant
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.)
Pending
Application number
DE2232025A
Other languages
German (de)
English (en)
Inventor
Hermann Dipl Ing Dr Tech Hagen
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 DE2232025A priority Critical patent/DE2232025A1/de
Priority to GB3079873A priority patent/GB1439255A/en
Priority to FR7324015A priority patent/FR2191022B3/fr
Priority to US375755A priority patent/US3877219A/en
Publication of DE2232025A1 publication Critical patent/DE2232025A1/de
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/12Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Combustion Of Fluid Fuel (AREA)
DE2232025A 1972-06-30 1972-06-30 Gasturbinenanlage, insbesondere triebwerk mit gleichraumverbrennung Pending DE2232025A1 (de)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE2232025A DE2232025A1 (de) 1972-06-30 1972-06-30 Gasturbinenanlage, insbesondere triebwerk mit gleichraumverbrennung
GB3079873A GB1439255A (en) 1972-06-30 1973-06-28 Gas turbine engine having substantially constant-volume combustion
FR7324015A FR2191022B3 (enExample) 1972-06-30 1973-06-29
US375755A US3877219A (en) 1972-06-30 1973-07-02 Constant volume combustion gas turbine with intermittent flows

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2232025A DE2232025A1 (de) 1972-06-30 1972-06-30 Gasturbinenanlage, insbesondere triebwerk mit gleichraumverbrennung

Publications (1)

Publication Number Publication Date
DE2232025A1 true DE2232025A1 (de) 1974-01-17

Family

ID=5849242

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2232025A Pending DE2232025A1 (de) 1972-06-30 1972-06-30 Gasturbinenanlage, insbesondere triebwerk mit gleichraumverbrennung

Country Status (4)

Country Link
US (1) US3877219A (enExample)
DE (1) DE2232025A1 (enExample)
FR (1) FR2191022B3 (enExample)
GB (1) GB1439255A (enExample)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT379217B (de) * 1982-10-27 1985-12-10 Lorenz Edmund Impulsgesteuerte gasturbine
US4693073A (en) * 1986-07-18 1987-09-15 Sundstrand Corporation Method and apparatus for starting a gas turbine engine
US4702072A (en) * 1984-08-20 1987-10-27 Gerhard Kielhorn Internal combustion engine
US9062606B2 (en) 2008-08-26 2015-06-23 Edmund Lorenz Combustion turbine in which combustion is intermittent

Families Citing this family (31)

* Cited by examiner, † Cited by third party
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US5237811A (en) * 1990-12-26 1993-08-24 Stockwell James K Rotary internal combustion engine apparatus
US6003301A (en) * 1993-04-14 1999-12-21 Adroit Systems, Inc. Exhaust nozzle for multi-tube detonative engines
US5345758A (en) * 1993-04-14 1994-09-13 Adroit Systems, Inc. Rotary valve multiple combustor pulse detonation engine
US5966927A (en) * 1997-03-31 1999-10-19 Wilson; Michael A. Efficiency enhanced turbine engine
US6105359A (en) * 1997-03-31 2000-08-22 Wilson; Michael A. Efficiency enhanced turbine engine
DE19860583A1 (de) * 1998-12-29 2000-07-06 Abb Alstom Power Ch Ag Brennkammer für eine Gasturbine
US6212875B1 (en) 1999-04-07 2001-04-10 Brian F. Lewis Direct fired compressor and method of producing compressed air
US6370864B1 (en) * 2000-09-12 2002-04-16 Richard V. Murphy Turbine engine with valve mechanism and integral combustion chamber
FR2829528B1 (fr) * 2001-09-07 2004-02-27 Bernard Gilbert Macarez Pulsomoteur-turbomoteur a impulsion-turbine a gaz a chambre de combustion impulsionnelle et a detente de bouffees
US7124571B2 (en) * 2002-02-28 2006-10-24 Stanevicius Algimantas Aleksan Rotary internal combustion engine
WO2004072451A1 (en) * 2003-02-12 2004-08-26 Ishikawajima-Harima Heavy Industries Co., Ltd. Pulse detonation engine system for driving turbine
US7096674B2 (en) 2004-09-15 2006-08-29 General Electric Company High thrust gas turbine engine with improved core system
US7093446B2 (en) * 2004-09-15 2006-08-22 General Electric Company Gas turbine engine having improved core system
US20060053801A1 (en) * 2004-09-15 2006-03-16 Orlando Robert J Cooling system for gas turbine engine having improved core system
US7448200B2 (en) * 2005-03-24 2008-11-11 United Technologies Corporation Pulse combustion device
US7500348B2 (en) * 2005-03-24 2009-03-10 United Technologies Corporation Pulse combustion device
GB0822676D0 (en) * 2008-12-12 2009-01-21 Rolls Royce Plc A gas turbine engine
US8701418B2 (en) * 2009-01-07 2014-04-22 General Electric Company Late lean injection for fuel flexibility
US8707707B2 (en) * 2009-01-07 2014-04-29 General Electric Company Late lean injection fuel staging configurations
US8701383B2 (en) 2009-01-07 2014-04-22 General Electric Company Late lean injection system configuration
US8112216B2 (en) 2009-01-07 2012-02-07 General Electric Company Late lean injection with adjustable air splits
US8701382B2 (en) * 2009-01-07 2014-04-22 General Electric Company Late lean injection with expanded fuel flexibility
US8683808B2 (en) * 2009-01-07 2014-04-01 General Electric Company Late lean injection control strategy
US8377232B2 (en) * 2009-05-04 2013-02-19 General Electric Company On-line cleaning of turbine hot gas path deposits via pressure pulsations
RU2553589C2 (ru) * 2012-08-28 2015-06-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Способ функционирования сверхзвукового пульсирующего детонационного прямоточного воздушно-реактивного двигателя
FR3032781B1 (fr) * 2015-02-17 2018-07-06 Safran Helicopter Engines Systeme de combustion a volume constant pour turbomachine de moteur d'aeronef
US20160298545A1 (en) * 2015-04-13 2016-10-13 General Electric Company Turbine airfoil
FR3037384B1 (fr) * 2015-06-11 2017-06-23 Turbomeca Module de chambre de combustion cvc de turbomachine comportant une prechambre de combustion
RU2610362C1 (ru) * 2015-10-06 2017-02-09 федеральное государственное автономное образовательное учреждение высшего образования "Самарский государственный аэрокосмический университет имени академика С.П. Королева (национальный исследовательский университет)" (СГАУ) Способ работы и устройство блока пульсирующих камер сгорания
RU2663607C1 (ru) * 2017-10-05 2018-08-07 Общество с ограниченной ответственностью "Новые физические принципы" Энергетическая установка с импульсно-детонационным сжиганием горючего
CN114207356B (zh) * 2019-06-09 2024-04-19 芬诺能源有限公司 控制无活塞燃烧器中的爆燃燃烧过程的方法

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1552272A (en) * 1921-04-18 1925-09-01 Carner James Frederick Explosive engine or turbine
US2427845A (en) * 1941-07-08 1947-09-23 Fairey Aviat Co Ltd Periodically actuated jet motor
US2479143A (en) * 1944-12-07 1949-08-16 Jr Samuel W Traylor Gas turbine
US2608055A (en) * 1948-04-29 1952-08-26 English Electric Co Ltd Gas turbine plant, including multiple fluid operated motors with treatment between stages
US2738645A (en) * 1949-10-22 1956-03-20 So Called Cie Electro Mecaniqu Multistage turbojet engine having auxiliary nozzles located in an intermediate stage
US2640314A (en) * 1949-12-16 1953-06-02 William E Abel Disk valve pulse jet engine
US2809493A (en) * 1951-03-19 1957-10-15 American Mach & Foundry Centrifugal flow compressor and gas turbine power plant with a centrifugal flow compressor, toroidal combustion chamber, and centripetal flow turbine
US2937498A (en) * 1953-01-13 1960-05-24 Fritz A F Schmidt Mechanically controlled multistage combustion chambers for gas-impulsetype engines and improved discharge control therefor
US3034298A (en) * 1958-06-12 1962-05-15 Gen Motors Corp Turbine cooling system
US3269119A (en) * 1960-03-16 1966-08-30 Nathan C Price Turbo-jet powerplant with toroidal combustion chamber
US3018623A (en) * 1960-11-04 1962-01-30 Birmann Rudolph Explosion gas turbines
FR1424457A (fr) * 1964-11-30 1966-01-14 Perfectionnements apportés aux chambres de combustion des moteurs à turbine à gaz
AT260624B (de) * 1965-04-01 1968-03-11 Wilhelm Kuesters Verfahren zum Betrieb eines oder mehrerer pulsierend arbeitender Brennrohre und Vorrichtung zur Durchführung des Verfahrens
DE2042478C3 (de) * 1970-08-27 1975-08-14 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Gasturbinentriebwerk, vorzugsweise Strahltriebwerk für Flugzeuge, mit Kühlluft- und gegebenenfalls Sperrluftentnahme
US3736747A (en) * 1971-07-09 1973-06-05 G Warren Combustor

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT379217B (de) * 1982-10-27 1985-12-10 Lorenz Edmund Impulsgesteuerte gasturbine
US4702072A (en) * 1984-08-20 1987-10-27 Gerhard Kielhorn Internal combustion engine
US4693073A (en) * 1986-07-18 1987-09-15 Sundstrand Corporation Method and apparatus for starting a gas turbine engine
US9062606B2 (en) 2008-08-26 2015-06-23 Edmund Lorenz Combustion turbine in which combustion is intermittent

Also Published As

Publication number Publication date
US3877219A (en) 1975-04-15
GB1439255A (en) 1976-06-16
FR2191022A1 (enExample) 1974-02-01
FR2191022B3 (enExample) 1976-06-18

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Legal Events

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