FR2433110B3 - - Google Patents

Info

Publication number
FR2433110B3
FR2433110B3 FR7919271A FR7919271A FR2433110B3 FR 2433110 B3 FR2433110 B3 FR 2433110B3 FR 7919271 A FR7919271 A FR 7919271A FR 7919271 A FR7919271 A FR 7919271A FR 2433110 B3 FR2433110 B3 FR 2433110B3
Authority
FR
France
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
FR7919271A
Other versions
FR2433110A1 (fr
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 GmbH
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
Publication of FR2433110A1 publication Critical patent/FR2433110A1/fr
Application granted granted Critical
Publication of FR2433110B3 publication Critical patent/FR2433110B3/fr
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/075Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
FR7919271A 1978-08-09 1979-07-26 Diviseur de flux reglable pour turbomachines, notamment pour moteurs a reaction a turbines a gaz Granted FR2433110A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19782834860 DE2834860A1 (de) 1978-08-09 1978-08-09 Verstellbarer stroemungsteiler fuer stroemungsmaschinen, insbesondere gasturbinenstrahltriebwerke

Publications (2)

Publication Number Publication Date
FR2433110A1 FR2433110A1 (fr) 1980-03-07
FR2433110B3 true FR2433110B3 (fr) 1981-04-17

Family

ID=6046580

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7919271A Granted FR2433110A1 (fr) 1978-08-09 1979-07-26 Diviseur de flux reglable pour turbomachines, notamment pour moteurs a reaction a turbines a gaz

Country Status (4)

Country Link
US (1) US4261686A (fr)
DE (1) DE2834860A1 (fr)
FR (1) FR2433110A1 (fr)
GB (1) GB2027813B (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4461145A (en) * 1982-10-08 1984-07-24 The United States Of America As Represented By The Secretary Of The Air Force Stall elimination and restart enhancement device
DE3542762A1 (de) * 1985-12-04 1987-06-11 Mtu Muenchen Gmbh Einrichtung zur steuerung oder regelung von gasturbinentriebwerken bzw. gasturbinenstrahltriebwerken
US5307624A (en) * 1990-04-04 1994-05-03 General Electric Company Variable area bypass valve assembly
US5113649A (en) * 1990-05-11 1992-05-19 General Electric Company Passive bypass valve assembly
US5184461A (en) * 1990-05-11 1993-02-09 General Electric Company Method and apparatus for automatic bypass operation
US5054286A (en) * 1990-06-29 1991-10-08 General Electric Company Bypass valve system
CA2036821A1 (fr) * 1990-06-29 1991-12-30 Larry W. Stransky Systeme de vanne de derivation
US5048286A (en) * 1990-06-29 1991-09-17 General Electric Company Bypass valve door
FR2692938B1 (fr) * 1992-06-24 1994-09-02 Snecma Réacteur combiné et muni de moyens de commutation entre deux états de fonctionnement.
US6048171A (en) * 1997-09-09 2000-04-11 United Technologies Corporation Bleed valve system
US8622687B2 (en) * 2009-09-25 2014-01-07 General Electric Company Method of operating adaptive core engines
FR3029171B1 (fr) * 2014-11-27 2016-12-30 Airbus Operations Sas Turbomachine d'aeronef presentant une entree d'air a section variable
RU2729558C1 (ru) * 2019-09-16 2020-08-07 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Промежуточный корпус компрессора двухконтурного турбореактивного двигателя
FR3126733A1 (fr) * 2021-09-06 2023-03-10 Safran Aircraft Engines Turbomachine a double flux a bec variable en position

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3224194A (en) * 1963-06-26 1965-12-21 Curtiss Wright Corp Gas turbine engine
DE1936800C3 (de) * 1969-07-19 1975-08-07 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Hinsichtlich ihres Austrittsquerschnitts änderbare konvergente Schubdüse für ein Gasturbinenstrahltriebwerk
DE2218874C3 (de) * 1972-04-19 1979-05-17 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Vorrichtung zur Verstellung der Gebläseschaufeln eines Turbinenstrahltriebwerks
US3988889A (en) * 1974-02-25 1976-11-02 General Electric Company Cowling arrangement for a turbofan engine

Also Published As

Publication number Publication date
FR2433110A1 (fr) 1980-03-07
GB2027813B (en) 1982-09-02
GB2027813A (en) 1980-02-27
DE2834860A1 (de) 1980-03-13
US4261686A (en) 1981-04-14

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Legal Events

Date Code Title Description
ST Notification of lapse