FR2156883A1 - - Google Patents

Info

Publication number
FR2156883A1
FR2156883A1 FR7237284A FR7237284A FR2156883A1 FR 2156883 A1 FR2156883 A1 FR 2156883A1 FR 7237284 A FR7237284 A FR 7237284A FR 7237284 A FR7237284 A FR 7237284A FR 2156883 A1 FR2156883 A1 FR 2156883A1
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.)
Granted
Application number
FR7237284A
Other languages
French (fr)
Other versions
FR2156883B1 (en:Method
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
Publication of FR2156883A1 publication Critical patent/FR2156883A1/fr
Application granted granted Critical
Publication of FR2156883B1 publication Critical patent/FR2156883B1/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants 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
    • F02K3/04—Plants 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
    • F02K3/075—Plants 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants 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
    • F02K3/025—Plants 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 by-pass flow being at least partly used to create an independent thrust component

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
FR7237284A 1971-10-20 1972-10-20 Expired FR2156883B1 (en:Method)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2152207 1971-10-20

Publications (2)

Publication Number Publication Date
FR2156883A1 true FR2156883A1 (en:Method) 1973-06-01
FR2156883B1 FR2156883B1 (en:Method) 1976-06-04

Family

ID=5822871

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7237284A Expired FR2156883B1 (en:Method) 1971-10-20 1972-10-20

Country Status (3)

Country Link
US (1) US3810360A (en:Method)
FR (1) FR2156883B1 (en:Method)
GB (1) GB1407428A (en:Method)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4039028A1 (de) * 1989-12-08 1991-06-13 Westland Helicopters Verbundhubschrauber
FR3055357A1 (fr) * 2016-08-30 2018-03-02 Guillaume Pelcot Turbomachine a deux turbines motrices libres de travail et independantes l'une de l'autre ainsi que son dispositif unique de permutation entre ses deux modes de fonctionnement reversibles

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1545365A (en) * 1977-02-24 1979-05-10 Rolls Royce Gas turbine engines
US4592508A (en) * 1983-10-27 1986-06-03 The Boeing Company Translating jet engine nozzle plug
US4598543A (en) * 1985-02-06 1986-07-08 The United States Of America As Represented By The Secretary Of The Air Force Variable cycle engine for high altitude aircraft
DE4025567A1 (de) * 1990-08-11 1992-02-13 Daimler Benz Ag Gasturbine mit einem bypass im nutzleistungsturbinenteil
FR2826054B1 (fr) * 2001-06-14 2003-12-19 Snecma Moteurs Dispositif de propulsion a cycle variable par derivation de gaz pour avion supersonique et procede de fonctionnement
US6837038B2 (en) * 2001-10-16 2005-01-04 United Technologies Corporation Variable cycle boost propulsor
US8061119B2 (en) * 2007-11-29 2011-11-22 United Technologies Corporation Actuation mechanism for a convertible gas turbine propulsion system
US20100170221A1 (en) * 2009-01-08 2010-07-08 Toyota Jidosha Kabushiki Kaisha Turbo fan engine
PH12013501135A1 (en) * 2010-12-10 2013-07-08 Corporation Mc2 Rech Internationales Turbine assembly, and kit with components for assembling the same
GB2490915B (en) * 2011-05-18 2013-04-03 Rolls Royce Plc Vertical lift fan

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2458600A (en) * 1942-01-26 1949-01-11 Rateau Soc Aerodynamic propelling means operating through direct reaction jet and scavenging

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2587649A (en) * 1946-10-18 1952-03-04 Pope Francis Selective turbopropeller jet power plant for aircraft
US2507657A (en) * 1948-07-21 1950-05-16 Wiessler Gaston Antoin Auguste Aircraft with mixed type propulsion and sustaining means
DE1168168B (de) * 1962-08-18 1964-04-16 Daimler Benz Ag Zweikreis-Gasturbinenstrahltriebwerk
FR1472962A (fr) * 1964-08-08 1967-03-17 Dornier Werke Gmbh équipement moteur pour avions
GB1099971A (en) * 1966-01-11 1968-01-17 Bristol Siddeley Engines Ltd Power plants of the gas turbine type for helicopter aircraft
US3678690A (en) * 1970-07-10 1972-07-25 United Aircraft Corp Convertible composite engine

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2458600A (en) * 1942-01-26 1949-01-11 Rateau Soc Aerodynamic propelling means operating through direct reaction jet and scavenging

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4039028A1 (de) * 1989-12-08 1991-06-13 Westland Helicopters Verbundhubschrauber
FR3055357A1 (fr) * 2016-08-30 2018-03-02 Guillaume Pelcot Turbomachine a deux turbines motrices libres de travail et independantes l'une de l'autre ainsi que son dispositif unique de permutation entre ses deux modes de fonctionnement reversibles

Also Published As

Publication number Publication date
GB1407428A (en) 1975-09-24
US3810360A (en) 1974-05-14
FR2156883B1 (en:Method) 1976-06-04

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Legal Events

Date Code Title Description
ST Notification of lapse