FR2506840B1 - - Google Patents

Info

Publication number
FR2506840B1
FR2506840B1 FR8110725A FR8110725A FR2506840B1 FR 2506840 B1 FR2506840 B1 FR 2506840B1 FR 8110725 A FR8110725 A FR 8110725A FR 8110725 A FR8110725 A FR 8110725A FR 2506840 B1 FR2506840 B1 FR 2506840B1
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
FR8110725A
Other versions
FR2506840A1 (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.)
Office National dEtudes et de Recherches Aerospatiales ONERA
Original Assignee
Office National dEtudes et de Recherches Aerospatiales ONERA
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 Office National dEtudes et de Recherches Aerospatiales ONERA filed Critical Office National dEtudes et de Recherches Aerospatiales ONERA
Priority to FR8110725A priority Critical patent/FR2506840A1/fr
Priority to GB8214903A priority patent/GB2099518B/en
Priority to US06/381,023 priority patent/US4463553A/en
Priority to DE3219615A priority patent/DE3219615C2/de
Publication of FR2506840A1 publication Critical patent/FR2506840A1/fr
Application granted granted Critical
Publication of FR2506840B1 publication Critical patent/FR2506840B1/fr
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/24—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like
    • F01D1/26—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like traversed by the working-fluid substantially axially
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • F04D19/02—Multi-stage pumps
    • F04D19/024—Multi-stage pumps with contrarotating parts

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR8110725A 1981-05-29 1981-05-29 Turboreacteur a roues contra-rotatives Granted FR2506840A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR8110725A FR2506840A1 (fr) 1981-05-29 1981-05-29 Turboreacteur a roues contra-rotatives
GB8214903A GB2099518B (en) 1981-05-29 1982-05-21 Turbojet with contrarotating wheels
US06/381,023 US4463553A (en) 1981-05-29 1982-05-24 Turbojet with contrarotating wheels
DE3219615A DE3219615C2 (de) 1981-05-29 1982-05-25 Gasturbinenstrahltriebwerk mit gegenläufigen Laufschaufelgittern

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8110725A FR2506840A1 (fr) 1981-05-29 1981-05-29 Turboreacteur a roues contra-rotatives

Publications (2)

Publication Number Publication Date
FR2506840A1 FR2506840A1 (fr) 1982-12-03
FR2506840B1 true FR2506840B1 (fr) 1983-10-21

Family

ID=9259018

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8110725A Granted FR2506840A1 (fr) 1981-05-29 1981-05-29 Turboreacteur a roues contra-rotatives

Country Status (4)

Country Link
US (1) US4463553A (fr)
DE (1) DE3219615C2 (fr)
FR (1) FR2506840A1 (fr)
GB (1) GB2099518B (fr)

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US4728255A (en) * 1985-02-25 1988-03-01 General Electric Company Removable stiffening disk
US4790133A (en) * 1986-08-29 1988-12-13 General Electric Company High bypass ratio counterrotating turbofan engine
US4860537A (en) * 1986-08-29 1989-08-29 Brandt, Inc. High bypass ratio counterrotating gearless front fan engine
GB2207191B (en) * 1987-07-06 1992-03-04 Gen Electric Gas turbine engine
GB2232720B (en) * 1989-06-15 1993-11-10 Rolls Royce Business Ventures Gas turbine engine power unit
JP2604636B2 (ja) * 1990-01-22 1997-04-30 浩保 谷川 オール動翼蒸気タービン
US5077968A (en) * 1990-04-06 1992-01-07 United Technologies Corporation Vaneless contrarotating turbine
EP1812688B1 (fr) 2004-11-12 2016-04-13 Board of Trustees of Michigan State University Rotor tisse de turbomachine
EP1825113B1 (fr) * 2004-12-01 2012-10-24 United Technologies Corporation Boîte de vitesses contre-rotative pour moteur à turbine en bout
US7882695B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Turbine blow down starter for turbine engine
WO2006110123A2 (fr) * 2004-12-01 2006-10-19 United Technologies Corporation Conduit de transition pour moteur a turbine
WO2006110122A2 (fr) 2004-12-01 2006-10-19 United Technologies Corporation Purgeur gonflable destine a un moteur a turbine
US7959532B2 (en) 2004-12-01 2011-06-14 United Technologies Corporation Hydraulic seal for a gearbox of a tip turbine engine
WO2006060014A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Systeme de generateur-demarreur pour moteur de turbine a pression d’entree
WO2006059990A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Refroidissement regeneratif des aubes et pales de turbine pour moteur a turbine d'extremite
EP1828547B1 (fr) 2004-12-01 2011-11-30 United Technologies Corporation Turbosoufflante comprenant une pluralité d'aubes directrices d'entrée commandées individuellement et procédé de commande associé
US7874802B2 (en) 2004-12-01 2011-01-25 United Technologies Corporation Tip turbine engine comprising turbine blade clusters and method of assembly
US7631480B2 (en) 2004-12-01 2009-12-15 United Technologies Corporation Modular tip turbine engine
US8152469B2 (en) 2004-12-01 2012-04-10 United Technologies Corporation Annular turbine ring rotor
US8096753B2 (en) 2004-12-01 2012-01-17 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
WO2006059971A2 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Logement de moteur a turbine integrant un ventilateur, un combustor, et une turbine
US7882694B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Variable fan inlet guide vane assembly for gas turbine engine
WO2006059985A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Compresseur axial pour moteur a turbine de bout
WO2006060010A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Pale de guidage d’entree de compresseur pour moteur de turbine a pression d’entree et procede de commande correspondant
WO2006059973A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Moteur de turbine a aube comprenant un echangeur thermique
WO2006059989A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Structure de support de moteur a turbine de bout
WO2006060011A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Moteur a turbine de pointe comprenant un compartiment non rotatif
US7921636B2 (en) * 2004-12-01 2011-04-12 United Technologies Corporation Tip turbine engine and corresponding operating method
US8807936B2 (en) 2004-12-01 2014-08-19 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
WO2006060003A2 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Pale de ventilateur comprenant une section de diffuseur integrale et une section de pale de turbine a aube destine a une moteur a turbine a aube
DE602004031986D1 (de) 2004-12-01 2011-05-05 United Technologies Corp Gebläse-turbinen-rotoranordnung für einen spitzenturbinenmotor
WO2006059970A2 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Moteur a turbine equipe d'un ventilateur et d'un compresseur entraines par un engrenage differentiel
DE602004028528D1 (de) * 2004-12-01 2010-09-16 United Technologies Corp Tip-Turbinentriebwerk mit mehreren Gebläse- und Turbinenstufen
US7883315B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
WO2006060006A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Cone arriere non metallique de moteur a turbine de bout
WO2006059994A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Ensemble de joint pour rotor de turbine-ventilateur de moteur de turbine a pression d’entree
EP1825170B1 (fr) 2004-12-01 2009-03-18 United Technologies Corporation Systeme de lubrification de boite de vitesses pour moteur a turbine d'extremite
US7959406B2 (en) 2004-12-01 2011-06-14 United Technologies Corporation Close coupled gearbox assembly for a tip turbine engine
US8061968B2 (en) 2004-12-01 2011-11-22 United Technologies Corporation Counter-rotating compressor case and assembly method for tip turbine engine
WO2006059972A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Commande à distance d'étage variable de compresseur pour moteur à turbine
WO2006059979A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Carter intégral, aube fixe, bâti et mélangeur d'un moteur à turbine en bout
US9003759B2 (en) 2004-12-01 2015-04-14 United Technologies Corporation Particle separator for tip turbine engine
DE602004023769D1 (de) * 2004-12-01 2009-12-03 United Technologies Corp Gestapelte ringförmige bauteile für turbinenmotoren
US8468795B2 (en) 2004-12-01 2013-06-25 United Technologies Corporation Diffuser aspiration for a tip turbine engine
US7921635B2 (en) * 2004-12-01 2011-04-12 United Technologies Corporation Peripheral combustor for tip turbine engine
EP1834076B1 (fr) 2004-12-01 2011-04-06 United Technologies Corporation Groupe d'aubes de turbine d'un rotor de soufflante et procédé de montage d'un tel groupe
US7980054B2 (en) * 2004-12-01 2011-07-19 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
EP1825112B1 (fr) 2004-12-01 2013-10-23 United Technologies Corporation Moteur a turbine de bout en porte-a-faux
US8024931B2 (en) 2004-12-01 2011-09-27 United Technologies Corporation Combustor for turbine engine
WO2006062497A1 (fr) 2004-12-04 2006-06-15 United Technologies Corporation Bâti moteur à turbine en bout de pale
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
US8485783B2 (en) * 2007-12-20 2013-07-16 Volvo Aero Corporation Gas turbine engine
GB0802309D0 (en) * 2008-02-08 2008-03-12 Hawkhill Inc Llc 1 Gas compressor
US20140174056A1 (en) 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8128021B2 (en) 2008-06-02 2012-03-06 United Technologies Corporation Engine mount system for a turbofan gas turbine engine
US9103345B2 (en) 2009-12-16 2015-08-11 General Electric Company Supersonic compressor rotor
FR2970746B1 (fr) * 2011-01-20 2015-12-04 Snecma Turbomachine a turbines haute pression et basse pression imbriquees
US9239012B2 (en) 2011-06-08 2016-01-19 United Technologies Corporation Flexible support structure for a geared architecture gas turbine engine
US9631558B2 (en) 2012-01-03 2017-04-25 United Technologies Corporation Geared architecture for high speed and small volume fan drive turbine
US20150345426A1 (en) 2012-01-31 2015-12-03 United Technologies Corporation Geared turbofan gas turbine engine architecture
US9222417B2 (en) 2012-01-31 2015-12-29 United Technologies Corporation Geared turbofan gas turbine engine architecture
US10287914B2 (en) 2012-01-31 2019-05-14 United Technologies Corporation Gas turbine engine with high speed low pressure turbine section and bearing support features
US8887487B2 (en) 2012-01-31 2014-11-18 United Technologies Corporation Geared turbofan gas turbine engine architecture
US8935913B2 (en) 2012-01-31 2015-01-20 United Technologies Corporation Geared turbofan gas turbine engine architecture
US9534608B2 (en) 2012-02-17 2017-01-03 Embry-Riddle Aeronautical University, Inc. Multi-stage axial compressor with counter-rotation
US9353754B2 (en) 2012-03-13 2016-05-31 Embry-Riddle Aeronautical University, Inc. Multi-stage axial compressor with counter-rotation using accessory drive
US10125693B2 (en) 2012-04-02 2018-11-13 United Technologies Corporation Geared turbofan engine with power density range
DE102012008710A1 (de) 2012-04-25 2013-11-14 Harald von Hacht Gegenläufige Energiewandler
US8756908B2 (en) 2012-05-31 2014-06-24 United Technologies Corporation Fundamental gear system architecture
US20150308351A1 (en) 2012-05-31 2015-10-29 United Technologies Corporation Fundamental gear system architecture
US8572943B1 (en) 2012-05-31 2013-11-05 United Technologies Corporation Fundamental gear system architecture
US10724479B2 (en) 2013-03-15 2020-07-28 United Technologies Corporation Thrust efficient turbofan engine
US9624827B2 (en) 2013-03-15 2017-04-18 United Technologies Corporation Thrust efficient turbofan engine
US9528706B2 (en) * 2013-12-13 2016-12-27 Siemens Energy, Inc. Swirling midframe flow for gas turbine engine having advanced transitions
US20160195010A1 (en) * 2014-07-15 2016-07-07 United Technologies Corporation Vaneless counterrotating turbine
BE1024024B1 (fr) * 2014-10-09 2017-10-30 Safran Aero Boosters S.A. Compresseur de turbomachine axiale avec rotor contrarotatif
US10711629B2 (en) * 2017-09-20 2020-07-14 Generl Electric Company Method of clearance control for an interdigitated turbine engine

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Publication number Priority date Publication date Assignee Title
FR455782A (fr) * 1912-03-26 1913-08-08 Thomas Gill Perfectionnements aux turbines motrices et aux turbines employées comme pompes ou comme compresseurs
DE459613C (de) * 1923-04-16 1929-02-22 Kreuzversand Klotz G M B H Vorrichtung zum Gebrauch fuer elektrische Lichtbaeder mit einem Parabolspiegel
CH294449A (de) * 1941-09-08 1953-11-15 Daimler Benz Ag Trommelförmiger Läufer.
US2472878A (en) * 1942-04-29 1949-06-14 Vickers Electrical Co Ltd Fluid turbine power plant with speed reduction transmission gearing
FR978412A (fr) * 1946-12-03 1951-04-13 Groupe turbo-compresseur à éléments tournant en sens opposés
US2639583A (en) * 1947-06-25 1953-05-26 Harry C Steele Contrarotating gas turbine having a power turbine and a plurality of compressor-turbines in series
DE938942C (de) * 1951-12-06 1956-02-09 Karl Dr-Ing Roeder Gasturbosatz
FR1514932A (fr) * 1965-06-24 1968-03-01 Snecma Compresseur axial à double rotor contrarotatif
FR1455272A (fr) * 1965-08-04 1966-04-01 Snecma Perfectionnement aux compresseurs axiaux à double rotor contrarotatif
FR1455278A (fr) * 1965-08-05 1966-04-01 Snecma Turboréacteur à double flux
FR1472085A (fr) * 1965-11-18 1967-03-10 Snecma Perfectionnement aux compresseurs contra-rotatifs
FR1561980A (fr) * 1967-12-14 1969-04-04
US3673802A (en) * 1970-06-18 1972-07-04 Gen Electric Fan engine with counter rotating geared core booster
US3861139A (en) * 1973-02-12 1975-01-21 Gen Electric Turbofan engine having counterrotating compressor and turbine elements and unique fan disposition

Also Published As

Publication number Publication date
DE3219615A1 (de) 1982-12-16
GB2099518B (en) 1984-09-26
US4463553A (en) 1984-08-07
DE3219615C2 (de) 1983-12-29
FR2506840A1 (fr) 1982-12-03
GB2099518A (en) 1982-12-08

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Legal Events

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ST Notification of lapse