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FR1555756A - - Google Patents

Info

Publication number
FR1555756A
FR1555756A FR1555756DA FR1555756A FR 1555756 A FR1555756 A FR 1555756A FR 1555756D A FR1555756D A FR 1555756DA FR 1555756 A FR1555756 A FR 1555756A
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
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 filed Critical
Application granted granted Critical
Publication of FR1555756A publication Critical patent/FR1555756A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1555756D 1966-11-30 1967-11-30 Expired FR1555756A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB53715/66A GB1175376A (en) 1966-11-30 1966-11-30 Gas Turbine Power Plants.

Publications (1)

Publication Number Publication Date
FR1555756A true FR1555756A (fr) 1969-01-31

Family

ID=10468746

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1555756D Expired FR1555756A (fr) 1966-11-30 1967-11-30

Country Status (3)

Country Link
US (1) US3465526A (fr)
FR (1) FR1555756A (fr)
GB (1) GB1175376A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2941493A1 (fr) * 2009-01-23 2010-07-30 Snecma Turbomachine a turbine libre entrainant un generateur electrique de puissance
WO2017013360A1 (fr) 2015-07-22 2017-01-26 Safran Aircraft Engines Aeronef comportant une turbomachine integree au fuselage arriere a alimentation variable
FR3039213A1 (fr) * 2015-07-22 2017-01-27 Snecma Turbomachine comportant au moins deux generateurs de gaz et une distribution de flux variable dans la turbine de puissance

Families Citing this family (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3520138A (en) * 1969-02-27 1970-07-14 United Aircraft Corp Convertible enginf
US3678691A (en) * 1970-07-10 1972-07-25 United Aircraft Corp Convertible composite engine control
US3678690A (en) * 1970-07-10 1972-07-25 United Aircraft Corp Convertible composite engine
US4791783A (en) * 1981-11-27 1988-12-20 General Electric Company Convertible aircraft engine
EP1825112B1 (fr) 2004-12-01 2013-10-23 United Technologies Corporation Moteur a turbine de bout en porte-a-faux
EP1841960B1 (fr) 2004-12-01 2011-05-25 United Technologies Corporation Ailettes de rotor de soufflante pour moteur a turbine en bout
EP1828573B1 (fr) 2004-12-01 2010-06-16 United Technologies Corporation Joint hydraulique pour boite de vitesses de moteur a turbine d'extremite
EP1825177B1 (fr) 2004-12-01 2012-01-25 United Technologies Corporation Purgeur gonflable destine a un moteur a turbine et methode de reglage d'air de purge
US9003759B2 (en) 2004-12-01 2015-04-14 United Technologies Corporation Particle separator for tip turbine engine
US20090148273A1 (en) * 2004-12-01 2009-06-11 Suciu Gabriel L Compressor inlet guide vane for tip turbine engine and corresponding control method
WO2006059985A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Compresseur axial pour moteur a turbine de bout
US7937927B2 (en) 2004-12-01 2011-05-10 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
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
DE602004016059D1 (de) * 2004-12-01 2008-10-02 United Technologies Corp Tip-turbinentriebwerk mit wärmetauscher
EP1825170B1 (fr) 2004-12-01 2009-03-18 United Technologies Corporation Systeme de lubrification de boite de vitesses pour moteur a turbine d'extremite
US7976273B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Tip turbine engine support structure
WO2006059971A2 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Logement de moteur a turbine integrant un ventilateur, un combustor, et une turbine
DE602004028528D1 (de) * 2004-12-01 2010-09-16 United Technologies Corp Tip-Turbinentriebwerk mit mehreren Gebläse- und Turbinenstufen
US7883314B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan-turbine rotor of a 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
EP1828574B1 (fr) 2004-12-01 2010-11-03 United Technologies Corporation Ensemble de boite de vitesses a couplage proximal pour moteur de turbine a pression d'entree
WO2006059969A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Carter de compresseur à rotation inverse et procédé d'assemblage pour un moteur à turbine en bout
EP1831521B1 (fr) * 2004-12-01 2008-08-20 United Technologies Corporation Ensemble aubes de guidage d'admission de soufflante variable, turbomachine dotee d'un tel ensemble et procede de commande correspondant
EP2333286A1 (fr) 2004-12-01 2011-06-15 United Technologies Corporation Vectorisation de conduite de transition pour moteur de turbine
DE602004019709D1 (de) * 2004-12-01 2009-04-09 United Technologies Corp Tip-turbinentriebwerk und entsprechendes betriebsverfahren
EP1828545A2 (fr) 2004-12-01 2007-09-05 United Technologies Corporation Elements annulaires de rotor de turbine
US8024931B2 (en) 2004-12-01 2011-09-27 United Technologies Corporation Combustor for turbine engine
DE602004031679D1 (de) 2004-12-01 2011-04-14 United Technologies Corp Regenerative Kühlung einer Leit- und Laufschaufel für ein Tipturbinentriebwerk
WO2006059986A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Moteur a turbine de bout et procede de fonctionnement avec inversion de la circulation d'air du noyau du ventilateur
EP1825116A2 (fr) * 2004-12-01 2007-08-29 United Technologies Corporation Refroidissement par ejecteur de l'enveloppe exterieure d'un moteur a turbine de bout
WO2006059980A2 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Aspiration par diffuseur pour moteur a turbine d'extremite
WO2006060001A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Rotor de ventilateur pour moteur a turbine de bout
WO2006110125A2 (fr) * 2004-12-01 2006-10-19 United Technologies Corporation Elements annulaires empiles pour moteurs a turbine
WO2006060011A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Moteur a turbine de pointe comprenant un compartiment non rotatif
WO2006059988A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Moteur a turbine de bout modulaire
US7883315B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
US7921635B2 (en) * 2004-12-01 2011-04-12 United Technologies Corporation Peripheral combustor for tip turbine engine
US8807936B2 (en) 2004-12-01 2014-08-19 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
US8641367B2 (en) 2004-12-01 2014-02-04 United Technologies Corporation Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method
WO2006112807A2 (fr) 2004-12-01 2006-10-26 United Technologies Corporation Turbo-demarreur d'extraction pour moteur a turbine
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
US7874802B2 (en) 2004-12-01 2011-01-25 United Technologies Corporation Tip turbine engine comprising turbine blade clusters and method of assembly
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
WO2006059972A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Commande à distance d'étage variable de compresseur pour moteur à turbine
WO2006060006A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Cone arriere non metallique de moteur a turbine de bout
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
PH12013501135A1 (en) * 2010-12-10 2013-07-08 Corporation Mc2 Rech Internationales Turbine assembly, and kit with components for assembling the same

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB857037A (en) * 1958-09-27 1960-12-29 Rolls Royce Improved power unit
US3186165A (en) * 1961-11-29 1965-06-01 Gen Electric Turbofan engine speed synchronizing arrangement
US3146590A (en) * 1962-03-12 1964-09-01 Gen Electric Power system with energy dividing means
GB1024969A (en) * 1964-09-14 1966-04-06 Rolls Royce Helicopter power plant
GB1064609A (en) * 1965-10-18 1967-04-05 Rolls Royce Gas turbine power plant

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2941493A1 (fr) * 2009-01-23 2010-07-30 Snecma Turbomachine a turbine libre entrainant un generateur electrique de puissance
WO2017013360A1 (fr) 2015-07-22 2017-01-26 Safran Aircraft Engines Aeronef comportant une turbomachine integree au fuselage arriere a alimentation variable
FR3039213A1 (fr) * 2015-07-22 2017-01-27 Snecma Turbomachine comportant au moins deux generateurs de gaz et une distribution de flux variable dans la turbine de puissance
US10082040B2 (en) 2015-07-22 2018-09-25 Safran Aircraft Engines Aircraft comprising a turbine engine incorporated into the rear fuselage with variable supply

Also Published As

Publication number Publication date
GB1175376A (en) 1969-12-23
US3465526A (en) 1969-09-09

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Legal Events

Date Code Title Description
TP Transmission of property
TP Transmission of property
TP Transmission of property
ST Notification of lapse