US2668413A
(en)
*
|
1948-03-15 |
1954-02-09 |
James V Giliberty |
Gas turbine power plant with duplexed blading
|
US2721445A
(en)
*
|
1949-12-22 |
1955-10-25 |
James V Giliberty |
Aircraft propulsion plant of the propeller-jet turbine type
|
US2672726A
(en)
*
|
1950-09-19 |
1954-03-23 |
Bell Aircraft Corp |
Ducted fan jet aircraft engine
|
US2835332A
(en)
*
|
1955-10-20 |
1958-05-20 |
Vern K Fry |
Power drive suitable for airplanes and helicopters
|
US2914918A
(en)
*
|
1955-12-28 |
1959-12-01 |
Poly Ind Inc |
Gas turbine jet engine starter with serially-connected concentrically-arranged combustion chambers
|
US2937495A
(en)
*
|
1956-02-27 |
1960-05-24 |
Power Jets Res & Dev Ltd |
Gas turbine plant
|
DE1085718B
(de)
*
|
1958-11-26 |
1960-07-21 |
Daimler Benz Ag |
Gasturbinentriebwerk
|
US3818695A
(en)
*
|
1971-08-02 |
1974-06-25 |
Rylewski Eugeniusz |
Gas turbine
|
US3861139A
(en)
*
|
1973-02-12 |
1975-01-21 |
Gen Electric |
Turbofan engine having counterrotating compressor and turbine elements and unique fan disposition
|
WO1998000628A1
(fr)
*
|
1996-06-28 |
1998-01-08 |
Hiroyasu Tanigawa |
Turbine a vapeur et a gaz combinees
|
US6397577B1
(en)
*
|
2001-04-02 |
2002-06-04 |
The United States Of America As Represented By The Secretary Of The Air Force |
Shaftless gas turbine engine spool
|
US7927075B2
(en)
*
|
2004-12-01 |
2011-04-19 |
United Technologies Corporation |
Fan-turbine rotor assembly for a tip turbine engine
|
EP1828573B1
(fr)
*
|
2004-12-01 |
2010-06-16 |
United Technologies Corporation |
Joint hydraulique pour boite de vitesses de moteur a turbine d'extremite
|
WO2006060004A1
(fr)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Dispositif de combustion pour moteur de turbine
|
US9003759B2
(en)
|
2004-12-01 |
2015-04-14 |
United Technologies Corporation |
Particle separator for tip turbine engine
|
US8757959B2
(en)
*
|
2004-12-01 |
2014-06-24 |
United Technologies Corporation |
Tip turbine engine comprising a nonrotable compartment
|
US8087885B2
(en)
*
|
2004-12-01 |
2012-01-03 |
United Technologies Corporation |
Stacked annular components for turbine engines
|
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
|
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
|
EP1825113B1
(fr)
|
2004-12-01 |
2012-10-24 |
United Technologies Corporation |
Boîte de vitesses contre-rotative pour moteur à turbine en bout
|
US20090148273A1
(en)
*
|
2004-12-01 |
2009-06-11 |
Suciu Gabriel L |
Compressor inlet guide vane for tip turbine engine and corresponding control method
|
EP1834067B1
(fr)
*
|
2004-12-01 |
2008-11-26 |
United Technologies Corporation |
Ensemble de pales de soufflante pour moteur a turbine de bout et procede de montage
|
WO2006059974A1
(fr)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Ensemble de boite de vitesses a couplage proximal pour moteur de turbine a pression d'entree
|
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
|
US8083030B2
(en)
*
|
2004-12-01 |
2011-12-27 |
United Technologies Corporation |
Gearbox lubrication supply system for a tip engine
|
WO2006060005A1
(fr)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Ensemble de rotor de turbine-ventilateur avec section d’induction integrale pour moteur de turbine a pression d’entree
|
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
|
WO2006059992A1
(fr)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Inducteur de pale de ventilateur de moteur de turbine a pression d’entree
|
US8104257B2
(en)
*
|
2004-12-01 |
2012-01-31 |
United Technologies Corporation |
Tip turbine engine with multiple fan and turbine stages
|
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
|
DE602004028297D1
(de)
*
|
2004-12-01 |
2010-09-02 |
United Technologies Corp |
Umfangsbrennkammer für spitzenturbinenmotor
|
EP1825112B1
(fr)
*
|
2004-12-01 |
2013-10-23 |
United Technologies Corporation |
Moteur a turbine de bout en porte-a-faux
|
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
|
DE602004032186D1
(de)
*
|
2004-12-01 |
2011-05-19 |
United Technologies Corp |
Turbinenschaufelgruppe eines Fanrotors sowie Verfahren zur Montage einer solchen Gruppe
|
US8365511B2
(en)
*
|
2004-12-01 |
2013-02-05 |
United Technologies Corporation |
Tip turbine engine integral case, vane, mount and mixer
|
WO2006059989A1
(fr)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Structure de support de moteur a turbine de bout
|
US7883314B2
(en)
*
|
2004-12-01 |
2011-02-08 |
United Technologies Corporation |
Seal assembly for a fan-turbine rotor of a tip turbine engine
|
WO2006059973A1
(fr)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Moteur de turbine a aube comprenant un echangeur thermique
|
US8061968B2
(en)
*
|
2004-12-01 |
2011-11-22 |
United Technologies Corporation |
Counter-rotating compressor case and assembly method for tip turbine engine
|
WO2006059971A2
(fr)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Logement de moteur a turbine integrant un ventilateur, un combustor, et une turbine
|
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
|
DE602004019709D1
(de)
*
|
2004-12-01 |
2009-04-09 |
United Technologies Corp |
Tip-turbinentriebwerk und entsprechendes betriebsverfahren
|
WO2006059988A1
(fr)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Moteur a turbine de bout modulaire
|
WO2006059996A1
(fr)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Ailettes de rotor de soufflante pour moteur a turbine en bout
|
US7607286B2
(en)
*
|
2004-12-01 |
2009-10-27 |
United Technologies Corporation |
Regenerative turbine blade and vane cooling for a tip turbine engine
|
EP1828567B1
(fr)
|
2004-12-01 |
2011-10-12 |
United Technologies Corporation |
Aspiration par diffuseur pour moteur a turbine d'extremite
|
WO2006060013A1
(fr)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Ensemble de joint de rotor de ventilateur de moteur de turbine a pression d’entree
|
EP1831530B1
(fr)
*
|
2004-12-01 |
2009-02-25 |
United Technologies Corporation |
Commande à distance d'étage variable de compresseur pour moteur à turbine
|
DE602004016065D1
(de)
|
2004-12-01 |
2008-10-02 |
United Technologies Corp |
Variable gebläseeinlassleitschaufelanordnung, turbinenmotor mit solch einer anordnung und entsprechendes steuerverfahren
|
WO2006060006A1
(fr)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Cone arriere non metallique de moteur a turbine de bout
|
WO2006059997A2
(fr)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Elements annulaires de rotor de turbine
|
WO2006060014A1
(fr)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Systeme de generateur-demarreur pour moteur de turbine a pression d’entree
|
US7845157B2
(en)
|
2004-12-01 |
2010-12-07 |
United Technologies Corporation |
Axial compressor for tip turbine engine
|
WO2006062497A1
(fr)
*
|
2004-12-04 |
2006-06-15 |
United Technologies Corporation |
Bâti moteur à turbine en bout de pale
|
US8192141B1
(en)
*
|
2007-04-05 |
2012-06-05 |
The United States Of America As Represented By The Secretary Of The Air Force |
Dual compression rotor
|
US8967945B2
(en)
|
2007-05-22 |
2015-03-03 |
United Technologies Corporation |
Individual inlet guide vane control for tip turbine engine
|
US8176725B2
(en)
*
|
2009-09-09 |
2012-05-15 |
United Technologies Corporation |
Reversed-flow core for a turbofan with a fan drive gear system
|
US20110146289A1
(en)
*
|
2009-12-21 |
2011-06-23 |
John Lewis Baughman |
Power extraction method
|
US20110146228A1
(en)
*
|
2009-12-21 |
2011-06-23 |
John Lewis Baughman |
Power extraction system
|
US20120324901A1
(en)
*
|
2011-06-23 |
2012-12-27 |
United Technologies Corporation |
Tandem fan-turbine rotor for a tip turbine engine
|
US9879694B2
(en)
*
|
2015-02-03 |
2018-01-30 |
United Technologies Corporation |
Turbo-compressor with geared turbofan
|
US10337401B2
(en)
*
|
2015-02-13 |
2019-07-02 |
United Technologies Corporation |
Turbine engine with a turbo-compressor
|
US10100731B2
(en)
*
|
2015-02-13 |
2018-10-16 |
United Technologies Corporation |
Turbine engine with a turbo-compressor
|
US10125722B2
(en)
|
2015-02-13 |
2018-11-13 |
United Technologies Corporation |
Turbine engine with a turbo-compressor
|
US10041408B2
(en)
*
|
2015-02-13 |
2018-08-07 |
United Technologies Corporation |
Turbine engine with a turbo-compressor
|
US10378438B2
(en)
*
|
2016-04-20 |
2019-08-13 |
Rolls-Royce North American Technologies, Inc. |
Reverse flow gas turbine engine with radially outward turbine
|
US10883424B2
(en)
|
2016-07-19 |
2021-01-05 |
Pratt & Whitney Canada Corp. |
Multi-spool gas turbine engine architecture
|
US11415063B2
(en)
|
2016-09-15 |
2022-08-16 |
Pratt & Whitney Canada Corp. |
Reverse-flow gas turbine engine
|
US10465611B2
(en)
|
2016-09-15 |
2019-11-05 |
Pratt & Whitney Canada Corp. |
Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
|
US11035293B2
(en)
|
2016-09-15 |
2021-06-15 |
Pratt & Whitney Canada Corp. |
Reverse flow gas turbine engine with offset RGB
|
US10815899B2
(en)
|
2016-11-15 |
2020-10-27 |
Pratt & Whitney Canada Corp. |
Gas turbine engine accessories arrangement
|
US10539020B2
(en)
*
|
2017-01-23 |
2020-01-21 |
General Electric Company |
Two spool gas turbine engine with interdigitated turbine section
|
US10544734B2
(en)
*
|
2017-01-23 |
2020-01-28 |
General Electric Company |
Three spool gas turbine engine with interdigitated turbine section
|
US10655537B2
(en)
*
|
2017-01-23 |
2020-05-19 |
General Electric Company |
Interdigitated counter rotating turbine system and method of operation
|
US10808624B2
(en)
|
2017-02-09 |
2020-10-20 |
Pratt & Whitney Canada Corp. |
Turbine rotor with low over-speed requirements
|
US10738709B2
(en)
|
2017-02-09 |
2020-08-11 |
Pratt & Whitney Canada Corp. |
Multi-spool gas turbine engine
|
US10215052B2
(en)
|
2017-03-14 |
2019-02-26 |
Pratt & Whitney Canada Corp. |
Inter-shaft bearing arrangement
|
US10746188B2
(en)
|
2017-03-14 |
2020-08-18 |
Pratt & Whitney Canada Corp. |
Inter-shaft bearing connected to a compressor boost system
|
US10718265B2
(en)
|
2017-05-25 |
2020-07-21 |
General Electric Company |
Interdigitated turbine engine air bearing and method of operation
|
US10605168B2
(en)
|
2017-05-25 |
2020-03-31 |
General Electric Company |
Interdigitated turbine engine air bearing cooling structure and method of thermal management
|
US10787931B2
(en)
|
2017-05-25 |
2020-09-29 |
General Electric Company |
Method and structure of interdigitated turbine engine thermal management
|
US10669893B2
(en)
|
2017-05-25 |
2020-06-02 |
General Electric Company |
Air bearing and thermal management nozzle arrangement for interdigitated turbine engine
|
US10344763B2
(en)
*
|
2017-08-28 |
2019-07-09 |
Mustafa Rez |
Disc turbo charger
|
US20190063313A1
(en)
*
|
2017-08-28 |
2019-02-28 |
Mustafa Rez |
Disc Turbine Engine
|
CN110529250B
(zh)
*
|
2018-05-23 |
2022-08-02 |
通用电气公司 |
燃气涡轮发动机
|
US11434831B2
(en)
|
2018-05-23 |
2022-09-06 |
General Electric Company |
Gas turbine combustor having a plurality of angled vanes circumferentially spaced within the combustor
|
CA3051562A1
(fr)
|
2018-08-08 |
2020-02-08 |
Pratt & Whitney Canada Corp. |
Systeme et procede a moteurs multiples
|
US11255266B2
(en)
*
|
2019-05-14 |
2022-02-22 |
Raytheon Technologies Corporation |
Recuperated cycle engine
|
EP4107378A4
(fr)
*
|
2020-02-19 |
2024-03-13 |
Nathan Geoffrey Andrews |
Ensemble turbine-compresseur compact
|
US11428160B2
(en)
|
2020-12-31 |
2022-08-30 |
General Electric Company |
Gas turbine engine with interdigitated turbine and gear assembly
|