DE3014279A1
(de)
*
|
1980-04-15 |
1981-10-22 |
M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 4200 Oberhausen |
Einrichtung zur kuehlung des inneren einer gasturbine
|
GB2075123B
(en)
*
|
1980-05-01 |
1983-11-16 |
Gen Electric |
Turbine cooling air deswirler
|
US4416111A
(en)
*
|
1981-02-25 |
1983-11-22 |
The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration |
Air modulation apparatus
|
US4456427A
(en)
*
|
1981-06-11 |
1984-06-26 |
General Electric Company |
Cooling air injector for turbine blades
|
US4435123A
(en)
*
|
1982-04-19 |
1984-03-06 |
United Technologies Corporation |
Cooling system for turbines
|
GB2118629B
(en)
*
|
1982-04-21 |
1985-07-17 |
Rolls Royce |
Device for passing a fluid flow eg. cooling air through a barrier eg. bolted joint
|
FR2552164B1
(fr)
*
|
1983-09-21 |
1986-12-26 |
Snecma |
Disque de compresseur avec accelerateur centripete integre pour l'aspiration d'air dans un dispositif de refroidissement d'une turbine a gaz
|
US4536129A
(en)
*
|
1984-06-15 |
1985-08-20 |
United Technologies Corporation |
Turbine blade with disk rim shield
|
US4708588A
(en)
*
|
1984-12-14 |
1987-11-24 |
United Technologies Corporation |
Turbine cooling air supply system
|
US4674955A
(en)
*
|
1984-12-21 |
1987-06-23 |
The Garrett Corporation |
Radial inboard preswirl system
|
US4882902A
(en)
*
|
1986-04-30 |
1989-11-28 |
General Electric Company |
Turbine cooling air transferring apparatus
|
US4666368A
(en)
*
|
1986-05-01 |
1987-05-19 |
General Electric Company |
Swirl nozzle for a cooling system in gas turbine engines
|
US4759688A
(en)
*
|
1986-12-16 |
1988-07-26 |
Allied-Signal Inc. |
Cooling flow side entry for cooled turbine blading
|
FR2661946B1
(fr)
*
|
1990-05-14 |
1994-06-10 |
Alsthom Gec |
Etage de turbine a action avec pertes secondaires reduites.
|
US5134844A
(en)
*
|
1990-07-30 |
1992-08-04 |
General Electric Company |
Aft entry cooling system and method for an aircraft engine
|
US5135354A
(en)
*
|
1990-09-14 |
1992-08-04 |
United Technologies Corporation |
Gas turbine blade and disk
|
US5245821A
(en)
*
|
1991-10-21 |
1993-09-21 |
General Electric Company |
Stator to rotor flow inducer
|
US5281097A
(en)
*
|
1992-11-20 |
1994-01-25 |
General Electric Company |
Thermal control damper for turbine rotors
|
GB2319308B
(en)
*
|
1996-11-12 |
2001-02-28 |
Rolls Royce Plc |
Gas turbine engine turbine system
|
DE19705441A1
(de)
*
|
1997-02-13 |
1998-08-20 |
Bmw Rolls Royce Gmbh |
Turbinen-Laufradscheibe
|
JP3337393B2
(ja)
*
|
1997-04-23 |
2002-10-21 |
三菱重工業株式会社 |
ガスタービン冷却動翼
|
FR2823794B1
(fr)
*
|
2001-04-19 |
2003-07-11 |
Snecma Moteurs |
Aube rapportee et refroidie pour turbine
|
US6735956B2
(en)
|
2001-10-26 |
2004-05-18 |
Pratt & Whitney Canada Corp. |
High pressure turbine blade cooling scoop
|
EP1380723A1
(fr)
*
|
2002-07-09 |
2004-01-14 |
Siemens Aktiengesellschaft |
Procédé de refroidissement d'aubes de turbine, dispositif induisant une prérotation de fluide, ainsi que turbine comprenant ledit dispositif
|
GB0227745D0
(en)
*
|
2002-11-28 |
2003-01-08 |
Rolls Royce Plc |
Blade cooling
|
US8128365B2
(en)
|
2007-07-09 |
2012-03-06 |
Siemens Energy, Inc. |
Turbine airfoil cooling system with rotor impingement cooling
|
CH699999A1
(de)
|
2008-11-26 |
2010-05-31 |
Alstom Technology Ltd |
Gekühlte schaufel für eine gasturbine.
|
GB2467790B
(en)
*
|
2009-02-16 |
2011-06-01 |
Rolls Royce Plc |
Vane
|
US8381533B2
(en)
*
|
2009-04-30 |
2013-02-26 |
Honeywell International Inc. |
Direct transfer axial tangential onboard injector system (TOBI) with self-supporting seal plate
|
WO2012052740A1
(fr)
*
|
2010-10-18 |
2012-04-26 |
University Of Durham |
Dispositif d'étanchéité pour réduire la fuite de fluide dans une turbine
|
US9133855B2
(en)
*
|
2010-11-15 |
2015-09-15 |
Mtu Aero Engines Gmbh |
Rotor for a turbo machine
|
US9080449B2
(en)
*
|
2011-08-16 |
2015-07-14 |
United Technologies Corporation |
Gas turbine engine seal assembly having flow-through tube
|
US20130170983A1
(en)
*
|
2012-01-04 |
2013-07-04 |
General Electric Company |
Turbine assembly and method for reducing fluid flow between turbine components
|
US9435206B2
(en)
*
|
2012-09-11 |
2016-09-06 |
General Electric Company |
Flow inducer for a gas turbine system
|
US9169729B2
(en)
*
|
2012-09-26 |
2015-10-27 |
Solar Turbines Incorporated |
Gas turbine engine turbine diaphragm with angled holes
|
EP2713009B1
(fr)
|
2012-09-26 |
2015-03-11 |
Alstom Technology Ltd |
Procédé et système de refroidissement pour refroidir des aubes d'au moins une rangée d'aubes dans une turbomachine rotative
|
US9175566B2
(en)
*
|
2012-09-26 |
2015-11-03 |
Solar Turbines Incorporated |
Gas turbine engine preswirler with angled holes
|
EP2725191B1
(fr)
*
|
2012-10-23 |
2016-03-16 |
Alstom Technology Ltd |
Turbine à gaz et aube de turbine pour une telle turbine à gaz
|
US9416674B1
(en)
*
|
2013-05-02 |
2016-08-16 |
S&J Design Llc |
Floating air riding seal for a turbine
|
US9777634B2
(en)
*
|
2013-09-12 |
2017-10-03 |
United Technologies Corporation |
Tube fed tangential on-board injector for gas turbine engine
|
GB201507390D0
(en)
|
2015-04-30 |
2015-06-17 |
Rolls Royce Plc |
Transfer couplings
|
DE102015111746A1
(de)
*
|
2015-07-20 |
2017-01-26 |
Rolls-Royce Deutschland Ltd & Co Kg |
Gekühltes Turbinenlaufrad, insbesondere für ein Flugtriebwerk
|
DE102015111750A1
(de)
|
2015-07-20 |
2017-01-26 |
Rolls-Royce Deutschland Ltd & Co Kg |
Gekühltes Turbinenlaufrad für ein Flugtriebwerk
|
JP6647952B2
(ja)
*
|
2016-04-25 |
2020-02-14 |
三菱重工業株式会社 |
ガスタービン
|
US10787920B2
(en)
|
2016-10-12 |
2020-09-29 |
General Electric Company |
Turbine engine inducer assembly
|
US11002138B2
(en)
|
2017-12-13 |
2021-05-11 |
Solar Turbines Incorporated |
Turbine blade cooling system with lower turning vane bank
|