FR2427469A1
(fr)
*
|
1978-06-01 |
1979-12-28 |
Snecma |
Dispositif de fixation d'une garniture d'etancheite sur un distributeur de turbomachine
|
US4222708A
(en)
*
|
1978-06-26 |
1980-09-16 |
General Electric Company |
Method and apparatus for reducing eccentricity in a turbomachine
|
GB2042646B
(en)
*
|
1979-02-20 |
1982-09-22 |
Rolls Royce |
Rotor blade tip clearance control for gas turbine engine
|
US4332523A
(en)
*
|
1979-05-25 |
1982-06-01 |
Teledyne Industries, Inc. |
Turbine shroud assembly
|
GB2050524B
(en)
*
|
1979-06-06 |
1982-10-20 |
Rolls Royce |
Turbine stator shroud assembly
|
US4329114A
(en)
*
|
1979-07-25 |
1982-05-11 |
The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration |
Active clearance control system for a turbomachine
|
US4487016A
(en)
*
|
1980-10-01 |
1984-12-11 |
United Technologies Corporation |
Modulated clearance control for an axial flow rotary machine
|
US5192186A
(en)
*
|
1980-10-03 |
1993-03-09 |
Rolls-Royce Plc |
Gas turbine engine
|
GB2117450B
(en)
*
|
1981-03-20 |
1984-06-27 |
Rolls Royce |
Casing support for a gas turbine engine
|
US4522559A
(en)
*
|
1982-02-19 |
1985-06-11 |
General Electric Company |
Compressor casing
|
GB2125111B
(en)
*
|
1982-03-23 |
1985-06-05 |
Rolls Royce |
Shroud assembly for a gas turbine engine
|
FR2540560B1
(fr)
*
|
1983-02-03 |
1987-06-12 |
Snecma |
Dispositif d'etancheite d'aubages mobiles de turbomachine
|
US4798047A
(en)
*
|
1983-12-19 |
1989-01-17 |
Elliott Turbomachinery Co., Inc. |
Particulate collection and cooling in a turbomachine
|
US4650394A
(en)
*
|
1984-11-13 |
1987-03-17 |
United Technologies Corporation |
Coolable seal assembly for a gas turbine engine
|
US4642024A
(en)
*
|
1984-12-05 |
1987-02-10 |
United Technologies Corporation |
Coolable stator assembly for a rotary machine
|
US4650395A
(en)
*
|
1984-12-21 |
1987-03-17 |
United Technologies Corporation |
Coolable seal segment for a rotary machine
|
FR2591674B1
(fr)
*
|
1985-12-18 |
1988-02-19 |
Snecma |
Dispositif de reglage des jeux radiaux entre rotor et stator d'un compresseur
|
FR2603340B1
(fr)
*
|
1986-09-03 |
1988-11-04 |
Snecma |
Turbomachine comportant un dispositif d'ajustement des jeux d'un joint a labyrinthe entre rotor et stator et de l'alignement de veine des gaz et methode d'application
|
US4767260A
(en)
*
|
1986-11-07 |
1988-08-30 |
United Technologies Corporation |
Stator vane platform cooling means
|
US4928240A
(en)
*
|
1988-02-24 |
1990-05-22 |
General Electric Company |
Active clearance control
|
US4826397A
(en)
*
|
1988-06-29 |
1989-05-02 |
United Technologies Corporation |
Stator assembly for a gas turbine engine
|
US4890978A
(en)
*
|
1988-10-19 |
1990-01-02 |
Westinghouse Electric Corp. |
Method and apparatus for vane segment support and alignment in combustion turbines
|
US5018942A
(en)
*
|
1989-09-08 |
1991-05-28 |
General Electric Company |
Mechanical blade tip clearance control apparatus for a gas turbine engine
|
US5056988A
(en)
*
|
1990-02-12 |
1991-10-15 |
General Electric Company |
Blade tip clearance control apparatus using shroud segment position modulation
|
US5049033A
(en)
*
|
1990-02-20 |
1991-09-17 |
General Electric Company |
Blade tip clearance control apparatus using cam-actuated shroud segment positioning mechanism
|
US5035573A
(en)
*
|
1990-03-21 |
1991-07-30 |
General Electric Company |
Blade tip clearance control apparatus with shroud segment position adjustment by unison ring movement
|
US5127794A
(en)
*
|
1990-09-12 |
1992-07-07 |
United Technologies Corporation |
Compressor case with controlled thermal environment
|
US5181826A
(en)
*
|
1990-11-23 |
1993-01-26 |
General Electric Company |
Attenuating shroud support
|
US5228828A
(en)
*
|
1991-02-15 |
1993-07-20 |
General Electric Company |
Gas turbine engine clearance control apparatus
|
US5167487A
(en)
*
|
1991-03-11 |
1992-12-01 |
General Electric Company |
Cooled shroud support
|
US5232339A
(en)
*
|
1992-01-28 |
1993-08-03 |
General Electric Company |
Finned structural disk spacer arm
|
US5921749A
(en)
*
|
1996-10-22 |
1999-07-13 |
Siemens Westinghouse Power Corporation |
Vane segment support and alignment device
|
US6120242A
(en)
*
|
1998-11-13 |
2000-09-19 |
General Electric Company |
Blade containing turbine shroud
|
US6340285B1
(en)
|
2000-06-08 |
2002-01-22 |
General Electric Company |
End rail cooling for combined high and low pressure turbine shroud
|
US6354795B1
(en)
|
2000-07-27 |
2002-03-12 |
General Electric Company |
Shroud cooling segment and assembly
|
GB0218060D0
(en)
*
|
2002-08-03 |
2002-09-11 |
Alstom Switzerland Ltd |
Sealing arrangements
|
US6877952B2
(en)
*
|
2002-09-09 |
2005-04-12 |
Florida Turbine Technologies, Inc |
Passive clearance control
|
DE10305899B4
(de)
*
|
2003-02-13 |
2012-06-14 |
Alstom Technology Ltd. |
Dichtungsanordnung zur Dichtspaltreduzierung bei einer Strömungsrotationsmaschine
|
US7575409B2
(en)
*
|
2005-07-01 |
2009-08-18 |
Allison Advanced Development Company |
Apparatus and method for active control of blade tip clearance
|
DE102007003028A1
(de)
*
|
2007-01-20 |
2008-07-24 |
Mtu Aero Engines Gmbh |
Turbomaschine
|
EP1965036A1
(de)
*
|
2007-03-02 |
2008-09-03 |
Siemens Aktiengesellschaft |
Strömungsmaschine mit verstellbarer Strömungskontur
|
FR2928963B1
(fr)
*
|
2008-03-19 |
2017-12-08 |
Snecma |
Distributeur de turbine pour une turbomachine.
|
US8256228B2
(en)
*
|
2008-04-29 |
2012-09-04 |
Rolls Royce Corporation |
Turbine blade tip clearance apparatus and method
|
GB2462581B
(en)
*
|
2008-06-25 |
2010-11-24 |
Rolls Royce Plc |
Rotor path arrangements
|
FR2943717B1
(fr)
*
|
2009-03-27 |
2016-02-19 |
Snecma |
Stator de compresseur ou turbine de turbomachine permettant un controle du jeu en sommet d'aubes d'un rotor en regard
|
EP2386726B1
(de)
*
|
2010-05-12 |
2012-10-31 |
Siemens Aktiengesellschaft |
Kanalwandabschnitt für einen ringförmigen Strömungskanal einer Axialturbomaschine mit Radialspalteinstellung, zugehöriger Axialverdichter und Gasturbine
|
US10077672B2
(en)
*
|
2013-03-08 |
2018-09-18 |
United Technologies Corporation |
Ring-shaped compliant support
|
WO2014186015A2
(en)
*
|
2013-03-11 |
2014-11-20 |
United Technologies Corporation |
Actuator for gas turbine engine blade outer air seal
|
US9598975B2
(en)
*
|
2013-03-14 |
2017-03-21 |
Rolls-Royce Corporation |
Blade track assembly with turbine tip clearance control
|
US10370999B2
(en)
|
2013-04-12 |
2019-08-06 |
United Technologies Corporation |
Gas turbine engine rapid response clearance control system with air seal segment interface
|
WO2014186004A2
(en)
*
|
2013-04-12 |
2014-11-20 |
United Technologies Corporation |
Rapid response clearance control system for gas turbine engine
|
WO2015050628A1
(en)
*
|
2013-10-04 |
2015-04-09 |
United Technologies Corporation |
Gas turbine engine ramped rapid response clearance control system
|
US9915163B2
(en)
*
|
2015-05-15 |
2018-03-13 |
United Technologies Corporation |
Cam-follower active clearance control
|
US9945244B2
(en)
*
|
2015-08-13 |
2018-04-17 |
General Electric Company |
Turbine shroud assembly and method for loading
|
FR3049003B1
(fr)
*
|
2016-03-21 |
2018-04-06 |
Safran Aircraft Engines |
Ensemble d'anneau de turbine sans jeu de montage a froid
|
FR3068071B1
(fr)
*
|
2017-06-26 |
2019-11-08 |
Safran Aircraft Engines |
Ensemble pour la liaison par palonnier entre un carter de turbine et un element annulaire de turbomachine
|