|
GB1385666A
(en)
*
|
1973-07-06 |
1975-02-26 |
Rolls Royce |
Sealing of vaned assemblies of gas turbine engines
|
|
US3965066A
(en)
*
|
1974-03-15 |
1976-06-22 |
General Electric Company |
Combustor-turbine nozzle interconnection
|
|
US3910716A
(en)
*
|
1974-05-23 |
1975-10-07 |
Westinghouse Electric Corp |
Gas turbine inlet vane structure utilizing a stable ceramic spherical interface arrangement
|
|
US3966353A
(en)
*
|
1975-02-21 |
1976-06-29 |
Westinghouse Electric Corporation |
Ceramic-to-metal (or ceramic) cushion/seal for use with three piece ceramic stationary vane assembly
|
|
USB552006I5
(US07655688-20100202-C00541.png)
*
|
1975-02-24 |
1976-02-03 |
|
|
|
USB563412I5
(US07655688-20100202-C00541.png)
*
|
1975-03-28 |
1976-02-24 |
|
|
|
US4008978A
(en)
*
|
1976-03-19 |
1977-02-22 |
General Motors Corporation |
Ceramic turbine structures
|
|
IT1167241B
(it)
*
|
1983-10-03 |
1987-05-13 |
Nuovo Pignone Spa |
Sistema perfezionato per il fissaggio degli ugelli statorici alla cassa di una turbina di potenza
|
|
US4639189A
(en)
*
|
1984-02-27 |
1987-01-27 |
Rockwell International Corporation |
Hollow, thermally-conditioned, turbine stator nozzle
|
|
US4768924A
(en)
*
|
1986-07-22 |
1988-09-06 |
Pratt & Whitney Canada Inc. |
Ceramic stator vane assembly
|
|
US4790137A
(en)
*
|
1987-07-17 |
1988-12-13 |
The United States Of America As Represented By The Secretary Of The Air Force |
Aircraft engine outer duct mounting device
|
|
US4861229A
(en)
*
|
1987-11-16 |
1989-08-29 |
Williams International Corporation |
Ceramic-matrix composite nozzle assembly for a turbine engine
|
|
US4863343A
(en)
*
|
1988-05-16 |
1989-09-05 |
Westinghouse Electric Corp. |
Turbine vane shroud sealing system
|
|
US4890978A
(en)
*
|
1988-10-19 |
1990-01-02 |
Westinghouse Electric Corp. |
Method and apparatus for vane segment support and alignment in combustion turbines
|
|
US4934900A
(en)
*
|
1989-07-31 |
1990-06-19 |
Fuller Company |
Assembly forming a cylindrical cage of spaced apart vanes
|
|
DE4017861A1
(de)
*
|
1990-06-02 |
1991-12-05 |
Mtu Muenchen Gmbh |
Leitkranz fuer eine gasturbine
|
|
US5141394A
(en)
*
|
1990-10-10 |
1992-08-25 |
Westinghouse Electric Corp. |
Apparatus and method for supporting a vane segment in a gas turbine
|
|
US5441385A
(en)
*
|
1993-12-13 |
1995-08-15 |
Solar Turbines Incorporated |
Turbine nozzle/nozzle support structure
|
|
US5653580A
(en)
*
|
1995-03-06 |
1997-08-05 |
Solar Turbines Incorporated |
Nozzle and shroud assembly mounting structure
|
|
US5618161A
(en)
*
|
1995-10-17 |
1997-04-08 |
Westinghouse Electric Corporation |
Apparatus for restraining motion of a turbo-machine stationary vane
|
|
DE19807247C2
(de)
*
|
1998-02-20 |
2000-04-20 |
Mtu Muenchen Gmbh |
Strömungsmaschine mit Rotor und Stator
|
|
US6517313B2
(en)
*
|
2001-06-25 |
2003-02-11 |
Pratt & Whitney Canada Corp. |
Segmented turbine vane support structure
|
|
FR2831600B1
(fr)
*
|
2001-10-25 |
2004-01-02 |
Snecma Moteurs |
Dispositif d'arret en rotation d'un secteur porteur d'aubes fixes dans une virole d'une turbomachine
|
|
JP4346412B2
(ja)
*
|
2003-10-31 |
2009-10-21 |
株式会社東芝 |
タービン翼列装置
|
|
US7160078B2
(en)
*
|
2004-09-23 |
2007-01-09 |
General Electric Company |
Mechanical solution for rail retention of turbine nozzles
|
|
US7665960B2
(en)
*
|
2006-08-10 |
2010-02-23 |
United Technologies Corporation |
Turbine shroud thermal distortion control
|
|
US7713024B2
(en)
*
|
2007-02-09 |
2010-05-11 |
General Electric Company |
Bling nozzle/carrier interface design for a steam turbine
|
|
FR2923530B1
(fr)
*
|
2007-11-09 |
2014-04-04 |
Snecma |
Raccordement de bras radiaux a une virole circulaire par des axes et des entretoises
|
|
FR2935430B1
(fr)
*
|
2008-08-26 |
2012-03-09 |
Snecma |
Turbine haute-pression de turbomachine amelioree, secteur de distributeur et moteur d'aeronef associes
|
|
US8133015B2
(en)
*
|
2008-09-30 |
2012-03-13 |
General Electric Company |
Turbine nozzle for a gas turbine engine
|
|
US9840917B2
(en)
|
2011-12-13 |
2017-12-12 |
United Technologies Corporation |
Stator vane shroud having an offset
|
|
WO2014046965A1
(en)
|
2012-09-20 |
2014-03-27 |
United Technologies Corporation |
Fan drive gear system module and inlet guide vane coupling mechanism
|
|
CN103511001B
(zh)
*
|
2013-07-11 |
2015-04-22 |
哈尔滨汽轮机厂有限责任公司 |
一种用于重型中低热值燃机的涡轮首级导叶
|
|
WO2015147821A1
(en)
*
|
2014-03-27 |
2015-10-01 |
Siemens Aktiengesellschaft |
Stator vane support system within a gas turbine engine
|
|
US9945242B2
(en)
*
|
2015-05-11 |
2018-04-17 |
General Electric Company |
System for thermally isolating a turbine shroud
|
|
US10233782B2
(en)
*
|
2016-08-03 |
2019-03-19 |
Solar Turbines Incorporated |
Turbine assembly and method for flow control
|
|
DE102016215807A1
(de)
*
|
2016-08-23 |
2018-03-01 |
MTU Aero Engines AG |
Innenring für einen Leitschaufelkranz einer Strömungsmaschine
|
|
DE102017109952A1
(de)
*
|
2017-05-09 |
2018-11-15 |
Rolls-Royce Deutschland Ltd & Co Kg |
Rotorvorrichtung einer Strömungsmaschine
|
|
DE102018210601A1
(de)
*
|
2018-06-28 |
2020-01-02 |
MTU Aero Engines AG |
Segmentring zur montage in einer strömungsmaschine
|
|
US11028709B2
(en)
*
|
2018-09-18 |
2021-06-08 |
General Electric Company |
Airfoil shroud assembly using tenon with externally threaded stud and nut
|
|
US10968777B2
(en)
*
|
2019-04-24 |
2021-04-06 |
Raytheon Technologies Corporation |
Chordal seal
|
|
PL431184A1
(pl)
|
2019-09-17 |
2021-03-22 |
General Electric Company Polska Spółka Z Ograniczoną Odpowiedzialnością |
Zespół silnika turbinowego
|
|
US11939888B2
(en)
*
|
2022-06-17 |
2024-03-26 |
Rtx Corporation |
Airfoil anti-rotation ring and assembly
|
