JPS50155818A
(it)
*
|
1974-06-07 |
1975-12-16 |
|
|
US4021138A
(en)
*
|
1975-11-03 |
1977-05-03 |
Westinghouse Electric Corporation |
Rotor disk, blade, and seal plate assembly for cooled turbine rotor blades
|
GB1512882A
(en)
*
|
1976-02-11 |
1978-06-01 |
Rolls Royce |
Bladed rotor assembly for a gas turbine engine
|
US4218189A
(en)
*
|
1977-08-09 |
1980-08-19 |
Rolls-Royce Limited |
Sealing means for bladed rotor for a gas turbine engine
|
US4275990A
(en)
*
|
1977-12-17 |
1981-06-30 |
Rolls-Royce Limited |
Disc channel for cooling rotor blade roots
|
US4685863A
(en)
*
|
1979-06-27 |
1987-08-11 |
United Technologies Corporation |
Turbine rotor assembly
|
FR2468727A1
(fr)
*
|
1979-10-26 |
1981-05-08 |
Snecma |
Perfectionnement aux aubes de turbine refroidies
|
US4422827A
(en)
*
|
1982-02-18 |
1983-12-27 |
United Technologies Corporation |
Blade root seal
|
US4439107A
(en)
*
|
1982-09-16 |
1984-03-27 |
United Technologies Corporation |
Rotor blade cooling air chamber
|
US4507052A
(en)
*
|
1983-03-31 |
1985-03-26 |
General Motors Corporation |
End seal for turbine blade bases
|
US4523890A
(en)
*
|
1983-10-19 |
1985-06-18 |
General Motors Corporation |
End seal for turbine blade base
|
US4674955A
(en)
*
|
1984-12-21 |
1987-06-23 |
The Garrett Corporation |
Radial inboard preswirl system
|
US4759688A
(en)
*
|
1986-12-16 |
1988-07-26 |
Allied-Signal Inc. |
Cooling flow side entry for cooled turbine blading
|
US4898514A
(en)
*
|
1987-10-27 |
1990-02-06 |
United Technologies Corporation |
Turbine balance arrangement with integral air passage
|
FR2639063A1
(fr)
*
|
1988-11-17 |
1990-05-18 |
Snecma |
Segment d'arret et d'etancheite d'un ensemble d'aubes monte sur un disque de rotor de turbomachine
|
US5018943A
(en)
*
|
1989-04-17 |
1991-05-28 |
General Electric Company |
Boltless balance weight for turbine rotors
|
US5112193A
(en)
*
|
1990-09-11 |
1992-05-12 |
Pratt & Whitney Canada |
Fan blade axial retention device
|
US5256035A
(en)
*
|
1992-06-01 |
1993-10-26 |
United Technologies Corporation |
Rotor blade retention and sealing construction
|
US5302086A
(en)
*
|
1992-08-18 |
1994-04-12 |
General Electric Company |
Apparatus for retaining rotor blades
|
JP3811502B2
(ja)
*
|
1994-08-24 |
2006-08-23 |
ウエスチングハウス・エレクトリック・コーポレイション |
冷却式プラットホームを備えたガスタービン翼
|
EP0789806B1
(en)
*
|
1994-10-31 |
1998-07-29 |
Westinghouse Electric Corporation |
Gas turbine blade with a cooled platform
|
US6059529A
(en)
*
|
1998-03-16 |
2000-05-09 |
Siemens Westinghouse Power Corporation |
Turbine blade assembly with cooling air handling device
|
US6273683B1
(en)
|
1999-02-05 |
2001-08-14 |
Siemens Westinghouse Power Corporation |
Turbine blade platform seal
|
CA2371131A1
(en)
*
|
1999-06-07 |
2000-12-14 |
Siemens Aktiengesellschaft |
Turbomachine and sealing element for a rotor of a turbomachine
|
JP3864157B2
(ja)
*
|
2003-12-05 |
2006-12-27 |
本田技研工業株式会社 |
軸流型タービンホイール
|
US7192245B2
(en)
*
|
2004-12-03 |
2007-03-20 |
Pratt & Whitney Canada Corp. |
Rotor assembly with cooling air deflectors and method
|
DE102005024932A1
(de)
*
|
2005-05-31 |
2006-12-07 |
Rolls-Royce Deutschland Ltd & Co Kg |
Turbinenschaufelaxialsperre
|
US20060275107A1
(en)
*
|
2005-06-07 |
2006-12-07 |
Ioannis Alvanos |
Combined blade attachment and disk lug fluid seal
|
WO2007028703A1
(de)
*
|
2005-09-07 |
2007-03-15 |
Siemens Aktiengesellschaft |
Anordnung zur axialsicherung von laufschaufeln in einem rotor sowie verwendung
|
US7484936B2
(en)
*
|
2005-09-26 |
2009-02-03 |
Pratt & Whitney Canada Corp. |
Blades for a gas turbine engine with integrated sealing plate and method
|
US7500832B2
(en)
*
|
2006-07-06 |
2009-03-10 |
Siemens Energy, Inc. |
Turbine blade self locking seal plate system
|
FR2905139B1
(fr)
*
|
2006-08-25 |
2012-09-28 |
Snecma |
Aube de rotor d'une turbomachine
|
DE602006006452D1
(de)
*
|
2006-09-25 |
2009-06-04 |
Siemens Ag |
Turbinenrotor mit Verschlussplatten und entsprechendes Montageverfahren
|
US7762780B2
(en)
*
|
2007-01-25 |
2010-07-27 |
Siemens Energy, Inc. |
Blade assembly in a combustion turbo-machine providing reduced concentration of mechanical stress and a seal between adjacent assemblies
|
US7566201B2
(en)
*
|
2007-01-30 |
2009-07-28 |
Siemens Energy, Inc. |
Turbine seal plate locking system
|
US8128371B2
(en)
*
|
2007-02-15 |
2012-03-06 |
General Electric Company |
Method and apparatus to facilitate increasing turbine rotor efficiency
|
FR2918106B1
(fr)
*
|
2007-06-27 |
2011-05-06 |
Snecma |
Dispositif de retenue axiale d'aubes montees sur un disque de rotor de turbomachine.
|
WO2009019126A1
(de)
*
|
2007-08-08 |
2009-02-12 |
Alstom Technology Ltd |
Rotoranordnung von einer turbine
|
US20090110561A1
(en)
*
|
2007-10-29 |
2009-04-30 |
Honeywell International, Inc. |
Turbine engine components, turbine engine assemblies, and methods of manufacturing turbine engine components
|
US10544677B2
(en)
|
2017-09-01 |
2020-01-28 |
United Technologies Corporation |
Turbine disk
|
US7918265B2
(en)
*
|
2008-02-14 |
2011-04-05 |
United Technologies Corporation |
Method and apparatus for as-cast seal on turbine blades
|
US8038405B2
(en)
*
|
2008-07-08 |
2011-10-18 |
General Electric Company |
Spring seal for turbine dovetail
|
EP2146051B1
(en)
*
|
2008-07-17 |
2011-09-07 |
Ansaldo Energia S.P.A. |
Rotor assembly for a gas turbine, gas turbine including said rotor assembly and method for cooling said rotor assembly
|
EP2218873A1
(de)
*
|
2009-02-17 |
2010-08-18 |
Siemens Aktiengesellschaft |
Rotorabschnitt für einen Rotor einer Turbomaschine, Laufschaufel für eine Turbomaschine und Blockierelement
|
US8696320B2
(en)
*
|
2009-03-12 |
2014-04-15 |
General Electric Company |
Gas turbine having seal assembly with coverplate and seal
|
US20100232939A1
(en)
*
|
2009-03-12 |
2010-09-16 |
General Electric Company |
Machine Seal Assembly
|
EP2236759A1
(de)
*
|
2009-03-27 |
2010-10-06 |
Siemens Aktiengesellschaft |
Laufschaufelsystem
|
US9109457B2
(en)
*
|
2010-09-03 |
2015-08-18 |
Siemens Energy, Inc. |
Axial locking seals for aft removable turbine blade
|
EP2964894B1
(en)
|
2013-03-05 |
2019-04-10 |
Rolls-Royce North American Technologies, Inc. |
Turbine segmented cover plate retention method
|
JP5358031B1
(ja)
*
|
2013-03-22 |
2013-12-04 |
三菱重工業株式会社 |
タービンロータ、タービン、及びシール板の取外方法
|
FR3011032B1
(fr)
*
|
2013-09-25 |
2017-12-29 |
Snecma |
Ensemble rotatif pour turbomachine
|
EP2860350A1
(de)
*
|
2013-10-10 |
2015-04-15 |
Siemens Aktiengesellschaft |
Turbinenschaufel sowie Gasturbine
|
EP2933436A1
(de)
*
|
2014-04-15 |
2015-10-21 |
Siemens Aktiengesellschaft |
Radscheibe mit wenigstens einem Dichtblech
|
GB201417038D0
(en)
*
|
2014-09-26 |
2014-11-12 |
Rolls Royce Plc |
A bladed rotor arrangement
|
EP3048256A1
(de)
*
|
2015-01-20 |
2016-07-27 |
Siemens Aktiengesellschaft |
Rotor umfassend eine Turbinenschaufel mit einer Sicherungseinrichtung
|
CN105065065A
(zh)
*
|
2015-08-07 |
2015-11-18 |
山东青能动力股份有限公司 |
一种枞树型叶根动叶片锁紧装置及其装配工艺
|
GB201516657D0
(en)
*
|
2015-09-21 |
2015-11-04 |
Rolls Royce Plc |
Seal-plate anti-rotation in a stage of a gas turbine engine
|
MX2019006639A
(es)
*
|
2016-12-13 |
2019-08-01 |
Mitsubishi Hitachi Power Sys |
Metodo para desmontar/montar turbina de gas, montaje de placa selladora y rotor de turbina de gas.
|
JP6817330B2
(ja)
*
|
2016-12-13 |
2021-01-20 |
三菱パワー株式会社 |
ガスタービンの分解組立方法、シール板組立体及びガスタービンロータ
|
WO2018110584A1
(ja)
*
|
2016-12-13 |
2018-06-21 |
三菱日立パワーシステムズ株式会社 |
ガスタービンの分解組立方法、ガスタービンロータ及びガスタービン
|
KR101882109B1
(ko)
*
|
2016-12-23 |
2018-07-25 |
두산중공업 주식회사 |
가스 터빈
|
FR3064667B1
(fr)
*
|
2017-03-31 |
2020-05-15 |
Safran Aircraft Engines |
Dispositif de refroidissement d'un rotor de turbomachine
|
KR101878360B1
(ko)
*
|
2017-04-12 |
2018-07-13 |
두산중공업 주식회사 |
리테이너 조립구조를 포함하는 가스터빈 블레이드 조립체 및 이를 포함하는 가스터빈
|
EP3438410B1
(en)
|
2017-08-01 |
2021-09-29 |
General Electric Company |
Sealing system for a rotary machine
|
US10724374B2
(en)
|
2017-09-01 |
2020-07-28 |
Raytheon Technologies Corporation |
Turbine disk
|
US10550702B2
(en)
*
|
2017-09-01 |
2020-02-04 |
United Technologies Corporation |
Turbine disk
|
US10641110B2
(en)
*
|
2017-09-01 |
2020-05-05 |
United Technologies Corporation |
Turbine disk
|
US10472968B2
(en)
|
2017-09-01 |
2019-11-12 |
United Technologies Corporation |
Turbine disk
|
EP3564489A1
(de)
*
|
2018-05-03 |
2019-11-06 |
Siemens Aktiengesellschaft |
Rotor mit fliehkraft-optimierten kontaktflächen
|
KR102142141B1
(ko)
*
|
2018-08-17 |
2020-08-06 |
두산중공업 주식회사 |
터빈, 가스 터빈, 및 터빈 블레이드 분리 방법
|
KR102134812B1
(ko)
|
2018-08-17 |
2020-07-16 |
두산중공업 주식회사 |
터빈, 이를 포함하는 가스 터빈, 터빈의 조립 방법, 및 터빈의 분해 방법
|
CN109707464A
(zh)
*
|
2018-12-14 |
2019-05-03 |
北京全四维动力科技有限公司 |
用于保护蒸汽轮机叶片叶根和轮槽的组合装置
|
KR102205571B1
(ko)
*
|
2019-06-05 |
2021-01-20 |
두산중공업 주식회사 |
터빈 로터 디스크에 대한 터빈 블레이드의 고정 및 실링 구조
|
US11377967B2
(en)
*
|
2019-12-06 |
2022-07-05 |
Raytheon Technologies Corporation |
Pre-formed faceted turbine blade damper seal
|
US11313240B2
(en)
*
|
2020-02-05 |
2022-04-26 |
Raytheon Technologies Corporation |
Rounded radial snap configuration for a gas turbine engine cover plate
|
US11352892B2
(en)
*
|
2020-04-17 |
2022-06-07 |
Raytheon Technologies Corporation |
Seal element for sealing a joint between a rotor blade and a rotor disk
|