|
US20020125215A1
(en)
*
|
2001-03-07 |
2002-09-12 |
Davis Brian Michael |
Chemical milling of gas turbine engine blisks
|
|
ITMI20021876A1
(it)
*
|
2002-09-03 |
2004-03-04 |
Nuovo Pignone Spa |
Procedimento migliorato per realizzare un rotore di un
|
|
US6780089B2
(en)
*
|
2002-12-03 |
2004-08-24 |
General Electric Company |
Method and apparatus for removing a predetermined amount of material from a bottom portion of a dovetail slot in gas turbine engine disk
|
|
GB2398882B
(en)
*
|
2003-02-27 |
2007-09-05 |
Rolls Royce Plc |
Rotor balancing
|
|
GB2411441B
(en)
*
|
2004-02-24 |
2006-04-19 |
Rolls Royce Plc |
Fan or compressor blisk
|
|
FR2886012B1
(fr)
*
|
2005-05-23 |
2007-07-06 |
Snecma Moteurs Sa |
Procede de calibrage en masse de pieces destinees a etre montees en peripherie d'un rotor
|
|
GB2438642B
(en)
*
|
2006-06-01 |
2008-04-09 |
Rolls Royce Plc |
Rotor unbalance correction
|
|
DE102007059155A1
(de)
*
|
2007-12-06 |
2009-06-10 |
Rolls-Royce Deutschland Ltd & Co Kg |
Verfahren zur Herstellung von in Integralbauweise ausgebildeten Laufrädern für Verdichter und Turbinen
|
|
US8313279B2
(en)
*
|
2008-04-21 |
2012-11-20 |
General Electric Company |
Dual rotor vibration monitoring
|
|
US8328519B2
(en)
|
2008-09-24 |
2012-12-11 |
Pratt & Whitney Canada Corp. |
Rotor with improved balancing features
|
|
US8342804B2
(en)
*
|
2008-09-30 |
2013-01-01 |
Pratt & Whitney Canada Corp. |
Rotor disc and method of balancing
|
|
DE102009014846B4
(de)
|
2009-03-30 |
2018-10-04 |
Rolls-Royce Deutschland Ltd & Co Kg |
Rotor für eine Strömungsmaschine, insbesondere für ein Gasturbinentriebwerk, der in Aussparungen eines Befestigungsflansches Materialentnahmestege zum Auswuchten des Rotors aufweist
|
|
US8316523B2
(en)
|
2009-10-01 |
2012-11-27 |
Pratt & Whitney Canada Corp. |
Method for centering engine structures
|
|
DE102010015404B4
(de)
*
|
2010-04-19 |
2012-02-16 |
Mtu Aero Engines Gmbh |
Verfahren zur Reparatur einer Rotoranordnung einer Turbomaschine, Ringelement für eine Rotoranordnung einer Turbomaschine sowie Rotoranordnung für eine Turbomaschine
|
|
GB2481582A
(en)
*
|
2010-06-28 |
2012-01-04 |
Rolls Royce Plc |
A method for predicting initial unbalance in a component such as a blisk
|
|
CA2761208C
(en)
*
|
2010-12-08 |
2019-03-05 |
Pratt & Whitney Canada Corp. |
Blade disk arrangement for blade frequency tuning
|
|
US9127563B2
(en)
|
2011-04-05 |
2015-09-08 |
General Electric Company |
Locking device arrangement for a rotating bladed stage
|
|
US9169730B2
(en)
|
2011-11-16 |
2015-10-27 |
Pratt & Whitney Canada Corp. |
Fan hub design
|
|
EP2604792B1
(de)
*
|
2011-12-15 |
2015-11-04 |
MTU Aero Engines GmbH |
Verfahren zur Reparatur eines Bauteils einer Turbomaschine und ein gemäß diesem Verfahren repariertes Bauteil
|
|
US20130156584A1
(en)
*
|
2011-12-16 |
2013-06-20 |
Carney R. Anderson |
Compressor rotor with internal stiffening ring of distinct material
|
|
US20130177430A1
(en)
*
|
2012-01-05 |
2013-07-11 |
General Electric Company |
System and method for reducing stress in a rotor
|
|
US9511457B2
(en)
|
2012-02-09 |
2016-12-06 |
Pratt & Whitney Canada Corp. |
Gas turbine engine rotor balancing
|
|
GB201210870D0
(en)
|
2012-06-20 |
2012-08-01 |
Rolls Royce Plc |
Rotor balancing method
|
|
US10982551B1
(en)
|
2012-09-14 |
2021-04-20 |
Raytheon Technologies Corporation |
Turbomachine blade
|
|
WO2015088620A2
(en)
|
2013-09-26 |
2015-06-18 |
United Technologies Corporation |
Rotating component balance ring
|
|
WO2015088623A2
(en)
|
2013-09-26 |
2015-06-18 |
United Technologies Corporation |
Balanced rotating component for a gas powered engine
|
|
GB201400756D0
(en)
*
|
2014-01-16 |
2014-03-05 |
Rolls Royce Plc |
Blisk
|
|
WO2015132091A1
(en)
|
2014-03-03 |
2015-09-11 |
Siemens Aktiengesellschaft |
Rotor component with surfaces for checking concentricity
|
|
FR3021064B1
(fr)
*
|
2014-05-16 |
2020-05-29 |
Safran Aircraft Engines |
Disque et procede d'equilibrage
|
|
US9624775B2
(en)
*
|
2014-05-30 |
2017-04-18 |
Rolls-Royce Plc |
Developments in or relating to rotor balancing
|
|
US20150354361A1
(en)
*
|
2014-06-09 |
2015-12-10 |
General Electric Company |
Rotor assembly and method of manufacturing thereof
|
|
EP2957792B1
(en)
*
|
2014-06-20 |
2020-07-29 |
United Technologies Corporation |
Reduced vibratory response rotor for a gas powered turbine
|
|
US9638037B2
(en)
|
2014-11-03 |
2017-05-02 |
Pratt & Whitney Canada Corp. |
Method of balancing a gas turbine engine rotor
|
|
US10544678B2
(en)
*
|
2015-02-04 |
2020-01-28 |
United Technologies Corporation |
Gas turbine engine rotor disk balancing
|
|
EP3091179B1
(de)
*
|
2015-05-07 |
2021-06-30 |
MTU Aero Engines AG |
Rotoranordnung für eine strömungsmaschine und verdichter
|
|
DE102016120346A1
(de)
|
2016-10-25 |
2018-04-26 |
Rolls-Royce Deutschland Ltd & Co Kg |
Verdichterrotor einer Strömungsmaschine
|
|
US10495097B2
(en)
*
|
2016-12-12 |
2019-12-03 |
Garrett Transporation I Inc. |
Turbocharger assembly
|
|
US11199096B1
(en)
|
2017-01-17 |
2021-12-14 |
Raytheon Technologies Corporation |
Turbomachine blade
|
|
US10968744B2
(en)
|
2017-05-04 |
2021-04-06 |
Rolls-Royce Corporation |
Turbine rotor assembly having a retaining collar for a bayonet mount
|
|
US20180320522A1
(en)
*
|
2017-05-04 |
2018-11-08 |
Rolls-Royce Corporation |
Turbine assembly with auxiliary wheel
|
|
US10774678B2
(en)
|
2017-05-04 |
2020-09-15 |
Rolls-Royce Corporation |
Turbine assembly with auxiliary wheel
|
|
US10865646B2
(en)
|
2017-05-04 |
2020-12-15 |
Rolls-Royce Corporation |
Turbine assembly with auxiliary wheel
|
|
US20190284936A1
(en)
*
|
2018-03-15 |
2019-09-19 |
United Technologies Corporation |
Gas turbine engine rotor disk
|
|
US10794190B1
(en)
*
|
2018-07-30 |
2020-10-06 |
Florida Turbine Technologies, Inc. |
Cast integrally bladed rotor with bore entry cooling
|
|
GB201819413D0
(en)
*
|
2018-11-29 |
2019-01-16 |
Rolls Royce Plc |
Geared turbofan engine
|
|
GB201819412D0
(en)
*
|
2018-11-29 |
2019-01-16 |
Rolls Royce Plc |
Geared turbofan engine
|
|
DE102019208666A1
(de)
*
|
2019-06-14 |
2020-12-17 |
MTU Aero Engines AG |
Rotoren für hochdruckverdichter und niederdruckturbine eines getriebefantriebwerks sowie verfahren zu ihrer herstellung
|
|
FR3108360B1
(fr)
*
|
2020-03-23 |
2023-04-14 |
Safran Aircraft Engines |
Procede et dispositif d’equilibrage d’une piece tournante pour une turbomachine d’aeronef
|
|
JP2022013322A
(ja)
*
|
2020-07-03 |
2022-01-18 |
三菱重工業株式会社 |
タービン
|