US4324441A
(en)
*
|
1980-10-24 |
1982-04-13 |
Rouverol William S |
Rolling contact element
|
US4353604A
(en)
*
|
1980-12-11 |
1982-10-12 |
United Technologies Corporation |
Viscous/friction damper
|
FR2504980B1
(fr)
*
|
1981-04-29 |
1985-06-14 |
Snecma |
Montage de palier, en particulier pour turbomachines
|
US4386812A
(en)
*
|
1981-07-06 |
1983-06-07 |
Marathon Electric Manufacturing Corp. |
Bearing lock for a dynamoelectric machine
|
JPS5910520U
(ja)
*
|
1982-07-12 |
1984-01-23 |
石川島播磨重工業株式会社 |
軸受用弾性支持バネ
|
US4570045A
(en)
*
|
1984-03-08 |
1986-02-11 |
Jeppson Morris R |
Conveyorized microwave heating chamber with dielectric wall structure
|
GB8421142D0
(en)
*
|
1984-08-20 |
1984-09-26 |
Brown R D |
Damping device
|
JPH028102Y2
(it)
*
|
1985-02-07 |
1990-02-27 |
|
|
US4872767A
(en)
*
|
1985-04-03 |
1989-10-10 |
General Electric Company |
Bearing support
|
JPS6375341A
(ja)
*
|
1986-09-17 |
1988-04-05 |
Fujio Hisashi |
ピストンピンのないピストンをもつレシプロエンジン
|
DE4134604C2
(de)
*
|
1991-10-19 |
2000-01-13 |
Schaeffler Waelzlager Ohg |
Wälzlager mit Geräuschdämpfung
|
DE4227366A1
(de)
*
|
1992-08-19 |
1994-02-24 |
Schaeffler Waelzlager Kg |
Lagerung mit Dämpfung
|
DE4424640A1
(de)
*
|
1994-07-13 |
1996-01-18 |
Abb Management Ag |
Lagerung eines Abgasturboladers
|
FR2749883B1
(fr)
*
|
1996-06-13 |
1998-07-31 |
Snecma |
Procede et support de palier permettant de maintenir en fonctionnement un turbomoteur pour aeronef apres apparition d'un balourd accidentel sur un rotor
|
GB2320526B
(en)
*
|
1996-12-20 |
2000-09-20 |
Rolls Royce Plc |
Ducted fan gas turbine engine
|
GB2323637B
(en)
*
|
1997-03-25 |
2000-12-13 |
Rolls Royce Plc |
Ducted fan gas turbine engine
|
US5791789A
(en)
*
|
1997-04-24 |
1998-08-11 |
United Technologies Corporation |
Rotor support for a turbine engine
|
US6332752B2
(en)
|
1997-06-27 |
2001-12-25 |
Ebara Corporation |
Turbo-molecular pump
|
US5971706A
(en)
*
|
1997-12-03 |
1999-10-26 |
General Electric Company |
Inter-rotor bearing assembly
|
US6786439B2
(en)
*
|
2000-11-15 |
2004-09-07 |
Diamond Z Manufacturing |
Retractable rod screens
|
US6439772B1
(en)
*
|
2000-12-01 |
2002-08-27 |
General Electric Company |
Method and apparatus for supporting rotor assembly bearings
|
US6428269B1
(en)
|
2001-04-18 |
2002-08-06 |
United Technologies Corporation |
Turbine engine bearing support
|
US6540483B2
(en)
|
2001-08-27 |
2003-04-01 |
General Electric Company |
Methods and apparatus for bearing outer race axial retention
|
DE10202977C1
(de)
*
|
2002-01-26 |
2003-10-30 |
Mtu Aero Engines Gmbh |
Drehlagerung mit einer Sollbruchstelle
|
GB2394015A
(en)
*
|
2002-10-12 |
2004-04-14 |
Rolls Royce Plc |
Powerplant shaft with vibration damping device
|
FR2846379B1
(fr)
*
|
2002-10-23 |
2005-01-21 |
Snecma Moteurs |
Systeme de decouplage par charge explosive d'une soufflante d'un turboreacteur
|
US6910863B2
(en)
*
|
2002-12-11 |
2005-06-28 |
General Electric Company |
Methods and apparatus for assembling a bearing assembly
|
DE10330829B4
(de)
*
|
2003-07-08 |
2012-08-23 |
Mtu Aero Engines Gmbh |
Lageranordnung für eine Gasturbine
|
FR2866068B1
(fr)
*
|
2004-02-06 |
2006-07-07 |
Snecma Moteurs |
Turboreacteur a soufflante solidaire d'un arbre d'entrainement supporte par un premier et un deuxieme paliers
|
US7097413B2
(en)
*
|
2004-05-12 |
2006-08-29 |
United Technologies Corporation |
Bearing support
|
DE102005003986A1
(de)
*
|
2005-01-28 |
2006-08-03 |
Schaeffler Kg |
Lager
|
US7704178B2
(en)
|
2006-07-05 |
2010-04-27 |
United Technologies Corporation |
Oil baffle for gas turbine fan drive gear system
|
US8667688B2
(en)
|
2006-07-05 |
2014-03-11 |
United Technologies Corporation |
Method of assembly for gas turbine fan drive gear system
|
US10107231B2
(en)
|
2006-08-15 |
2018-10-23 |
United Technologies Corporation |
Gas turbine engine with geared architecture
|
US8753243B2
(en)
|
2006-08-15 |
2014-06-17 |
United Technologies Corporation |
Ring gear mounting arrangement with oil scavenge scheme
|
US9976437B2
(en)
|
2006-08-15 |
2018-05-22 |
United Technologies Corporation |
Epicyclic gear train
|
US8104262B2
(en)
|
2006-10-12 |
2012-01-31 |
United Technologies Corporation |
Dual function cascade integrated variable area fan nozzle and thrust reverser
|
US20080273961A1
(en)
|
2007-03-05 |
2008-11-06 |
Rosenkrans William E |
Flutter sensing and control system for a gas turbine engine
|
JP4882888B2
(ja)
*
|
2007-06-27 |
2012-02-22 |
日本精工株式会社 |
転がり軸受固定装置
|
US11242805B2
(en)
|
2007-08-01 |
2022-02-08 |
Raytheon Technologies Corporation |
Turbine section of high bypass turbofan
|
US11486311B2
(en)
|
2007-08-01 |
2022-11-01 |
Raytheon Technologies Corporation |
Turbine section of high bypass turbofan
|
US11346289B2
(en)
|
2007-08-01 |
2022-05-31 |
Raytheon Technologies Corporation |
Turbine section of high bypass turbofan
|
US11149650B2
(en)
|
2007-08-01 |
2021-10-19 |
Raytheon Technologies Corporation |
Turbine section of high bypass turbofan
|
US20150377123A1
(en)
|
2007-08-01 |
2015-12-31 |
United Technologies Corporation |
Turbine section of high bypass turbofan
|
US9701415B2
(en)
|
2007-08-23 |
2017-07-11 |
United Technologies Corporation |
Gas turbine engine with axial movable fan variable area nozzle
|
US9957918B2
(en)
|
2007-08-28 |
2018-05-01 |
United Technologies Corporation |
Gas turbine engine front architecture
|
US20140157754A1
(en)
|
2007-09-21 |
2014-06-12 |
United Technologies Corporation |
Gas turbine engine compressor arrangement
|
US20140174056A1
(en)
|
2008-06-02 |
2014-06-26 |
United Technologies Corporation |
Gas turbine engine with low stage count low pressure turbine
|
US8182156B2
(en)
*
|
2008-07-31 |
2012-05-22 |
General Electric Company |
Nested bearing cages
|
US9885313B2
(en)
|
2009-03-17 |
2018-02-06 |
United Technologes Corporation |
Gas turbine engine bifurcation located fan variable area nozzle
|
US8727699B2
(en)
*
|
2009-12-29 |
2014-05-20 |
Rolls-Royce Corporation |
Rotating machinery with damping system
|
US8845277B2
(en)
|
2010-05-24 |
2014-09-30 |
United Technologies Corporation |
Geared turbofan engine with integral gear and bearing supports
|
US9995174B2
(en)
|
2010-10-12 |
2018-06-12 |
United Technologies Corporation |
Planetary gear system arrangement with auxiliary oil system
|
US10605167B2
(en)
|
2011-04-15 |
2020-03-31 |
United Technologies Corporation |
Gas turbine engine front center body architecture
|
US9631558B2
(en)
|
2012-01-03 |
2017-04-25 |
United Technologies Corporation |
Geared architecture for high speed and small volume fan drive turbine
|
US9523422B2
(en)
|
2011-06-08 |
2016-12-20 |
United Technologies Corporation |
Flexible support structure for a geared architecture gas turbine engine
|
US9239012B2
(en)
|
2011-06-08 |
2016-01-19 |
United Technologies Corporation |
Flexible support structure for a geared architecture gas turbine engine
|
US9506422B2
(en)
|
2011-07-05 |
2016-11-29 |
United Technologies Corporation |
Efficient, low pressure ratio propulsor for gas turbine engines
|
US9909505B2
(en)
|
2011-07-05 |
2018-03-06 |
United Technologies Corporation |
Efficient, low pressure ratio propulsor for gas turbine engines
|
US8727632B2
(en)
|
2011-11-01 |
2014-05-20 |
General Electric Company |
Bearing support apparatus for a gas turbine engine
|
US9416677B2
(en)
|
2012-01-10 |
2016-08-16 |
United Technologies Corporation |
Gas turbine engine forward bearing compartment architecture
|
US20130186058A1
(en)
|
2012-01-24 |
2013-07-25 |
William G. Sheridan |
Geared turbomachine fan and compressor rotation
|
DE202012000906U1
(de)
|
2012-01-31 |
2013-02-01 |
Tu Darmstadt |
Erfindung betreffend Gleitlager
|
US8863491B2
(en)
|
2012-01-31 |
2014-10-21 |
United Technologies Corporation |
Gas turbine engine shaft bearing configuration
|
US10287914B2
(en)
|
2012-01-31 |
2019-05-14 |
United Technologies Corporation |
Gas turbine engine with high speed low pressure turbine section and bearing support features
|
US20130192198A1
(en)
|
2012-01-31 |
2013-08-01 |
Lisa I. Brilliant |
Compressor flowpath
|
US10113434B2
(en)
|
2012-01-31 |
2018-10-30 |
United Technologies Corporation |
Turbine blade damper seal
|
US10724431B2
(en)
|
2012-01-31 |
2020-07-28 |
Raytheon Technologies Corporation |
Buffer system that communicates buffer supply air to one or more portions of a gas turbine engine
|
US9394852B2
(en)
|
2012-01-31 |
2016-07-19 |
United Technologies Corporation |
Variable area fan nozzle with wall thickness distribution
|
EP2623800A1
(de)
|
2012-01-31 |
2013-08-07 |
Technische Universität Darmstadt |
Gleitlager
|
US10400629B2
(en)
|
2012-01-31 |
2019-09-03 |
United Technologies Corporation |
Gas turbine engine shaft bearing configuration
|
US20160130949A1
(en)
|
2012-01-31 |
2016-05-12 |
United Technologies Corporation |
Low noise turbine for geared turbofan engine
|
US20130192251A1
(en)
|
2012-01-31 |
2013-08-01 |
Peter M. Munsell |
Buffer system that communicates buffer supply air to one or more portions of a gas turbine engine
|
US10415468B2
(en)
|
2012-01-31 |
2019-09-17 |
United Technologies Corporation |
Gas turbine engine buffer system
|
US20130192191A1
(en)
|
2012-01-31 |
2013-08-01 |
Frederick M. Schwarz |
Gas turbine engine with high speed low pressure turbine section and bearing support features
|
US8869508B2
(en)
|
2012-01-31 |
2014-10-28 |
United Technologies Corporation |
Gas turbine engine variable area fan nozzle control
|
US9169781B2
(en)
|
2012-01-31 |
2015-10-27 |
United Technologies Corporation |
Turbine engine gearbox
|
US10107191B2
(en)
|
2012-02-29 |
2018-10-23 |
United Technologies Corporation |
Geared gas turbine engine with reduced fan noise
|
US10125693B2
(en)
|
2012-04-02 |
2018-11-13 |
United Technologies Corporation |
Geared turbofan engine with power density range
|
US10138809B2
(en)
|
2012-04-02 |
2018-11-27 |
United Technologies Corporation |
Geared turbofan engine with a high ratio of thrust to turbine volume
|
US10001028B2
(en)
|
2012-04-23 |
2018-06-19 |
General Electric Company |
Dual spring bearing support housing
|
US9074485B2
(en)
|
2012-04-25 |
2015-07-07 |
United Technologies Corporation |
Geared turbofan with three turbines all counter-rotating
|
US8572943B1
(en)
|
2012-05-31 |
2013-11-05 |
United Technologies Corporation |
Fundamental gear system architecture
|
WO2014051672A1
(en)
|
2012-09-28 |
2014-04-03 |
United Technologies Corporation |
Split-zone flow metering t-tube
|
BR112015007733B1
(pt)
|
2012-10-08 |
2022-05-03 |
United Technologies Corporation |
Motores de turbina a gás, e, método para distribuir peso entre um conjunto de propulsor e um conjunto de gerador de gás de um motor de turbina a gás
|
WO2014058710A1
(en)
|
2012-10-09 |
2014-04-17 |
United Technologies Corporation |
Improved operability geared turbofan engine including compressor section variable guide vanes
|
US9920653B2
(en)
|
2012-12-20 |
2018-03-20 |
United Technologies Corporation |
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
|
US9932933B2
(en)
|
2012-12-20 |
2018-04-03 |
United Technologies Corporation |
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
|
US10436120B2
(en)
|
2013-02-06 |
2019-10-08 |
United Technologies Corporation |
Exhaust nozzle for an elongated gear turbofan with high bypass ratio
|
EP3882448B1
(en)
|
2013-03-12 |
2024-07-10 |
RTX Corporation |
Flexible coupling for geared turbine engine
|
US11719161B2
(en)
|
2013-03-14 |
2023-08-08 |
Raytheon Technologies Corporation |
Low noise turbine for geared gas turbine engine
|
US10605172B2
(en)
|
2013-03-14 |
2020-03-31 |
United Technologies Corporation |
Low noise turbine for geared gas turbine engine
|
US10024241B2
(en)
*
|
2013-03-15 |
2018-07-17 |
United Technologies Corporation |
Turbine engine face seal arrangement including anti-rotation features
|
US10113481B2
(en)
|
2013-03-15 |
2018-10-30 |
United Technologies Corporation |
Turbofan engine bearing and gearbox arrangement
|
US10724479B2
(en)
|
2013-03-15 |
2020-07-28 |
United Technologies Corporation |
Thrust efficient turbofan engine
|
EP3008323B1
(en)
|
2013-05-09 |
2021-11-10 |
Raytheon Technologies Corporation |
Turbofan engine front section
|
EP2994628A4
(en)
|
2013-05-09 |
2017-01-18 |
United Technologies Corporation |
Turbofan engine front section
|
WO2015088619A2
(en)
|
2013-10-16 |
2015-06-18 |
United Technologies Corporation |
Geared turbofan engine with targeted modular efficiency
|
DE102013111532A1
(de)
*
|
2013-10-18 |
2015-04-23 |
Rolls-Royce Deutschland Ltd & Co Kg |
Vorrichtung zur Lagerung einer Welle eines Strahltriebwerks
|
WO2015112212A2
(en)
|
2013-11-01 |
2015-07-30 |
United Technologies Corporation |
Geared turbofan arrangement with core split power ratio
|
US10502163B2
(en)
|
2013-11-01 |
2019-12-10 |
United Technologies Corporation |
Geared turbofan arrangement with core split power ratio
|
US8869504B1
(en)
|
2013-11-22 |
2014-10-28 |
United Technologies Corporation |
Geared turbofan engine gearbox arrangement
|
US10502229B2
(en)
|
2014-02-19 |
2019-12-10 |
United Technologies Corporation |
Gas turbine engine airfoil
|
US10570916B2
(en)
|
2014-02-19 |
2020-02-25 |
United Technologies Corporation |
Gas turbine engine airfoil
|
US10495106B2
(en)
|
2014-02-19 |
2019-12-03 |
United Technologies Corporation |
Gas turbine engine airfoil
|
US10605259B2
(en)
|
2014-02-19 |
2020-03-31 |
United Technologies Corporation |
Gas turbine engine airfoil
|
WO2015126774A1
(en)
|
2014-02-19 |
2015-08-27 |
United Technologies Corporation |
Gas turbine engine airfoil
|
US10557477B2
(en)
|
2014-02-19 |
2020-02-11 |
United Technologies Corporation |
Gas turbine engine airfoil
|
US10584715B2
(en)
|
2014-02-19 |
2020-03-10 |
United Technologies Corporation |
Gas turbine engine airfoil
|
US10465702B2
(en)
|
2014-02-19 |
2019-11-05 |
United Technologies Corporation |
Gas turbine engine airfoil
|
US10280843B2
(en)
|
2014-03-07 |
2019-05-07 |
United Technologies Corporation |
Geared turbofan with integral front support and carrier
|
US9976490B2
(en)
|
2014-07-01 |
2018-05-22 |
United Technologies Corporation |
Geared gas turbine engine with oil deaerator
|
US10060289B2
(en)
|
2014-07-29 |
2018-08-28 |
United Technologies Corporation |
Geared gas turbine engine with oil deaerator and air removal
|
US9915225B2
(en)
|
2015-02-06 |
2018-03-13 |
United Technologies Corporation |
Propulsion system arrangement for turbofan gas turbine engine
|
US9470093B2
(en)
|
2015-03-18 |
2016-10-18 |
United Technologies Corporation |
Turbofan arrangement with blade channel variations
|
US10371168B2
(en)
|
2015-04-07 |
2019-08-06 |
United Technologies Corporation |
Modal noise reduction for gas turbine engine
|
US10458270B2
(en)
|
2015-06-23 |
2019-10-29 |
United Technologies Corporation |
Roller bearings for high ratio geared turbofan engine
|
US9909451B2
(en)
|
2015-07-09 |
2018-03-06 |
General Electric Company |
Bearing assembly for supporting a rotor shaft of a gas turbine engine
|
US10508562B2
(en)
|
2015-12-01 |
2019-12-17 |
United Technologies Corporation |
Geared turbofan with four star/planetary gear reduction
|
US10669948B2
(en)
|
2017-01-03 |
2020-06-02 |
Raytheon Technologies Corporation |
Geared turbofan with non-epicyclic gear reduction system
|
US10662811B2
(en)
*
|
2017-05-11 |
2020-05-26 |
Raytheon Technologies Corporation |
Fluid damping structure ring and method of fluid damping
|
EP3412877B1
(en)
*
|
2017-06-05 |
2020-08-19 |
General Electric Company |
Bearing bumper for blade out events
|
US10738646B2
(en)
|
2017-06-12 |
2020-08-11 |
Raytheon Technologies Corporation |
Geared turbine engine with gear driving low pressure compressor and fan at common speed, and failsafe overspeed protection and shear section
|
FR3071546B1
(fr)
|
2017-09-25 |
2019-09-13 |
Safran Aircraft Engines |
Retention axiale de l'arbre de soufflante dans un moteur a turbine a gaz
|
US10724445B2
(en)
|
2018-01-03 |
2020-07-28 |
Raytheon Technologies Corporation |
Method of assembly for fan drive gear system with rotating carrier
|
CN111005937B
(zh)
*
|
2018-10-04 |
2021-11-19 |
三菱重工业株式会社 |
挤压油膜阻尼器以及旋转机械
|
US11092020B2
(en)
|
2018-10-18 |
2021-08-17 |
Raytheon Technologies Corporation |
Rotor assembly for gas turbine engines
|
US10808755B2
(en)
*
|
2019-03-04 |
2020-10-20 |
Pratt & Whitney Canada Corp. |
Method to seal damper cavity of multi-film oil damper
|
US11125110B2
(en)
*
|
2019-03-18 |
2021-09-21 |
Pratt & Whitney Canada Corp. |
Method and system to supply oil to a multi-film oil damper
|
US11067121B2
(en)
*
|
2019-03-18 |
2021-07-20 |
Pratt & Whitney Canada Corp. |
Multi-film oil damper with tapered damper rings
|
US10954817B2
(en)
*
|
2019-07-26 |
2021-03-23 |
Pratt & Whitney Canada Corp. |
Method of separating and sealing multi film damper rings
|
US10883383B1
(en)
*
|
2019-07-26 |
2021-01-05 |
Pratt & Whitney Canada Corp. |
Multi-film damper rings with spacers
|
US10947863B2
(en)
*
|
2019-07-26 |
2021-03-16 |
Pratt & Whitney Canada Corp. |
Method to supply oil to a multi-film damper
|
US11781506B2
(en)
|
2020-06-03 |
2023-10-10 |
Rtx Corporation |
Splitter and guide vane arrangement for gas turbine engines
|
US11441605B1
(en)
|
2021-03-01 |
2022-09-13 |
Pratt & Whitney Canada Corp. |
Dual-film damper
|
US11814968B2
(en)
|
2021-07-19 |
2023-11-14 |
Rtx Corporation |
Gas turbine engine with idle thrust ratio
|
US11754000B2
(en)
|
2021-07-19 |
2023-09-12 |
Rtx Corporation |
High and low spool configuration for a gas turbine engine
|
US11719245B2
(en)
|
2021-07-19 |
2023-08-08 |
Raytheon Technologies Corporation |
Compressor arrangement for a gas turbine engine
|
US12123356B2
(en)
|
2021-07-19 |
2024-10-22 |
Rtx Corporation |
Gas turbine engine with higher low spool torque-to-thrust ratio
|