US7578132B2
(en)
*
|
2001-03-03 |
2009-08-25 |
Rolls-Royce Plc |
Gas turbine engine exhaust nozzle
|
GB0105349D0
(en)
*
|
2001-03-03 |
2001-04-18 |
Rolls Royce Plc |
Gas turbine engine exhaust nozzle
|
WO2003018853A2
(en)
*
|
2001-08-24 |
2003-03-06 |
University Of Virginia Patent Foundation |
Reversible shape memory multifunctional structural designs and method of using and making the same
|
FR2829802B1
(fr)
*
|
2001-09-19 |
2004-05-28 |
Centre Nat Rech Scient |
Dispositif de controle de melange de jets propulsifs pour reacteur d'avion
|
BR0306781B1
(pt)
*
|
2002-01-09 |
2013-01-22 |
|
bocal de exaustço de turbofan e mÉtodo para reduzir ruÍdo em um motor turbofan possuindo um bocal de exaustço de turbofan.
|
US6543224B1
(en)
|
2002-01-29 |
2003-04-08 |
United Technologies Corporation |
System and method for controlling shape memory alloy actuators
|
US6718752B2
(en)
*
|
2002-05-29 |
2004-04-13 |
The Boeing Company |
Deployable segmented exhaust nozzle for a jet engine
|
US7055329B2
(en)
*
|
2003-03-31 |
2006-06-06 |
General Electric Company |
Method and apparatus for noise attenuation for gas turbine engines using at least one synthetic jet actuator for injecting air
|
GB0312505D0
(en)
*
|
2003-05-31 |
2003-07-09 |
Rolls Royce Plc |
Engine nozzle
|
US7458221B1
(en)
|
2003-10-23 |
2008-12-02 |
The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration |
Variable area nozzle including a plurality of convexly vanes with a crowned contour, in a vane to vane sealing arrangement and with nonuniform lengths
|
US7093423B2
(en)
*
|
2004-01-20 |
2006-08-22 |
General Electric Company |
Methods and apparatus for operating gas turbine engines
|
US7377109B2
(en)
*
|
2004-04-09 |
2008-05-27 |
The Boeing Company |
Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flows
|
US7377108B2
(en)
*
|
2004-04-09 |
2008-05-27 |
The Boeing Company |
Apparatus and method for reduction jet noise from single jets
|
US20050274103A1
(en)
*
|
2004-06-10 |
2005-12-15 |
United Technologies Corporation |
Gas turbine engine inlet with noise reduction features
|
US7174704B2
(en)
*
|
2004-07-23 |
2007-02-13 |
General Electric Company |
Split shroud exhaust nozzle
|
US7587899B2
(en)
|
2004-08-27 |
2009-09-15 |
University Of Houston |
Shape memory alloy actuated adaptive exhaust nozzle for jet engine
|
FR2875559B1
(fr)
*
|
2004-09-21 |
2007-02-23 |
Snecma Moteurs Sa |
Levier de commande du calage angulaire d'une aube de stator dans une turbomachine
|
US7546727B2
(en)
*
|
2004-11-12 |
2009-06-16 |
The Boeing Company |
Reduced noise jet engine
|
US7216831B2
(en)
*
|
2004-11-12 |
2007-05-15 |
The Boeing Company |
Shape changing structure
|
US7340883B2
(en)
*
|
2004-11-12 |
2008-03-11 |
The Boeing Company |
Morphing structure
|
US20060150612A1
(en)
*
|
2005-01-12 |
2006-07-13 |
Honeywell International Inc. |
Thrust vector control
|
US7367776B2
(en)
*
|
2005-01-26 |
2008-05-06 |
General Electric Company |
Turbine engine stator including shape memory alloy and clearance control method
|
EP1893847B1
(de)
*
|
2005-06-13 |
2017-03-29 |
GKN Aerospace Sweden AB |
Vorrichtung zum bewegen mindestens eines beweglichen elements in einer gasturbine
|
US20070241670A1
(en)
*
|
2006-04-17 |
2007-10-18 |
Battelle Memorial Institute |
Organic materials with phosphine sulfide moieties having tunable electric and electroluminescent properties
|
US7669785B2
(en)
|
2006-04-24 |
2010-03-02 |
The Boeing Company |
Integrated engine exhaust systems and methods for drag and thermal stress reduction
|
US8360361B2
(en)
|
2006-05-23 |
2013-01-29 |
University Of Virginia Patent Foundation |
Method and apparatus for jet blast deflection
|
US7721551B2
(en)
*
|
2006-06-29 |
2010-05-25 |
United Technologies Corporation |
Fan variable area nozzle for a gas turbine engine fan nacelle
|
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
|
FR2904372B1
(fr)
*
|
2006-07-26 |
2008-10-31 |
Snecma Sa |
Tuyere d'ejection des gaz pour turbomachine a double flux ayant une section d'ejection ou de col variable par deplacement du capot secondaire
|
US9976437B2
(en)
|
2006-08-15 |
2018-05-22 |
United Technologies Corporation |
Epicyclic gear train
|
US8858388B2
(en)
|
2006-08-15 |
2014-10-14 |
United Technologies Corporation |
Gas turbine engine gear train
|
US8753243B2
(en)
|
2006-08-15 |
2014-06-17 |
United Technologies Corporation |
Ring gear mounting arrangement with oil scavenge scheme
|
US10107231B2
(en)
|
2006-08-15 |
2018-10-23 |
United Technologies Corporation |
Gas turbine engine with geared architecture
|
US7762078B2
(en)
*
|
2006-09-13 |
2010-07-27 |
Aerojet-General Corporation |
Nozzle with temperature-responsive throat diameter
|
EP2066890B1
(de)
*
|
2006-10-12 |
2010-12-15 |
United Technologies Corporation |
Modulationsströmung durch turbomotorkühlsystem
|
WO2008045081A1
(en)
|
2006-10-12 |
2008-04-17 |
United Technologies Corporation |
Variable fan nozzle using shape memory material
|
EP2074307B1
(de)
*
|
2006-10-12 |
2011-01-26 |
United Technologies Corporation |
Translatorisch bewegbare innenhaube mit aerodynamischen klappenabschnitten
|
EP3141730A1
(de)
*
|
2006-10-12 |
2017-03-15 |
United Technologies Corporation |
Turbofantriebwerkbetriebssteuerung
|
WO2008045072A1
(en)
|
2006-10-12 |
2008-04-17 |
United Technologies Corporation |
Dual function cascade integrated variable area fan nozzle and thrust reverser
|
EP2074298B1
(de)
*
|
2006-10-12 |
2013-03-13 |
United Technologies Corporation |
Durch eine düse mit variablem querschnitt unterstützter neustart einens turbinentriebwerks
|
EP2074321B1
(de)
|
2006-10-12 |
2012-12-05 |
United Technologies Corporation |
Mantelstromdüse mit variablem austrittsquerschnitt mit adaptiver struktur sowie verfahren zur veränderung des austrittquerschnitts der gebläsedüse einer gasturbine
|
US7254997B1
(en)
*
|
2006-10-12 |
2007-08-14 |
David Hui |
Anti-steal tire pressure monitoring apparatus
|
US7721549B2
(en)
*
|
2007-02-08 |
2010-05-25 |
United Technologies Corporation |
Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system
|
US20080273961A1
(en)
|
2007-03-05 |
2008-11-06 |
Rosenkrans William E |
Flutter sensing and control system for a gas turbine engine
|
US7883049B2
(en)
*
|
2007-04-27 |
2011-02-08 |
The Boeing Company |
Jet nozzle having noise attenuating shield and method therefor
|
US7966827B2
(en)
*
|
2007-05-31 |
2011-06-28 |
United Technologies Corporation |
Gas turbine engine with fan variable area nozzle having a rotational valve system
|
US8299411B2
(en)
*
|
2007-06-01 |
2012-10-30 |
Her Majesty In Right Of Canada As Represented By The Minister Of National Defence |
Control surface actuation system
|
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
|
US20150377123A1
(en)
|
2007-08-01 |
2015-12-31 |
United Technologies Corporation |
Turbine section of high bypass turbofan
|
US8844265B2
(en)
|
2007-08-01 |
2014-09-30 |
United Technologies Corporation |
Turbine section of high bypass turbofan
|
US11242805B2
(en)
|
2007-08-01 |
2022-02-08 |
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
|
CN101939528B
(zh)
*
|
2007-08-08 |
2013-07-24 |
罗尔股份有限公司 |
具有旁通流的面积可调风扇喷嘴
|
US9759087B2
(en)
|
2007-08-08 |
2017-09-12 |
Rohr, Inc. |
Translating variable area fan nozzle providing an upstream bypass flow exit
|
US9494084B2
(en)
|
2007-08-23 |
2016-11-15 |
United Technologies Corporation |
Gas turbine engine with fan variable area nozzle for low fan pressure ratio
|
US10167813B2
(en)
|
2007-08-23 |
2019-01-01 |
United Technologies Corporation |
Gas turbine engine with fan variable area nozzle to reduce fan instability
|
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
|
US8197209B2
(en)
*
|
2007-12-19 |
2012-06-12 |
United Technologies Corp. |
Systems and methods involving variable throat area vanes
|
FR2926603B1
(fr)
*
|
2008-01-23 |
2010-03-26 |
Snecma |
Guidage d'un arbre dans une turbomachine
|
WO2009114357A2
(en)
*
|
2008-03-07 |
2009-09-17 |
Gm Global Technology Operations, Inc. |
Shape memory alloy cables
|
US8141366B2
(en)
*
|
2008-08-19 |
2012-03-27 |
United Technologies Corporation |
Gas turbine engine with variable area fan nozzle
|
US9267463B2
(en)
*
|
2008-03-25 |
2016-02-23 |
United Technologies Corp. |
Gas turbine engine systems involving variable nozzles with flexible panels
|
US8356483B2
(en)
*
|
2008-04-10 |
2013-01-22 |
United Technologies Corp |
Gas turbine engine systems involving variable nozzles with sliding doors
|
GB0807593D0
(en)
*
|
2008-04-28 |
2008-06-04 |
Rolls Royce Plc |
A composite article comprising a shape memory material member
|
US20140174056A1
(en)
|
2008-06-02 |
2014-06-26 |
United Technologies Corporation |
Gas turbine engine with low stage count low pressure turbine
|
US8973364B2
(en)
|
2008-06-26 |
2015-03-10 |
United Technologies Corporation |
Gas turbine engine with noise attenuating variable area fan nozzle
|
US7716932B2
(en)
*
|
2008-07-24 |
2010-05-18 |
Spirit Aerosystems, Inc. |
Dilating fan duct nozzle
|
DE102008063823B4
(de)
*
|
2008-12-19 |
2014-05-15 |
Deutsches Zentrum für Luft- und Raumfahrt e.V. |
Flugzeug
|
US8459036B2
(en)
|
2008-12-26 |
2013-06-11 |
Rolls-Royce Corporation |
Aircraft nozzle having actuators capable of changing a flow area of the aircraft nozzle
|
GB2468346B
(en)
*
|
2009-03-06 |
2011-06-22 |
Rolls Royce Plc |
Cooling system for an aero gas turbine engine
|
US9885313B2
(en)
|
2009-03-17 |
2018-02-06 |
United Technologes Corporation |
Gas turbine engine bifurcation located fan variable area nozzle
|
GB0907513D0
(en)
|
2009-05-01 |
2009-06-10 |
Rolls Royce Plc |
A flow modulating device
|
US8434293B2
(en)
*
|
2009-08-06 |
2013-05-07 |
The Boeing Company |
High stiffness shape memory alloy actuated aerostructure
|
US8443586B2
(en)
*
|
2009-11-24 |
2013-05-21 |
United Technologies Corporation |
Variable area fan nozzle bearing track
|
US20110120078A1
(en)
*
|
2009-11-24 |
2011-05-26 |
Schwark Jr Fred W |
Variable area fan nozzle track
|
US20110120079A1
(en)
*
|
2009-11-24 |
2011-05-26 |
Schwark Jr Fred W |
Variable area fan nozzle stiffeners and placement
|
US8123150B2
(en)
|
2010-03-30 |
2012-02-28 |
General Electric Company |
Variable area fuel nozzle
|
FR2960600B1
(fr)
*
|
2010-06-01 |
2013-10-25 |
Aircelle Sa |
Systeme d'actionnement d'un dispositif d'inversion de poussee
|
US9995174B2
(en)
|
2010-10-12 |
2018-06-12 |
United Technologies Corporation |
Planetary gear system arrangement with auxiliary oil system
|
US8549834B2
(en)
|
2010-10-21 |
2013-10-08 |
United Technologies Corporation |
Gas turbine engine with variable area fan nozzle
|
US9416751B2
(en)
|
2010-12-07 |
2016-08-16 |
Hamilton Sundstrand Corporation |
Actuation system
|
US10605167B2
(en)
|
2011-04-15 |
2020-03-31 |
United Technologies Corporation |
Gas turbine engine front center body architecture
|
CH704995A1
(de)
*
|
2011-05-24 |
2012-11-30 |
Alstom Technology Ltd |
Turbomaschine.
|
US9410608B2
(en)
|
2011-06-08 |
2016-08-09 |
United Technologies Corporation |
Flexible support structure for a geared architecture gas turbine engine
|
US9631558B2
(en)
|
2012-01-03 |
2017-04-25 |
United Technologies Corporation |
Geared architecture for high speed and small volume fan drive turbine
|
US9239012B2
(en)
|
2011-06-08 |
2016-01-19 |
United Technologies Corporation |
Flexible support structure for a geared architecture gas turbine engine
|
US8613398B2
(en)
|
2011-06-17 |
2013-12-24 |
General Electric Company |
Apparatus and methods for linear actuation of flow altering components of jet engine nozzle
|
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
|
US9938898B2
(en)
|
2011-07-29 |
2018-04-10 |
United Technologies Corporation |
Geared turbofan bearing arrangement
|
US9334802B2
(en)
|
2011-10-31 |
2016-05-10 |
United Technologies Corporation |
Gas turbine engine thermal management system
|
US8567745B2
(en)
|
2011-12-15 |
2013-10-29 |
United Technologies Corporation |
Apparatuses and systems with vertically and longitudinally offset mounting flanges
|
US9416677B2
(en)
|
2012-01-10 |
2016-08-16 |
United Technologies Corporation |
Gas turbine engine forward bearing compartment architecture
|
US9004849B2
(en)
|
2012-01-10 |
2015-04-14 |
United Technologies Corporation |
Gas turbine engine forward bearing compartment architecture
|
US10125724B2
(en)
|
2012-01-17 |
2018-11-13 |
United Technologies Corporation |
Start system for gas turbine engines
|
US20130186058A1
(en)
|
2012-01-24 |
2013-07-25 |
William G. Sheridan |
Geared turbomachine fan and compressor rotation
|
US9447694B2
(en)
|
2012-01-30 |
2016-09-20 |
United Technologies Corporation |
Internal manifold for turning mid-turbine frame flow distribution
|
US20130192240A1
(en)
|
2012-01-31 |
2013-08-01 |
Peter M. Munsell |
Buffer system for a gas turbine engine
|
US10400629B2
(en)
|
2012-01-31 |
2019-09-03 |
United Technologies Corporation |
Gas turbine engine shaft bearing configuration
|
US10415468B2
(en)
|
2012-01-31 |
2019-09-17 |
United Technologies Corporation |
Gas turbine engine buffer system
|
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
|
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
|
US9845726B2
(en)
|
2012-01-31 |
2017-12-19 |
United Technologies Corporation |
Gas turbine engine with high speed low pressure turbine section
|
US8869508B2
(en)
|
2012-01-31 |
2014-10-28 |
United Technologies Corporation |
Gas turbine engine variable area fan nozzle control
|
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
|
US8375699B1
(en)
|
2012-01-31 |
2013-02-19 |
United Technologies Corporation |
Variable area fan nozzle with wall thickness distribution
|
US10240526B2
(en)
|
2012-01-31 |
2019-03-26 |
United Technologies Corporation |
Gas turbine engine with high speed low pressure turbine section
|
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
|
US9169781B2
(en)
|
2012-01-31 |
2015-10-27 |
United Technologies Corporation |
Turbine engine gearbox
|
US8863491B2
(en)
|
2012-01-31 |
2014-10-21 |
United Technologies Corporation |
Gas turbine engine shaft bearing configuration
|
US20130192195A1
(en)
|
2012-01-31 |
2013-08-01 |
Eric J. Wehmeier |
Gas turbine engine with compressor inlet guide vane positioned for starting
|
US20150345426A1
(en)
|
2012-01-31 |
2015-12-03 |
United Technologies Corporation |
Geared turbofan gas turbine engine architecture
|
US9593628B2
(en)
|
2012-01-31 |
2017-03-14 |
United Technologies Corporation |
Gas turbine engine variable area fan nozzle with ice management
|
US10502135B2
(en)
|
2012-01-31 |
2019-12-10 |
United Technologies Corporation |
Buffer system for communicating one or more buffer supply airs throughout a gas turbine engine
|
US20150192070A1
(en)
|
2012-01-31 |
2015-07-09 |
United Technologies Corporation |
Geared turbofan gas turbine engine architecture
|
US9394852B2
(en)
|
2012-01-31 |
2016-07-19 |
United Technologies Corporation |
Variable area fan nozzle with wall thickness distribution
|
US10113434B2
(en)
|
2012-01-31 |
2018-10-30 |
United Technologies Corporation |
Turbine blade damper seal
|
US20130192198A1
(en)
|
2012-01-31 |
2013-08-01 |
Lisa I. Brilliant |
Compressor flowpath
|
US9835052B2
(en)
|
2012-01-31 |
2017-12-05 |
United Technologies Corporation |
Gas turbine engine with high speed low pressure turbine section and bearing support features
|
US8402741B1
(en)
|
2012-01-31 |
2013-03-26 |
United Technologies Corporation |
Gas turbine engine shaft bearing configuration
|
US9611859B2
(en)
|
2012-01-31 |
2017-04-04 |
United Technologies Corporation |
Gas turbine engine with high speed low pressure turbine section and bearing support features
|
US8366382B1
(en)
|
2012-01-31 |
2013-02-05 |
United Technologies Corporation |
Mid-turbine frame buffer system
|
US8935913B2
(en)
|
2012-01-31 |
2015-01-20 |
United Technologies Corporation |
Geared turbofan gas turbine engine architecture
|
US9121282B2
(en)
|
2012-02-02 |
2015-09-01 |
Honeywell International Inc. |
Methods for the controlled reduction of turbine nozzle flow areas and turbine nozzle components having reduced flow areas
|
US9297270B2
(en)
|
2012-02-29 |
2016-03-29 |
United Technologies Corporation |
Gas turbine engine driving multiple fans
|
US10107191B2
(en)
|
2012-02-29 |
2018-10-23 |
United Technologies Corporation |
Geared gas turbine engine with reduced fan noise
|
US10309232B2
(en)
|
2012-02-29 |
2019-06-04 |
United Technologies Corporation |
Gas turbine engine with stage dependent material selection for blades and disk
|
US8790075B2
(en)
|
2012-03-30 |
2014-07-29 |
United Technologies Corporation |
Gas turbine engine geared architecture axial retention arrangement
|
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
|
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
|
US20150308351A1
(en)
|
2012-05-31 |
2015-10-29 |
United Technologies Corporation |
Fundamental gear system architecture
|
US9476323B2
(en)
|
2012-05-31 |
2016-10-25 |
United Technologies Corporation |
Turbine gear assembly support having symmetrical removal features
|
US9328818B2
(en)
|
2012-09-21 |
2016-05-03 |
United Technologies Corporation |
Gear carrier flex mount lubrication
|
US8753065B2
(en)
|
2012-09-27 |
2014-06-17 |
United Technologies Corporation |
Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
|
WO2014051672A1
(en)
|
2012-09-28 |
2014-04-03 |
United Technologies Corporation |
Split-zone flow metering t-tube
|
US9624834B2
(en)
|
2012-09-28 |
2017-04-18 |
United Technologies Corporation |
Low noise compressor rotor for geared turbofan engine
|
US20160138474A1
(en)
|
2012-09-28 |
2016-05-19 |
United Technologies Corporation |
Low noise compressor rotor for geared turbofan engine
|
EP2904233A4
(de)
|
2012-10-01 |
2016-06-29 |
United Technologies Corp |
Gasturbinenmotor mit grossem leichtgewichtigen lüfter
|
US10036316B2
(en)
|
2012-10-02 |
2018-07-31 |
United Technologies Corporation |
Geared turbofan engine with high compressor exit temperature
|
US10100745B2
(en)
|
2012-10-08 |
2018-10-16 |
United Technologies Corporation |
Geared turbine engine with relatively lightweight propulsor module
|
US11280271B2
(en)
|
2012-10-09 |
2022-03-22 |
Raytheon Technologies Corporation |
Operability geared turbofan engine including compressor section variable guide vanes
|
US9989009B2
(en)
|
2012-10-31 |
2018-06-05 |
The Boeing Company |
Methods and apparatus for sealing variable area fan nozzles of jet engines
|
US9261101B2
(en)
*
|
2012-10-31 |
2016-02-16 |
Hamilton Sundstrand Corporation |
Fan housing for ram air fan
|
GB201220378D0
(en)
*
|
2012-11-13 |
2012-12-26 |
Rolls Royce Plc |
A gas turbine engine exhaust nozzle
|
US20140165575A1
(en)
*
|
2012-12-13 |
2014-06-19 |
United Technologies Corporation |
Nozzle section for a gas turbine engine
|
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
|
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
|
US10436120B2
(en)
|
2013-02-06 |
2019-10-08 |
United Technologies Corporation |
Exhaust nozzle for an elongated gear turbofan with high bypass ratio
|
EP2971698B1
(de)
|
2013-03-12 |
2021-04-21 |
Raytheon Technologies Corporation |
Flexible kupplung für einen turbinenmotor mit einem getriebe
|
US10605172B2
(en)
|
2013-03-14 |
2020-03-31 |
United Technologies Corporation |
Low noise turbine for geared gas turbine engine
|
US11719161B2
(en)
|
2013-03-14 |
2023-08-08 |
Raytheon Technologies Corporation |
Low noise turbine for geared gas turbine engine
|
US10724479B2
(en)
|
2013-03-15 |
2020-07-28 |
United Technologies Corporation |
Thrust efficient turbofan engine
|
WO2014151673A1
(en)
|
2013-03-15 |
2014-09-25 |
United Technologies Corporation |
Aerodynamic track fairing for a gas turbine engine fan nacelle
|
WO2014151785A1
(en)
|
2013-03-15 |
2014-09-25 |
United Technologies Corporation |
Turbofan engine bearing and gearbox arrangement
|
US10287917B2
(en)
|
2013-05-09 |
2019-05-14 |
United Technologies Corporation |
Turbofan engine front section
|
EP3008323B1
(de)
|
2013-05-09 |
2021-11-10 |
Raytheon Technologies Corporation |
Stirnteil für turbofantriebwerk
|
US9581145B2
(en)
*
|
2013-05-14 |
2017-02-28 |
The Boeing Company |
Shape memory alloy actuation system for variable area fan nozzle
|
WO2015047515A2
(en)
|
2013-07-07 |
2015-04-02 |
United Technologies Corporation |
Fan drive gear system manifold radial tube filters
|
US20150300264A1
(en)
|
2013-09-30 |
2015-10-22 |
United Technologies Corporation |
Geared turbofan architecture for regional jet aircraft
|
EP3058202A4
(de)
|
2013-10-16 |
2017-06-28 |
United Technologies Corporation |
Turbogebläsemotor mit gezielter modularer wirkung
|
US9488130B2
(en)
|
2013-10-17 |
2016-11-08 |
Honeywell International Inc. |
Variable area fan nozzle systems with improved drive couplings
|
US10502163B2
(en)
|
2013-11-01 |
2019-12-10 |
United Technologies Corporation |
Geared turbofan arrangement with core split power ratio
|
EP3063385A4
(de)
|
2013-11-01 |
2017-07-12 |
United Technologies Corporation |
Getriebeturbolüfteranordnung mit geteilter kernleistung
|
US8869504B1
(en)
|
2013-11-22 |
2014-10-28 |
United Technologies Corporation |
Geared turbofan engine gearbox arrangement
|
US9739205B2
(en)
|
2013-12-23 |
2017-08-22 |
United Technologies Corporation |
Geared turbofan with a gearbox upstream of a fan drive turbine
|
EP3097291B1
(de)
|
2014-01-20 |
2019-10-23 |
United Technologies Corporation |
Getriebefan-triebwerk mit reduzierter öltankgrösse
|
US9140127B2
(en)
|
2014-02-19 |
2015-09-22 |
United Technologies Corporation |
Gas turbine engine airfoil
|
EP3108113A4
(de)
|
2014-02-19 |
2017-03-15 |
United Technologies Corporation |
Gasturbinenmotor-tragfläche
|
US10393139B2
(en)
|
2014-02-19 |
2019-08-27 |
United Technologies Corporation |
Gas turbine engine airfoil
|
US10584715B2
(en)
|
2014-02-19 |
2020-03-10 |
United Technologies Corporation |
Gas turbine engine airfoil
|
WO2015126449A1
(en)
|
2014-02-19 |
2015-08-27 |
United Technologies Corporation |
Gas turbine engine airfoil
|
WO2015126451A1
(en)
|
2014-02-19 |
2015-08-27 |
United Technologies Corporation |
Gas turbine engine airfoil
|
US10385866B2
(en)
|
2014-02-19 |
2019-08-20 |
United Technologies Corporation |
Gas turbine engine airfoil
|
WO2015175058A2
(en)
|
2014-02-19 |
2015-11-19 |
United Technologies Corporation |
Gas turbine engine airfoil
|
WO2015175043A2
(en)
|
2014-02-19 |
2015-11-19 |
United Technologies Corporation |
Gas turbine engine airfoil
|
WO2015175051A2
(en)
|
2014-02-19 |
2015-11-19 |
United Technologies Corporation |
Gas turbine engine airfoil
|
EP3108118B1
(de)
|
2014-02-19 |
2019-09-18 |
United Technologies Corporation |
Gasturbinenmotor-tragfläche
|
EP3108116B1
(de)
|
2014-02-19 |
2024-01-17 |
RTX Corporation |
Gasturbinenmotor
|
WO2015126454A1
(en)
|
2014-02-19 |
2015-08-27 |
United Technologies Corporation |
Gas turbine engine airfoil
|
EP3108123B1
(de)
|
2014-02-19 |
2023-10-04 |
Raytheon Technologies Corporation |
Turboluftstrahltriebwerk mit getriebefan und niederdruckverdichterschaufeln
|
WO2015126824A1
(en)
|
2014-02-19 |
2015-08-27 |
United Technologies Corporation |
Gas turbine engine airfoil
|
WO2015175052A2
(en)
|
2014-02-19 |
2015-11-19 |
United Technologies Corporation |
Gas turbine engine airfoil
|
WO2015175045A2
(en)
|
2014-02-19 |
2015-11-19 |
United Technologies Corporation |
Gas turbine engine airfoil
|
EP3108122B1
(de)
|
2014-02-19 |
2023-09-20 |
Raytheon Technologies Corporation |
Turboluftstrahltriebwerk mit getriebefan und niederdruckverdichterschaufeln
|
US9163517B2
(en)
|
2014-02-19 |
2015-10-20 |
United Technologies Corporation |
Gas turbine engine airfoil
|
EP3108105B1
(de)
|
2014-02-19 |
2021-05-12 |
Raytheon Technologies Corporation |
Gasturbinenmotor-tragfläche
|
US9567858B2
(en)
|
2014-02-19 |
2017-02-14 |
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
|
US9879608B2
(en)
|
2014-03-17 |
2018-01-30 |
United Technologies Corporation |
Oil loss protection for a fan drive gear system
|
US9828943B2
(en)
|
2014-06-09 |
2017-11-28 |
United Technologies Corporation |
Variable area nozzle for gas turbine engine
|
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
|
US9333603B1
(en)
|
2015-01-28 |
2016-05-10 |
United Technologies Corporation |
Method of assembling gas turbine engine section
|
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
|
US9874145B2
(en)
|
2015-04-27 |
2018-01-23 |
United Technologies Corporation |
Lubrication system for gas turbine engines
|
US10458270B2
(en)
|
2015-06-23 |
2019-10-29 |
United Technologies Corporation |
Roller bearings for high ratio geared turbofan engine
|
US10267233B2
(en)
|
2015-10-23 |
2019-04-23 |
United Technologies Corporation |
Method and apparatus for monitoring lubrication pump operation during windmilling
|
US10233773B2
(en)
|
2015-11-17 |
2019-03-19 |
United Technologies Corporation |
Monitoring system for non-ferrous metal particles
|
US10508562B2
(en)
|
2015-12-01 |
2019-12-17 |
United Technologies Corporation |
Geared turbofan with four star/planetary gear reduction
|
GB201609071D0
(en)
|
2016-05-24 |
2016-07-06 |
Rolls Royce Plc |
Aircraft gas turbine engine nacelle
|
US11421551B2
(en)
|
2016-05-25 |
2022-08-23 |
General Electric Company |
Turbine bearing support
|
US10197102B2
(en)
|
2016-10-21 |
2019-02-05 |
General Electric Company |
Load reduction assemblies for a gas turbine engine
|
US10669948B2
(en)
|
2017-01-03 |
2020-06-02 |
Raytheon Technologies Corporation |
Geared turbofan with non-epicyclic gear reduction system
|
CA3000360C
(en)
|
2017-04-14 |
2020-05-26 |
General Electric Company |
Support assembly having variable stiffness member
|
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
|
US10724445B2
(en)
|
2018-01-03 |
2020-07-28 |
Raytheon Technologies Corporation |
Method of assembly for fan drive gear system with rotating carrier
|
US20190293020A1
(en)
*
|
2018-03-21 |
2019-09-26 |
Spirit Aerosystems, Inc. |
Flexible sleeve for adjustable fan duct nozzle
|
GB201811861D0
(en)
*
|
2018-07-20 |
2018-09-05 |
Rolls Royce Plc |
Supersonic aircraft turbofan engine
|
US11092020B2
(en)
|
2018-10-18 |
2021-08-17 |
Raytheon Technologies Corporation |
Rotor assembly for gas turbine engines
|
US11440671B2
(en)
*
|
2019-01-24 |
2022-09-13 |
Amazon Technologies, Inc. |
Adjustable motor fairings for aerial vehicles
|
US11420755B2
(en)
|
2019-08-08 |
2022-08-23 |
General Electric Company |
Shape memory alloy isolator for a gas turbine engine
|
US11021998B2
(en)
|
2019-08-08 |
2021-06-01 |
General Electric Company |
Shape memory alloy sleeve support assembly for a bearing
|
US11105223B2
(en)
|
2019-08-08 |
2021-08-31 |
General Electric Company |
Shape memory alloy reinforced casing
|
FR3102144B1
(fr)
*
|
2019-10-16 |
2021-10-01 |
Safran |
Système propulsif pour un aéronef
|
US11280219B2
(en)
|
2019-11-27 |
2022-03-22 |
General Electric Company |
Rotor support structures for rotating drum rotors of gas turbine engines
|
US11274557B2
(en)
|
2019-11-27 |
2022-03-15 |
General Electric Company |
Damper assemblies for rotating drum rotors of gas turbine engines
|
US11781506B2
(en)
|
2020-06-03 |
2023-10-10 |
Rtx Corporation |
Splitter and guide vane arrangement for gas turbine engines
|
US11828235B2
(en)
|
2020-12-08 |
2023-11-28 |
General Electric Company |
Gearbox for a gas turbine engine utilizing shape memory alloy dampers
|
US11719245B2
(en)
|
2021-07-19 |
2023-08-08 |
Raytheon Technologies Corporation |
Compressor arrangement for a gas turbine engine
|
US11754000B2
(en)
|
2021-07-19 |
2023-09-12 |
Rtx Corporation |
High and low spool configuration for a gas turbine engine
|
US11814968B2
(en)
|
2021-07-19 |
2023-11-14 |
Rtx Corporation |
Gas turbine engine with idle thrust ratio
|
CN114165355B
(zh)
*
|
2021-10-20 |
2024-01-09 |
中国航发四川燃气涡轮研究院 |
基于形状记忆合金的智能尾喷管结构及排气系统
|
US20230340927A1
(en)
*
|
2022-04-26 |
2023-10-26 |
General Electric Company |
Reverse thrust turbofan engine
|