EP0784564B1
(de)
*
|
1994-10-18 |
1998-12-30 |
United Technologies Corporation |
Gondel und ihre halterungsvorrichtung auf einem flugzeug
|
GB9921935D0
(en)
|
1999-09-17 |
1999-11-17 |
Rolls Royce |
A nacelle assembly for a gas turbine engine
|
US6220546B1
(en)
|
1999-12-29 |
2001-04-24 |
The Boeing Company |
Aircraft engine and associated aircraft engine cowl
|
GB2359052B
(en)
*
|
2000-02-09 |
2003-09-17 |
Rolls Royce Plc |
Engine arrangement
|
JP4426467B2
(ja)
*
|
2003-04-28 |
2010-03-03 |
スネクマ |
ターボプロップエンジンの空気取入口装置
|
GB0312490D0
(en)
*
|
2003-06-02 |
2003-07-09 |
Rolls Royce Plc |
Aeroengine nacelle
|
US7090165B2
(en)
*
|
2003-06-02 |
2006-08-15 |
Rolls-Royce Plc |
Aeroengine nacelle
|
GB0315431D0
(en)
*
|
2003-07-02 |
2003-08-06 |
Rolls Royce Plc |
Aircraft configuration
|
US7607286B2
(en)
*
|
2004-12-01 |
2009-10-27 |
United Technologies Corporation |
Regenerative turbine blade and vane cooling for a tip turbine engine
|
EP1828567B1
(de)
|
2004-12-01 |
2011-10-12 |
United Technologies Corporation |
Diffusor-ansaugung für einen spitzenturbinenmotor
|
WO2006060006A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine non-metallic tailcone
|
US8096753B2
(en)
*
|
2004-12-01 |
2012-01-17 |
United Technologies Corporation |
Tip turbine engine and operating method with reverse core airflow
|
WO2006060003A2
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
|
WO2006060001A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Fan rotor assembly for a tip turbine engine
|
US7976273B2
(en)
*
|
2004-12-01 |
2011-07-12 |
United Technologies Corporation |
Tip turbine engine support structure
|
US20090169385A1
(en)
*
|
2004-12-01 |
2009-07-02 |
Suciu Gabriel L |
Fan-turbine rotor assembly with integral inducer section for a tip turbine engine
|
US7854112B2
(en)
*
|
2004-12-01 |
2010-12-21 |
United Technologies Corporation |
Vectoring transition duct for turbine engine
|
US7934902B2
(en)
*
|
2004-12-01 |
2011-05-03 |
United Technologies Corporation |
Compressor variable stage remote actuation for turbine engine
|
WO2006060013A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Seal assembly for a fan rotor of a tip turbine engine
|
US20080219833A1
(en)
*
|
2004-12-01 |
2008-09-11 |
United Technologies Corporation |
Inducer for a Fan Blade of a Tip Turbine Engine
|
US7882694B2
(en)
|
2004-12-01 |
2011-02-08 |
United Technologies Corporation |
Variable fan inlet guide vane assembly for gas turbine engine
|
US8365511B2
(en)
*
|
2004-12-01 |
2013-02-05 |
United Technologies Corporation |
Tip turbine engine integral case, vane, mount and mixer
|
DE602004027766D1
(de)
*
|
2004-12-01 |
2010-07-29 |
United Technologies Corp |
Hydraulische dichtung für ein getriebe eines spitzenturbinenmotors
|
WO2006059997A2
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Annular turbine ring rotor
|
US8087885B2
(en)
*
|
2004-12-01 |
2012-01-03 |
United Technologies Corporation |
Stacked annular components for turbine engines
|
WO2006059970A2
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Turbine engine with differential gear driven fan and compressor
|
WO2006112807A2
(en)
|
2004-12-01 |
2006-10-26 |
United Technologies Corporation |
Turbine engine and method for starting a turbine engine
|
WO2006059985A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Axial compressor for tip turbine engine
|
EP1828591B1
(de)
*
|
2004-12-01 |
2010-07-21 |
United Technologies Corporation |
Umfangsbrennkammer für spitzenturbinenmotor
|
US20090148273A1
(en)
*
|
2004-12-01 |
2009-06-11 |
Suciu Gabriel L |
Compressor inlet guide vane for tip turbine engine and corresponding control method
|
EP1831519B1
(de)
*
|
2004-12-01 |
2010-08-04 |
United Technologies Corporation |
Tip-Turbinentriebwerk mit mehreren Gebläse- und Turbinenstufen
|
EP1828547B1
(de)
|
2004-12-01 |
2011-11-30 |
United Technologies Corporation |
Turbofantriebwerk mit einer Mehrzahl von einzeln steuerbaren Einlassleitschaufeln und zugehöriges Steuerverfahren
|
US8083030B2
(en)
*
|
2004-12-01 |
2011-12-27 |
United Technologies Corporation |
Gearbox lubrication supply system for a tip engine
|
WO2006059988A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Modular tip turbine engine
|
US7959406B2
(en)
*
|
2004-12-01 |
2011-06-14 |
United Technologies Corporation |
Close coupled gearbox assembly for a tip turbine engine
|
US9003759B2
(en)
|
2004-12-01 |
2015-04-14 |
United Technologies Corporation |
Particle separator for tip turbine engine
|
US8061968B2
(en)
*
|
2004-12-01 |
2011-11-22 |
United Technologies Corporation |
Counter-rotating compressor case and assembly method for tip turbine engine
|
US7874802B2
(en)
*
|
2004-12-01 |
2011-01-25 |
United Technologies Corporation |
Tip turbine engine comprising turbine blade clusters and method of assembly
|
EP1831520B1
(de)
*
|
2004-12-01 |
2009-02-25 |
United Technologies Corporation |
Tip-turbinentriebwerk und entsprechendes betriebsverfahren
|
EP1825112B1
(de)
*
|
2004-12-01 |
2013-10-23 |
United Technologies Corporation |
Freigetragene tipturbinentriebwerk
|
WO2006059971A2
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine integral fan, combustor, and turbine case
|
EP1825177B1
(de)
|
2004-12-01 |
2012-01-25 |
United Technologies Corporation |
Aufblasbares ablassventil für eine turbomaschine und verfahren zur steuerung von ablassluft
|
WO2006060009A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Turbine blade engine comprising turbine clusters and radial attachment lock arrangement therefor
|
US8807936B2
(en)
*
|
2004-12-01 |
2014-08-19 |
United Technologies Corporation |
Balanced turbine rotor fan blade for a tip turbine engine
|
EP1825113B1
(de)
|
2004-12-01 |
2012-10-24 |
United Technologies Corporation |
Gegenläufiges getriebe für ein tip-turbinen-triebwerk
|
WO2006059994A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Seal assembly for a fan-turbine rotor of a tip turbine engine
|
US7980054B2
(en)
*
|
2004-12-01 |
2011-07-19 |
United Technologies Corporation |
Ejector cooling of outer case for tip turbine engine
|
WO2006060011A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine comprising a nonrotable compartment
|
US7631485B2
(en)
|
2004-12-01 |
2009-12-15 |
United Technologies Corporation |
Tip turbine engine with a heat exchanger
|
EP1841960B1
(de)
*
|
2004-12-01 |
2011-05-25 |
United Technologies Corporation |
Starter-generatorsystem für einen spitzenturbinenmotor
|
EP1828683B1
(de)
|
2004-12-01 |
2013-04-10 |
United Technologies Corporation |
Brennkammer für turbinenmotor
|
US9109537B2
(en)
*
|
2004-12-04 |
2015-08-18 |
United Technologies Corporation |
Tip turbine single plane mount
|
US20060145001A1
(en)
*
|
2004-12-30 |
2006-07-06 |
Smith Matthew C |
Fan cowl door elimination
|
FR2885877B1
(fr)
*
|
2005-05-23 |
2008-12-12 |
Airbus France Sas |
Mat d'accrochage de turboreacteur pour aeronef
|
FR2885878B1
(fr)
*
|
2005-05-23 |
2007-06-29 |
Airbus France Sas |
Ensemble moteur pour aeronef
|
FR2887521B1
(fr)
*
|
2005-06-28 |
2007-08-17 |
Airbus France Sas |
Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un dispositif d'accrochage d'un tel moteur
|
GB0516066D0
(en)
*
|
2005-08-04 |
2005-09-14 |
Airbus Uk Ltd |
Removal of components from aircraft
|
FR2891254B1
(fr)
*
|
2005-09-29 |
2007-10-26 |
Airbus France Sas |
Ensemble moteur pour aeronef
|
FR2900907B1
(fr)
*
|
2006-05-09 |
2008-12-19 |
Airbus France Sas |
Ensemble moteur pour aeronef a nacelle et mat integres
|
US7721525B2
(en)
*
|
2006-07-19 |
2010-05-25 |
Rohr, Inc. |
Aircraft engine inlet having zone of deformation
|
FR2905990A1
(fr)
*
|
2006-09-20 |
2008-03-21 |
Snecma Sa |
Systeme propulsif a pylone integre pour avion.
|
WO2008043903A2
(fr)
*
|
2006-10-11 |
2008-04-17 |
Aircelle |
Nacelle pour turboréacteur double flux
|
FR2913664B1
(fr)
*
|
2007-03-16 |
2009-07-24 |
Aircelle Sa |
Nacelle pour turboreacteur double flux
|
FR2907098B1
(fr)
*
|
2006-10-11 |
2010-04-16 |
Aircelle Sa |
Nacelle pour turboreacteur double flux
|
US8967945B2
(en)
|
2007-05-22 |
2015-03-03 |
United Technologies Corporation |
Individual inlet guide vane control for tip turbine engine
|
FR2917710A1
(fr)
*
|
2007-06-22 |
2008-12-26 |
Aircelle Sa |
Platine de fixation et longeron de manutention d'ensemble propulsif monobloc d'un aeronef
|
US11149650B2
(en)
|
2007-08-01 |
2021-10-19 |
Raytheon Technologies Corporation |
Turbine section of high bypass turbofan
|
US8256707B2
(en)
*
|
2007-08-01 |
2012-09-04 |
United Technologies Corporation |
Engine mounting configuration for a turbofan gas turbine engine
|
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
|
US20150377123A1
(en)
|
2007-08-01 |
2015-12-31 |
United 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
|
US11486311B2
(en)
|
2007-08-01 |
2022-11-01 |
Raytheon Technologies Corporation |
Turbine section of high bypass turbofan
|
FR2926285B1
(fr)
*
|
2008-01-15 |
2009-12-11 |
Aircelle Sa |
Nacelle a capotage simplifie
|
US8118251B2
(en)
*
|
2008-01-18 |
2012-02-21 |
United Technologies Corporation |
Mounting system for a gas turbine engine
|
FR2928347B1
(fr)
*
|
2008-03-07 |
2010-06-25 |
Aircelle Sa |
Structure d'accrochage pour turboreacteur
|
US8167237B2
(en)
*
|
2008-03-21 |
2012-05-01 |
United Technologies Corporation |
Mounting system for a gas turbine engine
|
US8800914B2
(en)
|
2008-06-02 |
2014-08-12 |
United Technologies Corporation |
Gas turbine engine with low stage count low pressure turbine
|
US8511605B2
(en)
|
2008-06-02 |
2013-08-20 |
United Technologies Corporation |
Gas turbine engine with low stage count low pressure turbine
|
US20140174056A1
(en)
|
2008-06-02 |
2014-06-26 |
United Technologies Corporation |
Gas turbine engine with low stage count low pressure turbine
|
US8807477B2
(en)
|
2008-06-02 |
2014-08-19 |
United Technologies Corporation |
Gas turbine engine compressor arrangement
|
US8128021B2
(en)
*
|
2008-06-02 |
2012-03-06 |
United Technologies Corporation |
Engine mount system for a turbofan gas turbine engine
|
US8695920B2
(en)
|
2008-06-02 |
2014-04-15 |
United Technologies Corporation |
Gas turbine engine with low stage count low pressure turbine
|
US20130232768A1
(en)
|
2012-03-12 |
2013-09-12 |
United Technologies Corporation |
Turbine engine case mount and dismount
|
US9091210B2
(en)
*
|
2012-04-26 |
2015-07-28 |
United Technologies Corporation |
TEC mount redundant fastening
|
US9581108B2
(en)
|
2013-02-22 |
2017-02-28 |
United Technologies Corporation |
Pivot thrust reverser with multi-point actuation
|
US9694912B2
(en)
|
2013-02-22 |
2017-07-04 |
United Technologies Corporation |
ATR guide pins for sliding nacelle
|
US9435293B2
(en)
|
2013-02-22 |
2016-09-06 |
United Technologies Corporation |
Full ring sliding nacelle with thrust reverser
|
FR3010147B1
(fr)
|
2013-08-28 |
2015-08-21 |
Snecma |
Suspension isostatique d'un turboreacteur par double support arriere
|
US10371047B2
(en)
|
2013-10-16 |
2019-08-06 |
United Technologies Corporation |
Geared turbofan engine with targeted modular efficiency
|
DE102015226546A1
(de)
*
|
2015-12-22 |
2017-06-22 |
Rolls-Royce Deutschland Ltd & Co Kg |
Triebwerksverkleidung
|
US9972896B2
(en)
*
|
2016-06-23 |
2018-05-15 |
General Electric Company |
Wireless aircraft engine monitoring system
|