US4240250A
(en)
*
|
1977-12-27 |
1980-12-23 |
The Boeing Company |
Noise reducing air inlet for gas turbine engines
|
US4482114A
(en)
*
|
1981-01-26 |
1984-11-13 |
The Boeing Company |
Integrated thermal anti-icing and environmental control system
|
US4406431A
(en)
*
|
1981-11-23 |
1983-09-27 |
Omac, Inc. |
Air scoop lip warmer de-icing system
|
DE3212575C1
(de)
*
|
1982-04-03 |
1983-08-11 |
Dornier System Gmbh, 7990 Friedrichshafen |
Verfahren und Vorrichtung zur Temperaturregelung der von einer am Hochdruckausgang einer Verdichterstufe eines Strahltriebwerks ausgehenden Zapfluft
|
US4738416A
(en)
*
|
1986-09-26 |
1988-04-19 |
Quiet Nacelle Corporation |
Nacelle anti-icing system
|
US4782658A
(en)
*
|
1987-05-07 |
1988-11-08 |
Rolls-Royce Plc |
Deicing of a geared gas turbine engine
|
US4783026A
(en)
*
|
1987-05-22 |
1988-11-08 |
Avco Corporation |
Anti-icing management system
|
US4831819A
(en)
*
|
1987-07-02 |
1989-05-23 |
Avco Corporation |
Anti-icing valve
|
US5088277A
(en)
*
|
1988-10-03 |
1992-02-18 |
General Electric Company |
Aircraft engine inlet cowl anti-icing system
|
US5014933A
(en)
*
|
1989-04-27 |
1991-05-14 |
The Boeing Company |
Translating lip aircraft cowling structure adapted for noise reduction
|
US5050109A
(en)
*
|
1989-12-19 |
1991-09-17 |
The Boeing Company |
Method and apparatus for measuring the humidity of ambient air surrounding an aircraft in flight
|
US5114100A
(en)
*
|
1989-12-29 |
1992-05-19 |
The Boeing Company |
Anti-icing system for aircraft
|
US5161364A
(en)
*
|
1991-04-01 |
1992-11-10 |
United Technologies Corporation |
Control of aircraft bleed air stage mixing
|
FR2705996B1
(fr)
*
|
1993-06-03 |
1995-07-07 |
Snecma |
Système de dégivrage des parties avant d'une turbomachine.
|
US5558303A
(en)
*
|
1994-12-27 |
1996-09-24 |
Koethe; Terence L. |
Method and apparatus for using hot fuels to de-ice aircraft
|
US5779196A
(en)
*
|
1995-12-08 |
1998-07-14 |
The Boeing Company |
Ram air drive laminar flow control system
|
FR2757823B1
(fr)
*
|
1996-12-26 |
1999-03-12 |
Aerospatiale |
Nacelle de turboreacteur a ecoulement laminaire
|
US6179251B1
(en)
*
|
1998-02-06 |
2001-01-30 |
Northrop Grumman Corporation |
Thin inlet lip design for low drag and reduced nacelle size
|
US6442944B1
(en)
*
|
2000-10-26 |
2002-09-03 |
Lockheet Martin Corporation |
Bleed air heat exchanger integral to a jet engine
|
US20020172858A1
(en)
*
|
2001-05-15 |
2002-11-21 |
Daniel Ashikian |
Thermo-dynamic battery storage unit
|
US6481210B1
(en)
|
2001-05-16 |
2002-11-19 |
Honeywell International, Inc. |
Smart surge bleed valve system and method
|
GB0122672D0
(en)
*
|
2001-09-20 |
2001-11-14 |
Honeywell Normalair Garrett |
Environmental control systems
|
GB0311663D0
(en)
*
|
2003-05-21 |
2003-06-25 |
Rolls Royce Plc |
Aeroengine intake
|
US6990797B2
(en)
*
|
2003-09-05 |
2006-01-31 |
General Electric Company |
Methods and apparatus for operating gas turbine engines
|
DE10361655B4
(de)
*
|
2003-12-30 |
2007-10-04 |
Airbus Deutschland Gmbh |
Vorrichtung und Verfahren zur Fußbodenheizung in einem Flugzeug
|
US7784739B2
(en)
*
|
2004-05-26 |
2010-08-31 |
The Boeing Company |
Detection system and method for ice and other debris
|
FR2875542B1
(fr)
*
|
2004-09-21 |
2009-02-13 |
Airbus France Sas |
Dispositif de protection contre le givrage pour moteurs d'aeronefs et procedes de degivrage associe
|
US7171819B2
(en)
*
|
2005-01-21 |
2007-02-06 |
Honeywell International, Inc. |
Indirect regenerative air cycle for integrated power and cooling machines
|
US8366047B2
(en)
*
|
2005-05-31 |
2013-02-05 |
United Technologies Corporation |
Electrothermal inlet ice protection system
|
US20070022732A1
(en)
*
|
2005-06-22 |
2007-02-01 |
General Electric Company |
Methods and apparatus for operating gas turbine engines
|
EP1739013B1
(fr)
*
|
2005-07-01 |
2008-05-28 |
Saab Ab |
Dispositif et système de dégivrage pour aéronefs comprenant ce dispositif
|
WO2008104716A2
(fr)
*
|
2007-02-20 |
2008-09-04 |
Airbus France |
Procede de realisation d ' un revetement pour le traitement acoustique et revetement ainsi obtenu
|
US7708230B2
(en)
*
|
2007-05-29 |
2010-05-04 |
United Technologies Corporation |
Flow distribution system for inlet flow control
|
US7874137B2
(en)
*
|
2007-06-18 |
2011-01-25 |
Honeywell International Inc. |
Gas turbine engine anti-ice formation device and system
|
US7856824B2
(en)
*
|
2007-06-25 |
2010-12-28 |
Honeywell International Inc. |
Cooling systems for use on aircraft
|
FR2925878B1
(fr)
*
|
2007-12-28 |
2010-04-23 |
Airbus France |
Ensemble propulsif d'aeronef comprenant des systemes de prelevement d'air chaud
|
DE102008007278B4
(de)
*
|
2008-02-01 |
2010-04-08 |
Airbus Deutschland Gmbh |
Bleedairduct-Segment, Bleedairduct-Anordnung mit solchen Bleedairduct-Segmenten und Bleedairduct-System mit Regulierungsvorrichtung
|
US8769924B2
(en)
*
|
2008-05-30 |
2014-07-08 |
United Technologies Corporation |
Gas turbine engine assembly including accessory components within the nacelle
|
US8061657B2
(en)
*
|
2008-12-31 |
2011-11-22 |
General Electric Company |
Method and apparatus for aircraft anti-icing
|
US20100329836A1
(en)
*
|
2009-06-30 |
2010-12-30 |
Wayne Garcia Edmondson |
Method of operating a heated guide vane assembly
|
US20100326041A1
(en)
*
|
2009-06-30 |
2010-12-30 |
Wayne Garcia Edmondson |
Heated guide vane
|
DE102009055879A1
(de)
*
|
2009-11-26 |
2011-06-01 |
Rolls-Royce Deutschland Ltd & Co Kg |
Flugzeugenteisungsvorrichtung und Triebwerksgondel einer Fluggasturbine mit Enteisungsvorrichtung
|
US8382039B2
(en)
*
|
2009-12-30 |
2013-02-26 |
MRA Systems Inc. |
Turbomachine nacelle and anti-icing system and method therefor
|
US9114877B2
(en)
*
|
2010-08-30 |
2015-08-25 |
Ge Aviation Systems, Llc |
Method and system for vehicle thermal management
|
FR2966127B1
(fr)
*
|
2010-10-15 |
2013-06-14 |
Airbus Operations Sas |
Nacelle d'aeronef incorporant au moins une cloison radiale entre deux conduits
|
US8397487B2
(en)
|
2011-02-28 |
2013-03-19 |
General Electric Company |
Environmental control system supply precooler bypass
|
EP3385510B1
(fr)
*
|
2011-03-17 |
2022-02-09 |
Airbus Canada Limited Partnership |
Procédé pour faire fonctionner un prérefroidisseur dans un aéronef et moteur aéronef
|
US8444093B1
(en)
|
2011-04-18 |
2013-05-21 |
Eran Epstein |
Airplane leading edge de-icing apparatus
|
US8463496B2
(en)
|
2011-07-06 |
2013-06-11 |
Hamilton Sundstrand Corporation |
Decoupling control architecture for pressure and flow controls in series
|
US9239005B2
(en)
|
2011-11-25 |
2016-01-19 |
Pratt & Whitney Canada Corp. |
Cooling system for engine and aircraft air
|
US9222411B2
(en)
|
2011-12-21 |
2015-12-29 |
General Electric Company |
Bleed air and hot section component cooling air system and method
|
US9109514B2
(en)
*
|
2012-01-10 |
2015-08-18 |
Hamilton Sundstrand Corporation |
Air recovery system for precooler heat-exchanger
|
US8452516B1
(en)
|
2012-01-31 |
2013-05-28 |
United Technologies Corporation |
Variable vane scheduling based on flight conditions for inclement weather
|
FR2987602B1
(fr)
*
|
2012-03-02 |
2014-02-28 |
Aircelle Sa |
Nacelle de turbomoteur equipe d'un echangeur de chaleur
|
US20130327012A1
(en)
*
|
2012-06-11 |
2013-12-12 |
General Electric Company |
Gas turbine anti-icing system
|
WO2014030024A1
(fr)
|
2012-08-22 |
2014-02-27 |
Bombardier Inc. |
Système de pré-refroidissement comprenant une soupape de dérivation, dispositif de commande associé et procédé et aéronef utilisant ceux-ci
|
US10385777B2
(en)
*
|
2012-10-01 |
2019-08-20 |
United Technologies Corporation |
Bifurcated inlet scoop for gas turbine engine
|
US9187180B2
(en)
*
|
2013-05-24 |
2015-11-17 |
Hamilton Sundstrand Corporation |
Thermal pneumatic deicing system for an aircraft RAM air heat exchanger
|
FR3007738B1
(fr)
*
|
2013-06-28 |
2015-07-31 |
Aircelle Sa |
Dispositif de degivrage et de conditionnement pour aeronef
|
GB2516648B
(en)
*
|
2013-07-29 |
2016-08-31 |
Charles Wells John |
Fitting for a gas turbine engine
|
WO2015183360A2
(fr)
|
2014-03-04 |
2015-12-03 |
Parker-Hannifin Corporation |
Échangeur de chaleur pour aéronef à écoulement laminaire
|
US10144520B2
(en)
*
|
2014-04-14 |
2018-12-04 |
Rohr, Inc. |
De-icing system with thermal management
|
FR3021350B1
(fr)
*
|
2014-05-20 |
2016-07-01 |
Snecma |
Procede de detection de fuite de fluide dans une turbomachine et systeme de distribution de fluide
|
US10487690B2
(en)
*
|
2014-08-18 |
2019-11-26 |
Rohr, Inc. |
Actively controlled cooling air exhaust door on an aircraft engine nacelle
|
GB201416928D0
(en)
*
|
2014-09-25 |
2014-11-12 |
Rolls Royce Plc |
A gas turbine and a method of washing a gas turbine engine
|
US10421551B2
(en)
*
|
2014-12-15 |
2019-09-24 |
United Technologies Corporation |
Aircraft anti-icing system
|
US10100733B2
(en)
*
|
2015-07-31 |
2018-10-16 |
Ge Aviation Systems Llc |
Turbine engine with anti-ice valve assembly, bleed air valve, and method of operating
|
US10393020B2
(en)
*
|
2015-08-26 |
2019-08-27 |
Rohr, Inc. |
Injector nozzle configuration for swirl anti-icing system
|
US10017262B2
(en)
*
|
2015-09-22 |
2018-07-10 |
Rohr, Inc. |
Pulsed deicing system
|
US11473497B2
(en)
*
|
2016-03-15 |
2022-10-18 |
Hamilton Sundstrand Corporation |
Engine bleed system with motorized compressor
|
US10450954B2
(en)
|
2016-03-17 |
2019-10-22 |
General Electric Company |
Internally heated engine inlet screen for aircraft engines
|
US10239626B2
(en)
*
|
2016-03-29 |
2019-03-26 |
Gulfstream Aerospace Corporation |
Arrangements and methods for supplying heated air to a wing anti-icing system
|
US10189572B2
(en)
*
|
2016-05-02 |
2019-01-29 |
The Boeing Company |
Systems and methods for preventing ice formation on portions of an aircraft
|
US10513978B2
(en)
|
2016-05-02 |
2019-12-24 |
General Electric Company |
Directed flow nozzle swirl enhancer
|
US10267334B2
(en)
*
|
2016-08-01 |
2019-04-23 |
United Technologies Corporation |
Annular heatshield
|
US10708979B2
(en)
|
2016-10-07 |
2020-07-07 |
De-Ice Technologies |
Heating a bulk medium
|
US10407164B2
(en)
|
2016-10-28 |
2019-09-10 |
Honeywell International Inc. |
Air distribution system with drag reducing inlet
|
US11242767B2
(en)
*
|
2017-05-01 |
2022-02-08 |
General Electric Company |
Additively manufactured component including an impingement structure
|
GB201716499D0
(en)
*
|
2017-10-09 |
2017-11-22 |
Rolls Royce Plc |
Gas turbine engine fireproofing
|
US10995997B2
(en)
|
2018-06-26 |
2021-05-04 |
Hamilton Sunstrand Corporation |
Heat exchanger with integral features
|
US11333438B2
(en)
|
2018-06-26 |
2022-05-17 |
Hamilton Sundstrand Corporation |
Heat exchanger with water extraction
|
US12024299B2
(en)
|
2018-08-27 |
2024-07-02 |
De-Ice Technologies, Inc. |
De-icing systems
|
FR3088961A1
(fr)
|
2018-11-22 |
2020-05-29 |
Airbus Operations (S.A.S.) |
Turbomachine équipée d’un système de dégivrage de l’entrée d’air.
|
FR3089204B1
(fr)
*
|
2018-11-29 |
2022-04-01 |
Safran |
Système de gestion d’air notamment pour pack de conditionnement d’air et dégivrage
|
US11560843B2
(en)
*
|
2020-02-25 |
2023-01-24 |
General Electric Company |
Frame for a heat engine
|
US11326519B2
(en)
|
2020-02-25 |
2022-05-10 |
General Electric Company |
Frame for a heat engine
|
US11255264B2
(en)
|
2020-02-25 |
2022-02-22 |
General Electric Company |
Frame for a heat engine
|
US11965697B2
(en)
|
2021-03-02 |
2024-04-23 |
General Electric Company |
Multi-fluid heat exchanger
|
US11788465B2
(en)
|
2022-01-19 |
2023-10-17 |
General Electric Company |
Bleed flow assembly for a gas turbine engine
|
US11808281B2
(en)
|
2022-03-04 |
2023-11-07 |
General Electric Company |
Gas turbine engine with variable pitch inlet pre-swirl features
|
US11834995B2
(en)
|
2022-03-29 |
2023-12-05 |
General Electric Company |
Air-to-air heat exchanger potential in gas turbine engines
|
US11680530B1
(en)
|
2022-04-27 |
2023-06-20 |
General Electric Company |
Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine
|
US11834992B2
(en)
|
2022-04-27 |
2023-12-05 |
General Electric Company |
Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
|
US11927134B1
(en)
|
2023-01-27 |
2024-03-12 |
General Electric Company |
Gas turbine engine having a heat exchanger located in an annular duct
|