FR2728938A1
(fr)
*
|
1995-01-04 |
1996-07-05 |
Snecma |
Systeme de regulation des temperatures de l'huile et du carburant dans un turboreacteur
|
DE19524733A1
(de)
*
|
1995-07-07 |
1997-01-09 |
Bmw Rolls Royce Gmbh |
Fluggasturbinen-Triebwerk mit einem Flüssigkeits-Luft-Wärmetauscher
|
FR2742479B1
(fr)
*
|
1995-12-13 |
1998-01-16 |
Snecma |
Dispositif de refroidissement d'un turbomoteur sur aeronef
|
FR2788308A1
(fr)
*
|
1999-01-07 |
2000-07-13 |
Snecma |
Dispositif de refroidissement d'un reducteur de vitesse de turbomachine
|
US6651929B2
(en)
*
|
2001-10-29 |
2003-11-25 |
Pratt & Whitney Canada Corp. |
Passive cooling system for auxiliary power unit installation
|
US7152410B2
(en)
*
|
2004-06-10 |
2006-12-26 |
Honeywell International, Inc. |
System and method for dumping surge flow into eductor primary nozzle for free turbine
|
US7454894B2
(en)
*
|
2004-12-07 |
2008-11-25 |
United Technologies Corporation |
Supplemental oil cooler airflow for gas turbine engine
|
FR2889254B1
(fr)
*
|
2005-07-28 |
2011-05-06 |
Airbus France |
Turboreacteur pour aeronef, ensemble propulseur comportant un tel turboreacteur, et aeronef comportant au moins un tel ensemble propulseur
|
DE102005048017A1
(de)
*
|
2005-10-06 |
2007-04-12 |
Rolls-Royce Deutschland Ltd & Co Kg |
Brennstoff-und Ölsystem einer Gasturbine
|
DE102005048019A1
(de)
*
|
2005-10-06 |
2007-04-12 |
Rolls-Royce Deutschland Ltd & Co Kg |
Verfahren zur Ölversorgung eines Flugzeugtriebwerks
|
GB0607773D0
(en)
*
|
2006-04-20 |
2006-05-31 |
Rolls Royce Plc |
A gas turbine engine
|
GB0607771D0
(en)
*
|
2006-04-20 |
2006-05-31 |
Rolls Royce Plc |
A heat exchanger arrangement
|
US8776952B2
(en)
*
|
2006-05-11 |
2014-07-15 |
United Technologies Corporation |
Thermal management system for turbofan engines
|
US7765788B2
(en)
*
|
2006-07-06 |
2010-08-03 |
United Technologies Corporation |
Cooling exchanger duct
|
US7658060B2
(en)
*
|
2006-07-19 |
2010-02-09 |
United Technologies Corporation |
Lubricant cooling exchanger dual intake duct
|
US20080053060A1
(en)
*
|
2006-08-29 |
2008-03-06 |
Pratt & Whitney Canada Corp. |
Bypass lip seal
|
US7861512B2
(en)
*
|
2006-08-29 |
2011-01-04 |
Pratt & Whitney Canada Corp. |
Turbofan bypass duct air cooled fluid cooler installation
|
US8205427B2
(en)
*
|
2006-11-09 |
2012-06-26 |
United Technologies Corporation |
Interdependent lubrication systems in a turbine engine
|
EP1944475B1
(de)
*
|
2007-01-08 |
2015-08-12 |
United Technologies Corporation |
Wärmeaustauschsystem
|
US7856824B2
(en)
*
|
2007-06-25 |
2010-12-28 |
Honeywell International Inc. |
Cooling systems for use on aircraft
|
US8763363B2
(en)
*
|
2007-07-06 |
2014-07-01 |
General Electric Company |
Method and system for cooling fluid in a turbine engine
|
US20090313999A1
(en)
*
|
2008-05-13 |
2009-12-24 |
Scott Hunter |
Method and apparatus for controlling fuel in a gas turbine engine
|
US7984606B2
(en)
|
2008-11-03 |
2011-07-26 |
Propulsion, Gas Turbine, And Energy Evaluations, Llc |
Systems and methods for thermal management in a gas turbine powerplant
|
US8627667B2
(en)
*
|
2008-12-29 |
2014-01-14 |
Roll-Royce Corporation |
Gas turbine engine duct having a coupled fluid volume
|
US8740102B2
(en)
*
|
2008-12-30 |
2014-06-03 |
Rolls-Royce Corporation |
Gas turbine engine valve
|
US8529189B2
(en)
*
|
2009-01-30 |
2013-09-10 |
Honeywell International Inc. |
Linear quadratic regulator control for bleed air system fan air valve
|
GB2473651B
(en)
*
|
2009-09-21 |
2011-08-31 |
Rolls Royce Plc |
Gas turbine aircraft engines and operation thereof
|
FR2951228B1
(fr)
*
|
2009-10-13 |
2013-07-19 |
Snecma |
Procede et systeme de gestion d'echanges thermiques entre fluides dans une turbomachine
|
FR2955616B1
(fr)
*
|
2010-01-26 |
2012-07-20 |
Airbus Operations Sas |
Dispositif de refroidissement pour propulseur d'aeronef
|
US20110182723A1
(en)
*
|
2010-01-26 |
2011-07-28 |
Airbus Operations (S.A.S) |
Turbomachine aircraft propeller
|
GB201001410D0
(en)
*
|
2010-01-29 |
2010-03-17 |
Rolls Royce Plc |
Oil cooler
|
FR2958974B1
(fr)
*
|
2010-04-16 |
2016-06-10 |
Snecma |
Moteur de turbine a gaz muni d'un echangeur de chaleur air-huile dans sa manche d'entree d'air
|
GB201007063D0
(en)
*
|
2010-04-28 |
2010-06-09 |
Rolls Royce Plc |
A gas turbine engine
|
US8602717B2
(en)
*
|
2010-10-28 |
2013-12-10 |
United Technologies Corporation |
Compression system for turbomachine heat exchanger
|
FR2969701B1
(fr)
*
|
2010-12-23 |
2015-06-19 |
Snecma |
Procede et systeme de gestion d'echanges thermiques entre fluides dans une turbomachine aeronautique.
|
US8904753B2
(en)
|
2011-04-28 |
2014-12-09 |
United Technologies Corporation |
Thermal management system for gas turbine engine
|
US9080511B2
(en)
|
2011-10-21 |
2015-07-14 |
United Technologies Corporation |
Integrated thermal system for a gas turbine engine
|
US9200569B2
(en)
*
|
2011-10-21 |
2015-12-01 |
United Technologies Corporation |
Compartment cooling for a gas turbine engine
|
US9243563B2
(en)
*
|
2012-01-25 |
2016-01-26 |
Honeywell International Inc. |
Gas turbine engine in-board cooled cooling air system
|
US8261527B1
(en)
*
|
2012-01-31 |
2012-09-11 |
United Technologies Corporation |
Gas turbine engine with geared turbofan and oil thermal management system with unique heat exchanger structure
|
US9200570B2
(en)
|
2012-02-24 |
2015-12-01 |
Pratt & Whitney Canada Corp. |
Air-cooled oil cooler for turbofan engine
|
US9267390B2
(en)
|
2012-03-22 |
2016-02-23 |
Honeywell International Inc. |
Bi-metallic actuator for selectively controlling air flow between plena in a gas turbine engine
|
EP2900965B1
(de)
|
2012-09-28 |
2017-11-22 |
United Technologies Corporation |
Gasturbinenmotor-wärmeregelungssystem für wärmetauscher mit bypass-strömung
|
GB201220174D0
(en)
*
|
2012-11-09 |
2012-12-26 |
Rolls Royce Plc |
Heat exchange arrangemnt
|
US9476313B2
(en)
|
2012-12-21 |
2016-10-25 |
United Technologies Corporation |
Gas turbine engine including a pre-diffuser heat exchanger
|
US10350521B2
(en)
|
2013-01-15 |
2019-07-16 |
United Technologies Corporation |
Fuel system ice and debris separator (IDS) with partial filter screen and torturous path
|
EP2981697B1
(de)
|
2013-01-21 |
2019-10-02 |
United Technologies Corporation |
Luft-/ölkühler-luftstromverstärkungssystem sowie dazugehöriges verfahren
|
EP2946090A4
(de)
|
2013-01-21 |
2016-06-01 |
United Technologies Corp |
Gasturbinenmotor mit getriebeturbolüfter und ölwärmeregelungssystem mit eigener wärmetauscherstruktur
|
US9206912B2
(en)
*
|
2013-01-23 |
2015-12-08 |
The Boeing Company |
Dual door fan air modulating valve
|
WO2014120125A1
(en)
|
2013-01-29 |
2014-08-07 |
United Technologies Corporation |
Gas turbine engine with lower bifurcation heat exchanger
|
US9840967B2
(en)
|
2013-03-04 |
2017-12-12 |
Rolls-Royce North American Technologies, Inc. |
Ram air thermal management system
|
US10352191B2
(en)
|
2013-03-15 |
2019-07-16 |
United Technologies Corporation |
Gas turbine engine with air-oil cooler oil tank
|
CN104373218B
(zh)
*
|
2014-11-05 |
2016-08-24 |
成都发动机(集团)有限公司 |
一种航空发动机滑油润滑升温保障系统
|
GB201504005D0
(en)
*
|
2015-03-10 |
2015-04-22 |
Rolls Royce Plc |
Engine fuel-oil heat exchange system
|
US10443503B2
(en)
|
2015-03-27 |
2019-10-15 |
Pratt & Whitney Canada Corp. |
Fuel system for a gas turbine engine
|
US10107200B2
(en)
|
2015-04-30 |
2018-10-23 |
General Electric Company |
Turbine engine thermal management
|
FR3044636B1
(fr)
*
|
2015-12-08 |
2019-08-30 |
Safran Aircraft Engines |
Turbomachine d'aeronef equipee d'un echangeur de chaleur surfacique air-huile
|
US10513981B2
(en)
*
|
2016-01-21 |
2019-12-24 |
Rolls-Royce North American Technologies Inc. |
Heat exchanger assembly for a gas turbine engine propulsion system
|
US10494949B2
(en)
*
|
2016-08-05 |
2019-12-03 |
General Electric Company |
Oil cooling systems for a gas turbine engine
|
US10544717B2
(en)
|
2016-09-07 |
2020-01-28 |
Pratt & Whitney Canada Corp. |
Shared oil system arrangement for an engine component and a generator
|
US10486816B2
(en)
*
|
2017-04-07 |
2019-11-26 |
Hamilton Sundstrand Corporation |
Fan bypass and shutoff check valve
|
CN106870160B
(zh)
*
|
2017-04-09 |
2018-02-23 |
中国科学院工程热物理研究所 |
一种发动机热端结构
|
US20190120140A1
(en)
*
|
2017-10-24 |
2019-04-25 |
United Technologies Corporation |
Gas turbine engine with vacuum generator for reducing bearing compartment pressure
|
FR3074533B1
(fr)
*
|
2017-12-06 |
2020-11-06 |
Safran Aircraft Engines |
Circuit de commande hydraulique et pneumatique pour turboreacteur a echangeur de chaleur carburant/air
|
US11028775B2
(en)
|
2018-08-23 |
2021-06-08 |
The Boeing Company |
Bleed air boosted engine oil cooler
|
US11512639B2
(en)
*
|
2021-01-26 |
2022-11-29 |
General Electric Company |
Heat transfer system
|
FR3120655B1
(fr)
*
|
2021-03-09 |
2023-01-27 |
Safran |
Échangeur de chaleur surfacique avec sorties additionelles
|
US20230068644A1
(en)
*
|
2021-08-31 |
2023-03-02 |
Pratt & Whitney Canada Corp. |
Heat exchange system using compressor air for fuel pre-heating
|
CN114151137B
(zh)
*
|
2021-10-20 |
2023-09-05 |
中国航发四川燃气涡轮研究院 |
一种高马赫数航空发动机舱与涡轮盘联合冷却热管理系统
|
US20230235700A1
(en)
*
|
2022-01-27 |
2023-07-27 |
Rolls-Royce Plc |
Gas turbine engine and a method of operating a heat exchanger assembly for a gas turbine engine
|
EP4239174A1
(de)
*
|
2022-03-03 |
2023-09-06 |
Rolls-Royce plc |
Brennstoffmanagementsystem
|