FR2734320B1
(fr)
*
|
1995-05-15 |
1997-07-18 |
Aerospatiale |
Dispositif pour prelever et refroidir de l'air chaud au niveau d'un moteur d'aeronef
|
US5697208A
(en)
*
|
1995-06-02 |
1997-12-16 |
Solar Turbines Incorporated |
Turbine cooling cycle
|
US5581996A
(en)
*
|
1995-08-16 |
1996-12-10 |
General Electric Company |
Method and apparatus for turbine cooling
|
US5724806A
(en)
*
|
1995-09-11 |
1998-03-10 |
General Electric Company |
Extracted, cooled, compressed/intercooled, cooling/combustion air for a gas turbine engine
|
US5680767A
(en)
*
|
1995-09-11 |
1997-10-28 |
General Electric Company |
Regenerative combustor cooling in a gas turbine engine
|
US5901548A
(en)
*
|
1996-12-23 |
1999-05-11 |
General Electric Company |
Air assist fuel atomization in a gas turbine engine
|
KR100243379B1
(ko)
*
|
1996-12-31 |
2000-03-02 |
유무성 |
공기 조화 시스템
|
US5918458A
(en)
*
|
1997-02-14 |
1999-07-06 |
General Electric Company |
System and method of providing clean filtered cooling air to a hot portion of a gas turbine engine
|
DE10019437A1
(de)
|
2000-04-19 |
2001-12-20 |
Rolls Royce Deutschland |
Verfahren und Vorrichtung zum Kühlen der Gehäuse von Turbinen von Strahltriebwerken
|
US6389793B1
(en)
*
|
2000-04-19 |
2002-05-21 |
General Electric Company |
Combustion turbine cooling media supply system and related method
|
US6401460B1
(en)
*
|
2000-08-18 |
2002-06-11 |
Siemens Westinghouse Power Corporation |
Active control system for gas turbine blade tip clearance
|
DE10122695A1
(de)
*
|
2001-05-10 |
2002-11-21 |
Siemens Ag |
Verfahren zur Kühlung einer Gasturbine und Gasturbinenanlage
|
US6550254B2
(en)
|
2001-08-17 |
2003-04-22 |
General Electric Company |
Gas turbine engine bleed scoops
|
US7121078B2
(en)
*
|
2003-01-28 |
2006-10-17 |
General Electric Company |
Methods and apparatus for operating gas turbine engines
|
FR2864996B1
(fr)
*
|
2004-01-13 |
2006-03-10 |
Snecma Moteurs |
Systeme de refroidissement de parties chaudes d'un moteur d'aeronef, et moteur d'aeronef equipe d'un tel systeme de refroidissement
|
US7225624B2
(en)
*
|
2004-06-08 |
2007-06-05 |
Allison Advanced Development Company |
Method and apparatus for increasing the pressure of cooling fluid within a gas turbine engine
|
US7269955B2
(en)
*
|
2004-08-25 |
2007-09-18 |
General Electric Company |
Methods and apparatus for maintaining rotor assembly tip clearances
|
DE102005011574A1
(de)
|
2005-03-14 |
2006-09-21 |
Robert Bosch Gmbh |
Zwischenelement für ein Brennstoffeinspritzventil
|
DE502006008758D1
(de)
*
|
2005-10-12 |
2011-03-03 |
Alstom Technology Ltd |
Gasturbine mit geregelter Luftkühlung
|
GB0607773D0
(en)
|
2006-04-20 |
2006-05-31 |
Rolls Royce Plc |
A gas turbine engine
|
US8387362B2
(en)
*
|
2006-10-19 |
2013-03-05 |
Michael Ralph Storage |
Method and apparatus for operating gas turbine engine heat exchangers
|
US7665327B2
(en)
*
|
2007-01-17 |
2010-02-23 |
Sub-Zero, Inc. |
Chilled food storage area for refrigerated appliance
|
GB2449095B
(en)
*
|
2007-05-10 |
2009-05-27 |
Rolls Royce Plc |
Re-Pressurisation device
|
US8763363B2
(en)
*
|
2007-07-06 |
2014-07-01 |
General Electric Company |
Method and system for cooling fluid in a turbine engine
|
US8590286B2
(en)
*
|
2007-12-05 |
2013-11-26 |
United Technologies Corp. |
Gas turbine engine systems involving tip fans
|
US8181443B2
(en)
*
|
2008-12-10 |
2012-05-22 |
Pratt & Whitney Canada Corp. |
Heat exchanger to cool turbine air cooling flow
|
US9249736B2
(en)
*
|
2008-12-29 |
2016-02-02 |
United Technologies Corporation |
Inlet guide vanes and gas turbine engine systems involving such vanes
|
EP2336525B1
(de)
*
|
2009-12-21 |
2015-08-26 |
Techspace Aero S.A. |
Einbau eines Luft-Flüssigkeits-Wärmetauschers in einen Motor
|
US8256229B2
(en)
*
|
2010-04-09 |
2012-09-04 |
United Technologies Corporation |
Rear hub cooling for high pressure compressor
|
US9410482B2
(en)
|
2010-12-24 |
2016-08-09 |
Rolls-Royce North American Technologies, Inc. |
Gas turbine engine heat exchanger
|
FR2975434B1
(fr)
*
|
2011-05-16 |
2015-08-14 |
Mbda France |
Turbomachine a chambre de detonation et engin volant pourvu d'une telle turbomachine
|
US20130092350A1
(en)
*
|
2011-10-14 |
2013-04-18 |
General Electric Company |
System for cooling fluid flow within an engine
|
US9045998B2
(en)
|
2011-12-12 |
2015-06-02 |
Honeywell International Inc. |
System for directing air flow to a plurality of plena
|
US9109514B2
(en)
|
2012-01-10 |
2015-08-18 |
Hamilton Sundstrand Corporation |
Air recovery system for precooler heat-exchanger
|
US8967528B2
(en)
*
|
2012-01-24 |
2015-03-03 |
The Boeing Company |
Bleed air systems for use with aircrafts and related methods
|
US9243563B2
(en)
*
|
2012-01-25 |
2016-01-26 |
Honeywell International Inc. |
Gas turbine engine in-board cooled cooling air system
|
US9038398B2
(en)
|
2012-02-27 |
2015-05-26 |
United Technologies Corporation |
Gas turbine engine buffer cooling system
|
US9157325B2
(en)
|
2012-02-27 |
2015-10-13 |
United Technologies Corporation |
Buffer cooling system providing gas turbine engine architecture cooling
|
US9347374B2
(en)
|
2012-02-27 |
2016-05-24 |
United Technologies Corporation |
Gas turbine engine buffer cooling system
|
US9435259B2
(en)
|
2012-02-27 |
2016-09-06 |
United Technologies Corporation |
Gas turbine engine cooling system
|
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
|
US20150252731A1
(en)
*
|
2012-10-01 |
2015-09-10 |
United Technologies Corporation |
Gas turbine engine including bleed system coupled to upstream and downstream locations of compressor
|
US9714610B2
(en)
*
|
2012-10-04 |
2017-07-25 |
United Technologies Corporation |
Low profile compressor bleed air-oil coolers
|
US9562475B2
(en)
*
|
2012-12-19 |
2017-02-07 |
Siemens Aktiengesellschaft |
Vane carrier temperature control system in a gas turbine engine
|
US10337406B2
(en)
|
2013-02-28 |
2019-07-02 |
United Technologies Corporation |
Method and apparatus for handling pre-diffuser flow for cooling high pressure turbine components
|
US9429072B2
(en)
|
2013-05-22 |
2016-08-30 |
General Electric Company |
Return fluid air cooler system for turbine cooling with optional power extraction
|
US9422063B2
(en)
|
2013-05-31 |
2016-08-23 |
General Electric Company |
Cooled cooling air system for a gas turbine
|
GB201319563D0
(en)
|
2013-11-06 |
2013-12-18 |
Rolls Royce Plc |
Pneumatic system for an aircraft
|
US9341119B2
(en)
*
|
2014-07-03 |
2016-05-17 |
Hamilton Sundstrand Corporation |
Cooling air system for aircraft turbine engine
|
US10125686B2
(en)
*
|
2014-12-05 |
2018-11-13 |
General Electric Company |
Turbine engine assembly and method of manufacturing
|
US20160237908A1
(en)
*
|
2015-02-12 |
2016-08-18 |
United Technologies Corporation |
Intercooled cooling air using existing heat exchanger
|
US10371055B2
(en)
|
2015-02-12 |
2019-08-06 |
United Technologies Corporation |
Intercooled cooling air using cooling compressor as starter
|
US10731560B2
(en)
|
2015-02-12 |
2020-08-04 |
Raytheon Technologies Corporation |
Intercooled cooling air
|
US20160237905A1
(en)
*
|
2015-02-12 |
2016-08-18 |
United Technologies Corporation |
Intercooled cooling air
|
US11808210B2
(en)
|
2015-02-12 |
2023-11-07 |
Rtx Corporation |
Intercooled cooling air with heat exchanger packaging
|
US20160237907A1
(en)
*
|
2015-02-12 |
2016-08-18 |
United Technologies Corporation |
Intercooled cooling air with auxiliary compressor control
|
US10480419B2
(en)
|
2015-04-24 |
2019-11-19 |
United Technologies Corporation |
Intercooled cooling air with plural heat exchangers
|
US10830148B2
(en)
|
2015-04-24 |
2020-11-10 |
Raytheon Technologies Corporation |
Intercooled cooling air with dual pass heat exchanger
|
US9850819B2
(en)
|
2015-04-24 |
2017-12-26 |
United Technologies Corporation |
Intercooled cooling air with dual pass heat exchanger
|
US10221862B2
(en)
|
2015-04-24 |
2019-03-05 |
United Technologies Corporation |
Intercooled cooling air tapped from plural locations
|
US10100739B2
(en)
|
2015-05-18 |
2018-10-16 |
United Technologies Corporation |
Cooled cooling air system for a gas turbine engine
|
US10794288B2
(en)
|
2015-07-07 |
2020-10-06 |
Raytheon Technologies Corporation |
Cooled cooling air system for a turbofan engine
|
EP3121411B1
(de)
*
|
2015-07-21 |
2018-12-12 |
United Technologies Corporation |
Zwischengekühlte kühlluft unter verwendung eines bestehenden wärmetauschers
|
US10371056B2
(en)
*
|
2015-12-10 |
2019-08-06 |
United Technologies Corporation |
Multi-source turbine cooling air
|
US10330010B2
(en)
*
|
2015-12-14 |
2019-06-25 |
United Technologies Corporation |
Compressor core inner diameter cooling
|
US10443508B2
(en)
|
2015-12-14 |
2019-10-15 |
United Technologies Corporation |
Intercooled cooling air with auxiliary compressor control
|
US20170184027A1
(en)
*
|
2015-12-29 |
2017-06-29 |
General Electric Company |
Method and system for compressor and turbine cooling
|
US20170218844A1
(en)
*
|
2016-02-01 |
2017-08-03 |
United Technologies Corporation |
Cooling air for variable area turbine
|
US20170241340A1
(en)
*
|
2016-02-19 |
2017-08-24 |
United Technologies Corporation |
Turbocompressor for aircraft environmental control system
|
US10125687B2
(en)
|
2016-02-29 |
2018-11-13 |
General Electric Company |
System and method for cooling a turbine engine assembly
|
US10344614B2
(en)
|
2016-04-12 |
2019-07-09 |
United Technologies Corporation |
Active clearance control for a turbine and case
|
US10760492B2
(en)
|
2016-04-13 |
2020-09-01 |
Raytheon Technologies Corporation |
Cooling air architecture for compact size and performance improvement
|
US20170306847A1
(en)
*
|
2016-04-26 |
2017-10-26 |
United Technologies Corporation |
Combined Drive for Cooling Air Using Cooing Compressor and Aircraft Air Supply Pump
|
US10746181B2
(en)
|
2016-08-22 |
2020-08-18 |
Raytheon Technologies Corporation |
Variable speed boost compressor for gas turbine engine cooling air supply
|
US10436115B2
(en)
*
|
2016-08-22 |
2019-10-08 |
United Technologies Corporation |
Heat exchanger for gas turbine engine with support damper mounting
|
US10982595B2
(en)
*
|
2016-08-23 |
2021-04-20 |
Raytheon Technologies Corporation |
Heat exchanger for gas turbine engine mounted in intermediate case
|
US10669940B2
(en)
|
2016-09-19 |
2020-06-02 |
Raytheon Technologies Corporation |
Gas turbine engine with intercooled cooling air and turbine drive
|
US10794290B2
(en)
|
2016-11-08 |
2020-10-06 |
Raytheon Technologies Corporation |
Intercooled cooled cooling integrated air cycle machine
|
US10550768B2
(en)
|
2016-11-08 |
2020-02-04 |
United Technologies Corporation |
Intercooled cooled cooling integrated air cycle machine
|
US10458332B2
(en)
*
|
2017-01-17 |
2019-10-29 |
United Technologies Corporation |
Cooled gas turbine engine cooling air with cold air dump
|
US10961911B2
(en)
|
2017-01-17 |
2021-03-30 |
Raytheon Technologies Corporation |
Injection cooled cooling air system for a gas turbine engine
|
US10995673B2
(en)
|
2017-01-19 |
2021-05-04 |
Raytheon Technologies Corporation |
Gas turbine engine with intercooled cooling air and dual towershaft accessory gearbox
|
US10823070B2
(en)
*
|
2017-01-20 |
2020-11-03 |
Raytheon Technologies Corporation |
Intercooled cooling air system with bypass
|
KR101953963B1
(ko)
*
|
2017-01-24 |
2019-03-04 |
두산중공업 주식회사 |
가스터빈
|
US10371383B2
(en)
|
2017-01-27 |
2019-08-06 |
General Electric Company |
Unitary flow path structure
|
US20180216575A1
(en)
*
|
2017-01-27 |
2018-08-02 |
General Electric Company |
Cool core gas turbine engine
|
US10393381B2
(en)
|
2017-01-27 |
2019-08-27 |
General Electric Company |
Unitary flow path structure
|
US11111858B2
(en)
*
|
2017-01-27 |
2021-09-07 |
General Electric Company |
Cool core gas turbine engine
|
US10378770B2
(en)
|
2017-01-27 |
2019-08-13 |
General Electric Company |
Unitary flow path structure
|
US10253643B2
(en)
|
2017-02-07 |
2019-04-09 |
General Electric Company |
Airfoil fluid curtain to mitigate or prevent flow path leakage
|
US10247019B2
(en)
|
2017-02-23 |
2019-04-02 |
General Electric Company |
Methods and features for positioning a flow path inner boundary within a flow path assembly
|
US10385709B2
(en)
|
2017-02-23 |
2019-08-20 |
General Electric Company |
Methods and features for positioning a flow path assembly within a gas turbine engine
|
US10385776B2
(en)
|
2017-02-23 |
2019-08-20 |
General Electric Company |
Methods for assembling a unitary flow path structure
|
US10378373B2
(en)
|
2017-02-23 |
2019-08-13 |
General Electric Company |
Flow path assembly with airfoils inserted through flow path boundary
|
US10370990B2
(en)
|
2017-02-23 |
2019-08-06 |
General Electric Company |
Flow path assembly with pin supported nozzle airfoils
|
US10253641B2
(en)
|
2017-02-23 |
2019-04-09 |
General Electric Company |
Methods and assemblies for attaching airfoils within a flow path
|
US10577964B2
(en)
|
2017-03-31 |
2020-03-03 |
United Technologies Corporation |
Cooled cooling air for blade air seal through outer chamber
|
US10711640B2
(en)
|
2017-04-11 |
2020-07-14 |
Raytheon Technologies Corporation |
Cooled cooling air to blade outer air seal passing through a static vane
|
US10385731B2
(en)
|
2017-06-12 |
2019-08-20 |
General Electric Company |
CTE matching hanger support for CMC structures
|
US11402097B2
(en)
|
2018-01-03 |
2022-08-02 |
General Electric Company |
Combustor assembly for a turbine engine
|
US10738703B2
(en)
|
2018-03-22 |
2020-08-11 |
Raytheon Technologies Corporation |
Intercooled cooling air with combined features
|
US10808619B2
(en)
|
2018-04-19 |
2020-10-20 |
Raytheon Technologies Corporation |
Intercooled cooling air with advanced cooling system
|
US10830145B2
(en)
|
2018-04-19 |
2020-11-10 |
Raytheon Technologies Corporation |
Intercooled cooling air fleet management system
|
US10718233B2
(en)
|
2018-06-19 |
2020-07-21 |
Raytheon Technologies Corporation |
Intercooled cooling air with low temperature bearing compartment air
|
US11255268B2
(en)
|
2018-07-31 |
2022-02-22 |
Raytheon Technologies Corporation |
Intercooled cooling air with selective pressure dump
|
US11066999B2
(en)
*
|
2019-01-16 |
2021-07-20 |
Raytheon Technologies Corporation |
Fuel cooled cooling air
|
EP3683419A1
(de)
*
|
2019-01-17 |
2020-07-22 |
United Technologies Corporation |
Integrierter kühlluft-boostverdichter und kraftstoffpumpe
|
FR3096444B1
(fr)
*
|
2019-05-20 |
2021-05-07 |
Safran |
Systeme d’echange de chaleur optimise
|
CN112901341B
(zh)
*
|
2019-12-04 |
2022-03-11 |
中国航发商用航空发动机有限责任公司 |
涡轮发动机
|
US11268394B2
(en)
|
2020-03-13 |
2022-03-08 |
General Electric Company |
Nozzle assembly with alternating inserted vanes for a turbine engine
|
US11428160B2
(en)
|
2020-12-31 |
2022-08-30 |
General Electric Company |
Gas turbine engine with interdigitated turbine and gear assembly
|
US11512639B2
(en)
*
|
2021-01-26 |
2022-11-29 |
General Electric Company |
Heat transfer system
|