|
FR2788308A1
(fr)
*
|
1999-01-07 |
2000-07-13 |
Snecma |
Dispositif de refroidissement d'un reducteur de vitesse de turbomachine
|
|
CA2329555A1
(en)
*
|
2000-12-22 |
2002-06-22 |
Jose Albero |
Main propulsion engine system integrated with secondary power unit
|
|
US6575406B2
(en)
*
|
2001-01-19 |
2003-06-10 |
The Boeing Company |
Integrated and/or modular high-speed aircraft
|
|
CA99703S
(en)
|
2001-03-22 |
2002-10-10 |
Boeing Co |
Airplane
|
|
AU148311S
(en)
|
2001-03-22 |
2002-07-01 |
Boeing Co |
Supersonic aircraft
|
|
US6615576B2
(en)
*
|
2001-03-29 |
2003-09-09 |
Honeywell International Inc. |
Tortuous path quiet exhaust eductor system
|
|
US6580179B2
(en)
|
2001-06-07 |
2003-06-17 |
Honeywell International Inc. |
Ram air turbine with high power density generator and self-contained fluid cooling loop
|
|
US6651929B2
(en)
*
|
2001-10-29 |
2003-11-25 |
Pratt & Whitney Canada Corp. |
Passive cooling system for auxiliary power unit installation
|
|
DE10200459A1
(de)
*
|
2002-01-09 |
2003-07-24 |
Airbus Gmbh |
Lufteinlauf für ein Hilfstriebwerk in einem Flugzeug
|
|
US7644888B2
(en)
*
|
2002-05-15 |
2010-01-12 |
The Boeing Company |
High-speed aircraft and methods for their manufacture
|
|
US6651928B1
(en)
|
2002-09-05 |
2003-11-25 |
The Boeing Company |
Aircraft engine nacelles and methods for their manufacture
|
|
US7210653B2
(en)
*
|
2002-10-22 |
2007-05-01 |
The Boeing Company |
Electric-based secondary power system architectures for aircraft
|
|
US6851255B2
(en)
|
2002-12-18 |
2005-02-08 |
Pratt & Whitney Canada Corp. |
Normally open reverse flow flapper valve
|
|
US7337605B2
(en)
*
|
2003-10-10 |
2008-03-04 |
Hamilton Sundstrand Corporation |
Thermal management for aircraft auxiliary power unit compartment
|
|
US7150431B2
(en)
*
|
2004-01-14 |
2006-12-19 |
Mjd Innovations, L.L.C. |
Electrical generator fluid-flow-coolant filtration
|
|
US20050200858A1
(en)
*
|
2004-01-28 |
2005-09-15 |
Hamilton Sundstrand Corporation |
Contoured inspection plug for low pressure drop
|
|
US7231767B2
(en)
*
|
2004-04-16 |
2007-06-19 |
Pratt & Whitney Canada Corp. |
Forced air cooling system
|
|
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
|
|
US20060032974A1
(en)
*
|
2004-08-16 |
2006-02-16 |
Honeywell International Inc. |
Modular installation kit for auxiliary power unit
|
|
US7377100B2
(en)
*
|
2004-08-27 |
2008-05-27 |
Pratt & Whitney Canada Corp. |
Bypass duct fluid cooler
|
|
US7267297B2
(en)
*
|
2004-09-02 |
2007-09-11 |
The Boeing Company |
Integrated axially varying engine muffler, and associated methods and systems
|
|
US20060059891A1
(en)
*
|
2004-09-23 |
2006-03-23 |
Honeywell International, Inc. |
Quiet chevron/tab exhaust eductor system
|
|
US7364116B2
(en)
*
|
2004-09-27 |
2008-04-29 |
The Boeing Company |
Automatic control systems for aircraft auxiliary power units, and associated methods
|
|
US7344107B2
(en)
*
|
2004-10-26 |
2008-03-18 |
The Boeing Company |
Dual flow APU inlet and associated systems and methods
|
|
US8127527B2
(en)
*
|
2004-11-22 |
2012-03-06 |
General Electric Company |
Methods and systems for operating oxidizer systems
|
|
US20060157613A1
(en)
*
|
2005-01-19 |
2006-07-20 |
Adamson Eric E |
Supersonic aircraft with active lift distribution control for reducing sonic boom
|
|
US20060163425A1
(en)
*
|
2005-01-27 |
2006-07-27 |
Honeywell International, Inc. |
Aircraft inlet assembly for reducing auxiliary power unit noise
|
|
US7513119B2
(en)
*
|
2005-02-03 |
2009-04-07 |
The Boeing Company |
Systems and methods for starting aircraft engines
|
|
US7698896B2
(en)
*
|
2005-07-27 |
2010-04-20 |
Honeywell International Inc. |
Compact, light weight eductor oil cooler plenum and surge flow plenum design
|
|
US8371521B2
(en)
*
|
2006-03-16 |
2013-02-12 |
Pratt & Whitney |
Low noise exhaust ducting system
|
|
US7600714B2
(en)
*
|
2006-04-20 |
2009-10-13 |
Honeywell International Inc. |
Diffusing air inlet door assembly
|
|
US7861512B2
(en)
*
|
2006-08-29 |
2011-01-04 |
Pratt & Whitney Canada Corp. |
Turbofan bypass duct air cooled fluid cooler installation
|
|
US20080053060A1
(en)
*
|
2006-08-29 |
2008-03-06 |
Pratt & Whitney Canada Corp. |
Bypass lip seal
|
|
US7857257B2
(en)
*
|
2006-09-01 |
2010-12-28 |
United Technologies Corporation |
Aircraft thermal management system with reduced exhaust re-ingestion
|
|
DE102006042584B4
(de)
*
|
2006-09-11 |
2008-11-20 |
Airbus Deutschland Gmbh |
Luftzufuhrsystem eines Flugzeuges sowie Verfahren zum Vermischen zweier Luftströme in einem Luftzufuhrsystem
|
|
US7690598B1
(en)
*
|
2006-09-11 |
2010-04-06 |
Plattner Wesley M |
Aircraft exhaust vent assembly
|
|
US7765784B2
(en)
*
|
2006-09-25 |
2010-08-03 |
The Boeing Company |
Thermally compliant APU exhaust duct arrangements and associated systems and methods
|
|
US20080203218A1
(en)
*
|
2007-02-26 |
2008-08-28 |
Honeywell International, Inc. |
Systems And Methods For Reducing Pressure Loss Of Air Flowing From A First Area To A Second Area
|
|
US20080236939A1
(en)
*
|
2007-03-30 |
2008-10-02 |
Hamilton Sundstrand Corporation |
Exhaust silencer assembly
|
|
US7862293B2
(en)
*
|
2007-05-03 |
2011-01-04 |
Pratt & Whitney Canada Corp. |
Low profile bleed air cooler
|
|
US9194293B2
(en)
*
|
2007-09-18 |
2015-11-24 |
Hamilton Sundstrand Corporation |
Air inlet noise attenuation assembly
|
|
US7578369B2
(en)
*
|
2007-09-25 |
2009-08-25 |
Hamilton Sundstrand Corporation |
Mixed-flow exhaust silencer assembly
|
|
DE102007061588B4
(de)
*
|
2007-12-20 |
2011-07-21 |
Airbus Operations GmbH, 21129 |
Flugzeugkühlsystem
|
|
US20100005806A1
(en)
|
2008-07-14 |
2010-01-14 |
Donnelly Brian G |
Eductor system for a gas turbine engine
|
|
US8181443B2
(en)
*
|
2008-12-10 |
2012-05-22 |
Pratt & Whitney Canada Corp. |
Heat exchanger to cool turbine air cooling flow
|
|
US8245494B2
(en)
*
|
2009-02-12 |
2012-08-21 |
Hamilton Sundstrand Corporation |
Gas turbine engine with eductor and eductor flow distribution shield
|
|
DE102009013159A1
(de)
*
|
2009-03-16 |
2010-09-23 |
Airbus Operations Gmbh |
Kühler für ein Flugzeugkühlsystem, Flugzeugkühlsystem und Verfahren zum Betreiben eines Flugzeugkühlsystems
|
|
US8657227B1
(en)
|
2009-09-11 |
2014-02-25 |
The Boeing Company |
Independent power generation in aircraft
|
|
US8621842B2
(en)
|
2010-05-05 |
2014-01-07 |
Hamilton Sundstrand Corporation |
Exhaust silencer convection cooling
|
|
US8602717B2
(en)
|
2010-10-28 |
2013-12-10 |
United Technologies Corporation |
Compression system for turbomachine heat exchanger
|
|
US8738268B2
(en)
|
2011-03-10 |
2014-05-27 |
The Boeing Company |
Vehicle electrical power management and distribution
|
|
US8596568B2
(en)
|
2011-04-26 |
2013-12-03 |
Hamilton Sundstrand Corporation |
Exhaust silencer with baffles
|
|
US8973552B2
(en)
|
2011-06-27 |
2015-03-10 |
United Technologies Corporation |
Integral oil system
|
|
US9188065B2
(en)
|
2011-08-03 |
2015-11-17 |
Hamilton Sundstrand Corporation |
APU selective cool down cycle
|
|
US9254924B2
(en)
|
2011-08-12 |
2016-02-09 |
Hamilton Sundstrand Corporation |
Pressure influencing assembly for an aircraft auxiliary system
|
|
FR2986275B1
(fr)
*
|
2012-02-01 |
2016-07-01 |
Turbomeca |
Procede d'ejection de gaz d'echappement de turbine a gaz et ensemble d'echappement de configuration optimisee
|
|
US9279386B2
(en)
|
2012-03-09 |
2016-03-08 |
Hamilton Sundstrand Corporation |
Jet noise reduction using eduction effect
|
|
CN102673793B
(zh)
*
|
2012-06-08 |
2015-04-29 |
中国航空工业集团公司西安飞机设计研究所 |
一种飞机辅助动力装置排气引射系统
|
|
US9097134B2
(en)
|
2012-09-14 |
2015-08-04 |
Pratt & Whitney Canada Corp. |
Air cooling design for tail-cone generator installation
|
|
US9458764B2
(en)
|
2012-11-26 |
2016-10-04 |
Pratt & Whitney Canada Corp. |
Air cooled air cooler for gas turbine engine air system
|
|
US9611050B2
(en)
|
2013-07-26 |
2017-04-04 |
The Boeing Company |
Auxiliary power unit inlet apparatus and methods
|
|
US9541030B2
(en)
*
|
2013-11-27 |
2017-01-10 |
Lockheed Martin Corporation |
Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices
|
|
DE102014208154A1
(de)
*
|
2014-04-30 |
2015-11-05 |
Airbus Operations Gmbh |
Flugzeugheckbereich mit einem Kühlsystem und Verfahren zur Kühlung einer wärmeerzeugenden Vorrichtung
|
|
GB201416407D0
(en)
|
2014-09-17 |
2014-10-29 |
Rolls Royce Plc |
Aircraft environmental control system air duct arrangement
|
|
US10240522B2
(en)
*
|
2015-08-07 |
2019-03-26 |
Pratt & Whitney Canada Corp. |
Auxiliary power unit with combined cooling of generator
|
|
US10253726B2
(en)
|
2015-08-07 |
2019-04-09 |
Pratt & Whitney Canada Corp. |
Engine assembly with combined engine and cooling exhaust
|
|
US11105340B2
(en)
|
2016-08-19 |
2021-08-31 |
General Electric Company |
Thermal management system for an electric propulsion engine
|
|
US10676205B2
(en)
|
2016-08-19 |
2020-06-09 |
General Electric Company |
Propulsion engine for an aircraft
|
|
US10800539B2
(en)
*
|
2016-08-19 |
2020-10-13 |
General Electric Company |
Propulsion engine for an aircraft
|
|
US10670178B2
(en)
|
2017-04-19 |
2020-06-02 |
General Electric Company |
Slip joint assembly
|
|
US10415502B2
(en)
|
2017-09-11 |
2019-09-17 |
Honeywell International Inc. |
Swirling flow eductor system and method
|
|
ES2890374T3
(es)
*
|
2017-10-30 |
2022-01-18 |
Airbus Operations Sl |
Cono de cola de aeronave que incorpora una APU con admisión de aire anular
|
|
US20190218972A1
(en)
*
|
2018-01-18 |
2019-07-18 |
General Electric Company |
Thermally protected thermoplastic duct and assembly
|
|
FR3079820B1
(fr)
*
|
2018-04-09 |
2020-04-17 |
Safran Electrical & Power |
Systeme et procede de demarrage/generation pour turbomachine d'aeronef
|
|
US11085372B2
(en)
*
|
2018-07-18 |
2021-08-10 |
The Boeing Company |
Anti-ice system exhaust air disruptor
|
|
US11156128B2
(en)
|
2018-08-22 |
2021-10-26 |
General Electric Company |
Embedded electric machine
|
|
CN109573074A
(zh)
*
|
2018-11-30 |
2019-04-05 |
中国航空工业集团公司金城南京机电液压工程研究中心 |
一种用于飞机辅助动力装置的滑油冷却系统
|
|
US20200180771A1
(en)
|
2018-12-06 |
2020-06-11 |
General Electric Company |
Thermal Management System for an Aircraft Including an Electric Propulsion Engine
|
|
JP7143904B2
(ja)
*
|
2019-02-13 |
2022-09-29 |
株式会社Ihi |
航空機用ガスタービンエンジンの冷却システム
|
|
US12179934B2
(en)
*
|
2019-05-06 |
2024-12-31 |
The Boeing Company |
Method and apparatus for auxiliary power unit installation
|
|
US10967983B2
(en)
|
2019-06-05 |
2021-04-06 |
Pratt & Whitney Canada Corp. |
Aircraft power plant
|
|
US10875660B1
(en)
|
2019-06-05 |
2020-12-29 |
Pratt & Whitney Canada Corp. |
Aircraft power plant
|
|
US11300053B2
(en)
|
2019-10-02 |
2022-04-12 |
Honeywell International Inc. |
Passive flame arrestor system
|
|
CN110901930A
(zh)
*
|
2019-12-06 |
2020-03-24 |
西安爱生技术集团公司 |
一种活塞发动机后置通风冷却装置
|
|
US11352885B2
(en)
|
2020-04-08 |
2022-06-07 |
Pratt & Whitney Canada Corp. |
Aircraft power plant cooling system
|
|
US11578621B2
(en)
|
2020-04-08 |
2023-02-14 |
General Electric Company |
System for cooling turbine shaft coupling
|
|
US12149154B2
(en)
|
2021-07-22 |
2024-11-19 |
General Electric Company |
Electric machine having a hybrid insulative-conductive manifold
|
|
ES2988133T3
(es)
*
|
2021-09-28 |
2024-11-19 |
Airbus Operations Slu |
Aeronave con motor de combustión que tiene el escape delante de la admisión de aire
|
|
JP7496812B2
(ja)
|
2021-12-28 |
2024-06-07 |
本田技研工業株式会社 |
ミキサ及び移動体
|
|
US20240017841A1
(en)
*
|
2022-07-15 |
2024-01-18 |
Pratt & Whitney Canada Corp. |
Aircraft propulsion system with intermittent combustion engine(s)
|
|
US12366217B2
(en)
|
2022-12-21 |
2025-07-22 |
General Electric Company |
Electric machine assembly
|
|
US12372010B1
(en)
*
|
2024-01-26 |
2025-07-29 |
Rtx Corporation |
Passive ventilation system for tail cone zone
|