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AU2001284746A1 - Integrated thermal management and coolant system for an aircraft - Google Patents

Integrated thermal management and coolant system for an aircraft

Info

Publication number
AU2001284746A1
AU2001284746A1 AU2001284746A AU8474601A AU2001284746A1 AU 2001284746 A1 AU2001284746 A1 AU 2001284746A1 AU 2001284746 A AU2001284746 A AU 2001284746A AU 8474601 A AU8474601 A AU 8474601A AU 2001284746 A1 AU2001284746 A1 AU 2001284746A1
Authority
AU
Australia
Prior art keywords
aircraft
thermal management
coolant system
integrated thermal
integrated
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
AU2001284746A
Inventor
Gregory M. Ott
George E. Wilmot Jr.
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hamilton Sundstrand Corp
Original Assignee
Hamilton Sundstrand Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hamilton Sundstrand Corp filed Critical Hamilton Sundstrand Corp
Publication of AU2001284746A1 publication Critical patent/AU2001284746A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F02C7/185—Cooling means for reducing the temperature of the cooling air or gas
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space
    • B64D13/006—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being used to cool structural parts of the aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/34—Conditioning fuel, e.g. heating
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/224—Heating fuel before feeding to the burner
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/50—On board measures aiming to increase energy efficiency
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
AU2001284746A 2000-08-22 2001-08-08 Integrated thermal management and coolant system for an aircraft Abandoned AU2001284746A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09643996 2000-08-22
US09/643,996 US6415595B1 (en) 2000-08-22 2000-08-22 Integrated thermal management and coolant system for an aircraft
PCT/US2001/024756 WO2002016743A1 (en) 2000-08-22 2001-08-08 Integrated thermal management and coolant system for an aircraft

Publications (1)

Publication Number Publication Date
AU2001284746A1 true AU2001284746A1 (en) 2002-03-04

Family

ID=24583014

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001284746A Abandoned AU2001284746A1 (en) 2000-08-22 2001-08-08 Integrated thermal management and coolant system for an aircraft

Country Status (3)

Country Link
US (1) US6415595B1 (en)
AU (1) AU2001284746A1 (en)
WO (1) WO2002016743A1 (en)

Families Citing this family (191)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6796527B1 (en) * 2001-09-20 2004-09-28 Hamilton Sundstrand Corporation Integrated air turbine driven system for providing aircraft environmental control
US6817575B1 (en) * 2001-09-20 2004-11-16 Hamilton Sundstrand Corporation Integrated system for providing aircraft environmental control
US6682016B1 (en) * 2002-09-05 2004-01-27 Hamilton Sundstrand Thermal management valve with drop-tight shutoff of return to tank
US6968674B2 (en) * 2003-01-28 2005-11-29 General Electric Company Methods and apparatus for operating gas turbine engines
US6939392B2 (en) * 2003-04-04 2005-09-06 United Technologies Corporation System and method for thermal management
GB2409001B (en) * 2003-12-13 2006-04-05 Rolls Royce Plc Transferring thermal energy between gas and a fuel in a gas turbine engine
US7260926B2 (en) * 2004-01-20 2007-08-28 United Technologies Corporation Thermal management system for an aircraft
US7013636B2 (en) * 2004-04-22 2006-03-21 The Boeing Company System and method for controlling the temperature and infrared signature of an engine
GB0414341D0 (en) * 2004-06-26 2004-07-28 Honeywell Normalair Garrett Closed loop air conditioning system
US7171819B2 (en) 2005-01-21 2007-02-06 Honeywell International, Inc. Indirect regenerative air cycle for integrated power and cooling machines
FR2889254B1 (en) * 2005-07-28 2011-05-06 Airbus France AIRCRAFT TURBOREACTOR, PROPELLER ASSEMBLY COMPRISING SUCH A TURBOJET ENGINE, AND AIRCRAFT HAVING AT LEAST ONE SUCH A PROPELLER ASSEMBLY
US20070101731A1 (en) * 2005-09-07 2007-05-10 United Technologies Corporation Deoxygenated fuel-cooled environmental control system pre-cooler for an aircraft
EP1795725B1 (en) * 2005-10-12 2011-01-19 Alstom Technology Ltd Gas turbine with controlled air cooling
US7966804B2 (en) * 2006-07-12 2011-06-28 General Electric Company Method and apparatus for testing gas turbine engines
DE102006040191A1 (en) * 2006-08-28 2008-03-13 Airbus Deutschland Gmbh Cooling system for cooling heat loads on board in aircraft, has coupling system to selectively couple two cold carrier fluid circuits coupled to cold producing device and connected to corresponding heat load
FR2914365B1 (en) * 2007-03-28 2012-05-18 Airbus France SYSTEM FOR COOLING AND REGULATING EQUIPMENT TEMPERATURE OF A PROPELLANT AIRCRAFT ASSEMBLY.
EP1975388A1 (en) * 2007-03-28 2008-10-01 Siemens Aktiengesellschaft Gas turbine engine with fuel booster
US20080236939A1 (en) * 2007-03-30 2008-10-02 Hamilton Sundstrand Corporation Exhaust silencer assembly
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
US20090107657A1 (en) * 2007-10-31 2009-04-30 Montminy Jeffrey E Adjustable cooling system for airplane electronics
FR2923462B1 (en) * 2007-11-14 2010-04-02 Airbus France METHOD FOR MANAGING THERMAL REJECTIONS GENERATED BY AN AIRCRAFT AND COOLING DEVICE FOR AN AIRCRAFT FOR CARRYING OUT SAID METHOD.
US8826641B2 (en) * 2008-01-28 2014-09-09 United Technologies Corporation Thermal management system integrated pylon
US9234481B2 (en) * 2008-01-25 2016-01-12 United Technologies Corporation Shared flow thermal management system
KR20100032054A (en) * 2008-09-17 2010-03-25 인제대학교 산학협력단 Apparatus and method for alzheimer's disease diagnosis using eeg(electroencephalogram) analysis
US20100107594A1 (en) * 2008-10-31 2010-05-06 General Electric Company Turbine integrated bleed system and method for a gas turbine engine
DE102008055888A1 (en) * 2008-11-05 2010-05-12 Airbus Deutschland Gmbh System for cooling a heat exchanger on board an aircraft
US20100170262A1 (en) * 2009-01-06 2010-07-08 Kaslusky Scott F Aircraft power and thermal management system with electric co-generation
US8529189B2 (en) * 2009-01-30 2013-09-10 Honeywell International Inc. Linear quadratic regulator control for bleed air system fan air valve
KR20120042713A (en) 2009-02-04 2012-05-03 퍼듀 리서치 파운데이션 Coiled and microchannel heat exchangers for metal hydride storage systems
US8636836B2 (en) 2009-02-04 2014-01-28 Purdue Research Foundation Finned heat exchangers for metal hydride storage systems
US20110302928A1 (en) * 2009-02-27 2011-12-15 Purdue Research Foundation Liquid-gas heat exchanger
US20100242492A1 (en) * 2009-03-30 2010-09-30 Honeywell International Inc. Distributed engine control systems and gas turbine engines
US8234870B2 (en) * 2009-04-17 2012-08-07 Hamilton Sundstrand Corporation Additive injection system for improving thermal stability of jet fuel
US8181669B2 (en) * 2009-05-06 2012-05-22 Hamilton Sundstrand Corporation Compliant check valve stop
US20100313591A1 (en) * 2009-06-12 2010-12-16 Hamilton Sundstrand Corporation Adaptive heat sink for aircraft environmental control system
IL199803A (en) * 2009-07-12 2012-07-31 Lv Technologies Ltd Method and system for enhancing engine performance
US8424285B2 (en) * 2009-07-31 2013-04-23 Hamilton Sundstrand Corporation Cooling system for electronic device in a gas turbine engine system
US20110079286A1 (en) * 2009-10-01 2011-04-07 Hamilton Sundstrand Corporation Expansion Valve
GB2478934B (en) * 2010-03-24 2012-06-13 Rolls Royce Plc Fuel heat management system
WO2011152049A1 (en) 2010-06-03 2011-12-08 パナソニック株式会社 Gas turbine system
US8522572B2 (en) 2010-07-01 2013-09-03 General Electric Company Adaptive power and thermal management system
US8651806B2 (en) 2010-08-17 2014-02-18 Hamilton Sundstrand Corporation Air turbine starter inlet housing assembly airflow path
US8672637B2 (en) 2010-08-17 2014-03-18 Hamilton Sundstrand Corporation Air turbine starter turbine blade airfoil
US8672620B2 (en) 2010-08-17 2014-03-18 Hamilton Sundstrand Corporation Air turbine starter turbine nozzle airfoil
US9028208B2 (en) 2010-08-17 2015-05-12 Hamilton Sundstrand Corporation Air turbine starter turbine nozzle airfoil
US8672638B2 (en) 2010-08-17 2014-03-18 Hamilton Sundstrand Corporation Air turbine starter
EP2622192A2 (en) * 2010-09-30 2013-08-07 General Electric Company Aircraft engine systems and methods for operating same
CA2812250A1 (en) * 2010-09-30 2012-04-05 General Electric Company Dual fuel aircraft system and method for operating same
US20120192578A1 (en) * 2011-01-27 2012-08-02 Hamilton Sundstrand Corporation Gas turbine bleed ecs cooling
US9527593B2 (en) * 2011-04-07 2016-12-27 Hamilton Sundstrand Corporation Thermal accumulator and method of use
US8596568B2 (en) 2011-04-26 2013-12-03 Hamilton Sundstrand Corporation Exhaust silencer with baffles
CA2777997A1 (en) 2011-05-27 2012-11-27 General Electric Company Adaptive power and thermal management system
US8789376B2 (en) 2011-05-27 2014-07-29 General Electric Company Flade duct turbine cooling and power and thermal management
US8943827B2 (en) 2011-05-31 2015-02-03 Pratt & Whitney Canada Corp. Fuel air heat exchanger
US9188380B2 (en) 2011-08-23 2015-11-17 B/E Aerospace, Inc. Aircraft galley liquid cooling system
US9080511B2 (en) 2011-10-21 2015-07-14 United Technologies Corporation Integrated thermal system for a gas turbine engine
US8495857B2 (en) * 2011-10-31 2013-07-30 United Technologies Corporation Gas turbine engine thermal management system
US9334802B2 (en) 2011-10-31 2016-05-10 United Technologies Corporation Gas turbine engine thermal management system
US9328661B2 (en) 2011-11-03 2016-05-03 Northrop Grumman Systems Corporation Apparatus for aircraft with high peak power equipment
US9239005B2 (en) * 2011-11-25 2016-01-19 Pratt & Whitney Canada Corp. Cooling system for engine and aircraft air
WO2013147953A1 (en) * 2011-12-30 2013-10-03 Rolls-Royce North American Technologies Inc. Aircraft propulsion gas turbine engine with heat exchange
US8904805B2 (en) * 2012-01-09 2014-12-09 United Technologies Corporation Environmental control system for aircraft utilizing turbo-compressor
US9109842B2 (en) 2012-02-24 2015-08-18 Pratt & Whitney Canada Corp. Fuel air heat exchanger
US9765694B2 (en) * 2012-08-07 2017-09-19 Unison Industries, Llc Gas turbine engine heat exchangers and methods of assembling the same
GB201217332D0 (en) 2012-09-28 2012-11-14 Rolls Royce Plc A gas turbine engine
US9561857B2 (en) 2013-02-06 2017-02-07 Raytheon Company Aircraft thermal management system for cooling using expendable coolants
WO2014151685A1 (en) 2013-03-15 2014-09-25 United Technologies Corporation Gas turbine engine with air-oil cooler oil tank
BR112015023299A2 (en) * 2013-03-15 2017-07-18 Gen Electric Cryogenic fuel usage method and fuel vaporization system
US9255645B2 (en) 2013-04-03 2016-02-09 Hamilton Sundstrand Corporation Reconfigurable valve
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
US9644898B2 (en) 2013-07-09 2017-05-09 The Boeing Company Systems and methods for heat balance and transport for aircraft hydraulic systems
US9644648B2 (en) 2013-07-09 2017-05-09 The Boeing Company Systems and methods for heat balance and transport for aircraft hydraulic systems
US10054051B2 (en) * 2014-04-01 2018-08-21 The Boeing Company Bleed air systems for use with aircraft and related methods
US9810158B2 (en) * 2014-04-01 2017-11-07 The Boeing Company Bleed air systems for use with aircraft and related methods
US9963994B2 (en) * 2014-04-08 2018-05-08 General Electric Company Method and apparatus for clearance control utilizing fuel heating
US10400674B2 (en) * 2014-05-09 2019-09-03 United Technologies Corporation Cooled fuel injector system for a gas turbine engine and method for operating the same
US10344677B2 (en) * 2014-05-29 2019-07-09 General Electric Company Systems and methods for preheating fuel for gas turbine engines
EP3164577A1 (en) 2014-07-03 2017-05-10 General Electric Company Jet engine cold air cooling system
EP2998223B1 (en) * 2014-09-19 2018-12-05 Airbus Operations GmbH Aircraft air conditioning system and method of operating an aircraft air conditioning system
US9657648B2 (en) 2014-11-25 2017-05-23 Hamilton Sundstrand Corporation Environmental air conditioning system
US9828887B2 (en) 2015-03-19 2017-11-28 General Electric Company Power generation system having compressor creating excess air flow and turbo-expander to increase turbine exhaust gas mass flow
US20160273396A1 (en) * 2015-03-19 2016-09-22 General Electric Company Power generation system having compressor creating excess air flow and heat exchanger therefor
US9863284B2 (en) 2015-03-19 2018-01-09 General Electric Company Power generation system having compressor creating excess air flow and cooling fluid injection therefor
US9822670B2 (en) 2015-03-19 2017-11-21 General Electric Company Power generation system having compressor creating excess air flow and turbo-expander for cooling inlet air
US9828870B2 (en) * 2015-06-11 2017-11-28 Northrop Grumman Systems Corporation Efficient power and thermal management system for high performance aircraft
US10100744B2 (en) 2015-06-19 2018-10-16 The Boeing Company Aircraft bleed air and engine starter systems and related methods
US10260419B2 (en) * 2015-07-31 2019-04-16 General Electric Company Cooling system
US10578028B2 (en) * 2015-08-18 2020-03-03 General Electric Company Compressor bleed auxiliary turbine
US10711702B2 (en) 2015-08-18 2020-07-14 General Electric Company Mixed flow turbocore
US10207809B2 (en) * 2015-08-31 2019-02-19 Honeywell International Inc. Integrated air and vapor cycle cooling system
US9534538B1 (en) * 2015-10-27 2017-01-03 General Electric Company Systems and methods for integrated power and thermal management in a turbine-powered aircraft
US10215097B2 (en) 2015-12-08 2019-02-26 General Electric Company Thermal management system
US10823066B2 (en) * 2015-12-09 2020-11-03 General Electric Company Thermal management system
US10697371B2 (en) 2015-12-28 2020-06-30 General Electric Company Method and system for a combined air-oil cooler and fuel-oil cooler heat exchanger
EP3187418A1 (en) * 2015-12-30 2017-07-05 Airbus Operations S.L. Air conditioning system
US10173780B2 (en) * 2016-01-26 2019-01-08 The Boeing Company Aircraft liquid heat exchanger anti-icing system
US20170217592A1 (en) * 2016-02-01 2017-08-03 General Electric Company Aircraft Thermal Management System
US10087777B2 (en) 2016-04-29 2018-10-02 Hamilton Sundstrand Corporation Lubricant cooling systems for high speed turbomachines
DE102016219680A1 (en) * 2016-10-11 2018-04-12 Siemens Aktiengesellschaft Drive system for a vehicle with internal combustion engine and fuel tank
US11052328B2 (en) * 2016-10-25 2021-07-06 Delavan Inc. Fuel stabilization systems
CN106762155B (en) * 2016-12-15 2021-06-01 中国航空工业集团公司西安飞机设计研究所 A turbo-compressor-based inverse booster air source system
US10429107B2 (en) * 2017-01-12 2019-10-01 Honeywell International Inc. Simplified recuperating electric ECS
US20180215475A1 (en) * 2017-02-01 2018-08-02 General Electric Company Systems and Methods for Integrated Power and Thermal Management in a Turbine-Powered Aircraft
US10752374B1 (en) * 2017-03-15 2020-08-25 Northrop Grumman Systems Corporation Active fuel thermal conditioning for aircraft
US11008115B2 (en) 2017-05-09 2021-05-18 Gulfstream Aerospace Corporation Fuel system for an aircraft
US20190041145A1 (en) * 2017-08-01 2019-02-07 Hamilton Sundstrand Corporation Three-way modulating valve for temperature control
US11187156B2 (en) 2017-11-21 2021-11-30 General Electric Company Thermal management system
US11125165B2 (en) * 2017-11-21 2021-09-21 General Electric Company Thermal management system
US11022037B2 (en) 2018-01-04 2021-06-01 General Electric Company Gas turbine engine thermal management system
US10941706B2 (en) 2018-02-13 2021-03-09 General Electric Company Closed cycle heat engine for a gas turbine engine
US11143104B2 (en) 2018-02-20 2021-10-12 General Electric Company Thermal management system
JP2019163761A (en) * 2018-03-20 2019-09-26 パナソニックＩｐマネジメント株式会社 Gas turbine system
US11174789B2 (en) 2018-05-23 2021-11-16 General Electric Company Air cycle assembly for a gas turbine engine assembly
US10954865B2 (en) 2018-06-19 2021-03-23 The Boeing Company Pressurized air systems for aircraft and related methods
US10801509B2 (en) * 2018-07-26 2020-10-13 Honeywell International Inc. Bleed air selector valve
US11077949B2 (en) * 2018-10-05 2021-08-03 The Boeing Company Dual turbine thermal management system (TMS)
US20200130858A1 (en) * 2018-10-29 2020-04-30 Pratt & Whitney Canada Corp. Method and system for cooling an auxiliary power unit using aircraft fuel
US11447263B2 (en) 2018-11-02 2022-09-20 General Electric Company Fuel oxygen reduction unit control system
US11161622B2 (en) 2018-11-02 2021-11-02 General Electric Company Fuel oxygen reduction unit
US11851204B2 (en) 2018-11-02 2023-12-26 General Electric Company Fuel oxygen conversion unit with a dual separator pump
US11193671B2 (en) 2018-11-02 2021-12-07 General Electric Company Fuel oxygen conversion unit with a fuel gas separator
US11186382B2 (en) 2018-11-02 2021-11-30 General Electric Company Fuel oxygen conversion unit
US11148824B2 (en) 2018-11-02 2021-10-19 General Electric Company Fuel delivery system having a fuel oxygen reduction unit
US11319085B2 (en) 2018-11-02 2022-05-03 General Electric Company Fuel oxygen conversion unit with valve control
US11577852B2 (en) 2018-11-02 2023-02-14 General Electric Company Fuel oxygen conversion unit
US11131256B2 (en) 2018-11-02 2021-09-28 General Electric Company Fuel oxygen conversion unit with a fuel/gas separator
US11420763B2 (en) 2018-11-02 2022-08-23 General Electric Company Fuel delivery system having a fuel oxygen reduction unit
US11085636B2 (en) 2018-11-02 2021-08-10 General Electric Company Fuel oxygen conversion unit
JP7120893B2 (en) * 2018-11-20 2022-08-17 三菱重工業株式会社 Gas turbine and its extraction amount adjustment method
US11015534B2 (en) 2018-11-28 2021-05-25 General Electric Company Thermal management system
US11391211B2 (en) 2018-11-28 2022-07-19 General Electric Company Waste heat recovery system
US11465757B2 (en) * 2018-12-06 2022-10-11 The Boeing Company Systems and methods to produce aircraft cabin supply air
US20200180771A1 (en) * 2018-12-06 2020-06-11 General Electric Company Thermal Management System for an Aircraft Including an Electric Propulsion Engine
CN109611212B (en) * 2018-12-10 2021-05-04 中国航发四川燃气涡轮研究院 Take aircraft engine thermal management system of hot oil tank returnable oil
US11066999B2 (en) 2019-01-16 2021-07-20 Raytheon Technologies Corporation Fuel cooled cooling air
US11067000B2 (en) 2019-02-13 2021-07-20 General Electric Company Hydraulically driven local pump
EP3708495B1 (en) * 2019-03-11 2021-11-17 Airbus SAS Aircraft propulsion system including a heat exchanger system
EP3726028B1 (en) 2019-04-17 2024-07-24 RTX Corporation Multiple stream heat exchanger
US10927761B2 (en) 2019-04-17 2021-02-23 General Electric Company Refreshing heat management fluid in a turbomachine
US11286857B2 (en) * 2019-04-29 2022-03-29 Hamilton Sundstrand Corporation Turbine-turbine generator power thermal management system
CN110094267B (en) * 2019-06-04 2024-11-29 江苏蓝芯航空航天科技有限公司 High-altitude fuel oil supply system of micro aviation turbine engine
US10914274B1 (en) 2019-09-11 2021-02-09 General Electric Company Fuel oxygen reduction unit with plasma reactor
US11774427B2 (en) 2019-11-27 2023-10-03 General Electric Company Methods and apparatus for monitoring health of fuel oxygen conversion unit
US11906163B2 (en) 2020-05-01 2024-02-20 General Electric Company Fuel oxygen conversion unit with integrated water removal
US11773776B2 (en) 2020-05-01 2023-10-03 General Electric Company Fuel oxygen reduction unit for prescribed operating conditions
US11866182B2 (en) 2020-05-01 2024-01-09 General Electric Company Fuel delivery system having a fuel oxygen reduction unit
US20220145796A1 (en) * 2020-11-06 2022-05-12 Ge Aviation Systems Llc Combustion engine including turbomachine
EP4001599B8 (en) * 2020-11-23 2023-04-12 The Boeing Company Methods and systems for generating power and thermal management having combined cycle architecture
US11492970B2 (en) 2020-12-21 2022-11-08 General Electric Company Thermal management system with fuel cooling
US11560239B2 (en) 2020-12-21 2023-01-24 General Electric Company Regenerative thermal management system
US12196136B2 (en) 2020-12-21 2025-01-14 General Electric Company Regenerative fuel heating system
US20220213802A1 (en) 2021-01-06 2022-07-07 General Electric Company System for controlling blade clearances within a gas turbine engine
US11434824B2 (en) 2021-02-03 2022-09-06 General Electric Company Fuel heater and energy conversion system
EP4056475B1 (en) * 2021-03-10 2023-04-26 Airbus Operations (S.A.S.) Aircraft including an engine and a cooling system
US11591965B2 (en) 2021-03-29 2023-02-28 General Electric Company Thermal management system for transferring heat between fluids
US12139270B2 (en) 2021-04-19 2024-11-12 General Electric Company Aircraft thermal transport system and method
US12115470B2 (en) 2021-04-27 2024-10-15 General Electric Company Fuel oxygen reduction unit
US11773781B2 (en) * 2021-06-11 2023-10-03 Pratt & Whitney Canada Corp. Means for handling gaseous fuel
US12005377B2 (en) 2021-06-15 2024-06-11 General Electric Company Fuel oxygen reduction unit with level control device
US11674396B2 (en) 2021-07-30 2023-06-13 General Electric Company Cooling air delivery assembly
US11920500B2 (en) 2021-08-30 2024-03-05 General Electric Company Passive flow modulation device
CN114151137B (en) * 2021-10-20 2023-09-05 中国航发四川燃气涡轮研究院 Combined cooling thermal management system for high Mach number aeroengine cabin and turbine disk
US11542870B1 (en) 2021-11-24 2023-01-03 General Electric Company Gas supply system
US11692448B1 (en) 2022-03-04 2023-07-04 General Electric Company Passive valve assembly for a nozzle of a gas turbine engine
EP4245664A1 (en) * 2022-03-16 2023-09-20 MTU Aero Engines AG Aircraft propulsion and method for operating an aircraft propulsion
US11946378B2 (en) 2022-04-13 2024-04-02 General Electric Company Transient control of a thermal transport bus
US11702985B1 (en) 2022-04-19 2023-07-18 General Electric Company Thermal management system
US11761344B1 (en) 2022-04-19 2023-09-19 General Electric Company Thermal management system
CN114704382A (en) * 2022-04-24 2022-07-05 中国航发沈阳发动机研究所 Aircraft engine thermal management method and architecture
FR3134849B1 (en) * 2022-04-26 2025-02-21 Safran System for controlling the temperature of a heat transfer fluid in a circulation loop, temperature control method
FR3134850B1 (en) * 2022-04-26 2025-03-07 Safran System for controlling the temperature of a heat transfer fluid in a circulation loop, temperature control method
US11927142B2 (en) 2022-07-25 2024-03-12 General Electric Company Systems and methods for controlling fuel coke formation
GB2622209B (en) * 2022-09-06 2024-12-04 Rolls Royce Plc A thermal management system for an aircraft
GB2622215B (en) 2022-09-06 2024-12-04 Rolls Royce Plc A thermal management system for an aircraft
US11898495B1 (en) 2022-09-16 2024-02-13 General Electric Company Hydrogen fuel system for a gas turbine engine
US11905884B1 (en) 2022-09-16 2024-02-20 General Electric Company Hydrogen fuel system for a gas turbine engine
US11873768B1 (en) 2022-09-16 2024-01-16 General Electric Company Hydrogen fuel system for a gas turbine engine
US12392290B2 (en) 2022-11-01 2025-08-19 General Electric Company Gas turbine engine
US12503980B2 (en) 2022-11-01 2025-12-23 General Electric Company Gas turbine engine
US12196131B2 (en) 2022-11-01 2025-01-14 General Electric Company Gas turbine engine
US12410753B2 (en) 2022-11-01 2025-09-09 General Electric Company Gas turbine engine
US12428992B2 (en) 2022-11-01 2025-09-30 General Electric Company Gas turbine engine
CN116534263B (en) * 2023-07-04 2023-09-22 中国航空工业集团公司金城南京机电液压工程研究中心 Aircraft step heat dissipation device and control method
DE102023130791A1 (en) * 2023-11-07 2025-05-08 MTU Aero Engines AG Aircraft propulsion system and method for operating an aircraft propulsion system
WO2025196403A1 (en) * 2024-03-19 2025-09-25 Bae Systems Plc Supplying a flow of compressed air
EP4620818A1 (en) * 2024-03-19 2025-09-24 BAE SYSTEMS plc Supplying a flow of compressed air
US12291997B1 (en) 2024-04-30 2025-05-06 General Electric Company Variable area turbine nozzle assembly
CN119641482B (en) * 2024-12-24 2025-09-09 中国航空工业集团公司金城南京机电液压工程研究中心 Thermal management type combined power system, aircraft and control method
US12523177B1 (en) * 2025-01-10 2026-01-13 Rtx Corporation Electronic controller cooling for aircraft propulsion system

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4474001A (en) 1981-04-01 1984-10-02 United Technologies Corporation Cooling system for the electrical generator of a turbofan gas turbine engine
GB2095756B (en) 1982-03-05 1985-01-16 United Technologies Corp Balancing the heat flow between components associated with a gas turbine engine
GB2131094A (en) 1982-11-29 1984-06-13 Gen Electric Engine oil heat recovery system
US4505124A (en) 1983-09-22 1985-03-19 The United States Of America As Represented By The Secretary Of The Air Force Heat management system for aircraft
US4696156A (en) 1986-06-03 1987-09-29 United Technologies Corporation Fuel and oil heat management system for a gas turbine engine
US4991394A (en) 1989-04-03 1991-02-12 Allied-Signal Inc. High performance turbine engine
US5014518A (en) 1989-06-23 1991-05-14 Allied-Signal Inc. ECS with advanced air cycle machine
US5299763A (en) 1991-12-23 1994-04-05 Allied-Signal Inc. Aircraft cabin air conditioning system with improved fresh air supply
US5392595A (en) * 1993-08-06 1995-02-28 United Technologies Corporation Endothermic fuel energy management system
US5414992A (en) 1993-08-06 1995-05-16 United Technologies Corporation Aircraft cooling method
US5452573A (en) * 1994-01-31 1995-09-26 United Technologies Corporation High pressure air source for aircraft and engine requirements
US6182435B1 (en) * 1997-06-05 2001-02-06 Hamilton Sundstrand Corporation Thermal and energy management method and apparatus for an aircraft
US5967461A (en) 1997-07-02 1999-10-19 Mcdonnell Douglas Corp. High efficiency environmental control systems and methods
US6735953B1 (en) 1997-12-22 2004-05-18 Allied Signal Inc. Turbomachine-driven environmental control system
FR2788308A1 (en) * 1999-01-07 2000-07-13 Snecma COOLING DEVICE FOR A TURBOMACHINE SPEED REDUCER

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