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BRPI0818111A2 - Processo de gerenciamento dos efluentes térmicos de uma aernave, dispositivo de resfriamento de uma aeronave e aeronave. - Google Patents

Processo de gerenciamento dos efluentes térmicos de uma aernave, dispositivo de resfriamento de uma aeronave e aeronave.

Info

Publication number
BRPI0818111A2
BRPI0818111A2 BRPI0818111A BRPI0818111A2 BR PI0818111 A2 BRPI0818111 A2 BR PI0818111A2 BR PI0818111 A BRPI0818111 A BR PI0818111A BR PI0818111 A2 BRPI0818111 A2 BR PI0818111A2
Authority
BR
Brazil
Prior art keywords
aircraft
managing
cooling device
effluents
thermal
Prior art date
Application number
Other languages
English (en)
Inventor
Guillaume Bulin
Jan Dittmar
Original Assignee
Airbus Gmbh
Jan Dittmar
Airbus Operations Sas
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 Airbus Gmbh, Jan Dittmar, Airbus Operations Sas filed Critical Airbus Gmbh
Publication of BRPI0818111A2 publication Critical patent/BRPI0818111A2/pt

Links

Classifications

    • 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
    • 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/08—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
    • B64D33/10—Radiator arrangement
    • 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
    • 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
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being conditioned
    • B64D2013/0603—Environmental Control Systems
    • B64D2013/0614—Environmental Control Systems with subsystems for cooling avionics
    • 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
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being conditioned
    • B64D2013/0603—Environmental Control Systems
    • B64D2013/0659—Environmental Control Systems comprising provisions for cooling fuel systems
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Fuel Cell (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
BRPI0818111 2007-11-14 2008-11-12 Processo de gerenciamento dos efluentes térmicos de uma aernave, dispositivo de resfriamento de uma aeronave e aeronave. BRPI0818111A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0759043A FR2923462B1 (fr) 2007-11-14 2007-11-14 Procede de gestion des rejections thermiques generees par un aeronef et dispositif de refroidissement pour aeronef permettant la mise en oeuvre dudit procede.
PCT/FR2008/052028 WO2009068807A2 (fr) 2007-11-14 2008-11-12 Procede de gestion des rejections thermiques generees par un aeronef et dispositif de refroidissement pour aeronef permettant la mise en oeuvre dudit procede

Publications (1)

Publication Number Publication Date
BRPI0818111A2 true BRPI0818111A2 (pt) 2015-03-31

Family

ID=39512751

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0818111 BRPI0818111A2 (pt) 2007-11-14 2008-11-12 Processo de gerenciamento dos efluentes térmicos de uma aernave, dispositivo de resfriamento de uma aeronave e aeronave.

Country Status (9)

Country Link
US (1) US8677755B2 (pt)
EP (1) EP2209716B1 (pt)
JP (1) JP2011502878A (pt)
CN (1) CN101970298A (pt)
BR (1) BRPI0818111A2 (pt)
CA (1) CA2705611C (pt)
FR (1) FR2923462B1 (pt)
RU (1) RU2478805C2 (pt)
WO (1) WO2009068807A2 (pt)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2416009A (en) * 2004-05-12 2006-01-11 Dunlop Aerospace Ltd Hydraulic fluid control apparatus
FR2936224B1 (fr) * 2008-09-25 2012-07-13 Airbus France Systeme de gestion des flux thermiques d'un aeronef.
DE102009039814A1 (de) * 2009-09-02 2011-03-10 Airbus Operations Gmbh System und Verfahren zum Kühlen mindestens einer Wärme erzeugenden Einrichtung in einem Flugzeug
FR2951228B1 (fr) * 2009-10-13 2013-07-19 Snecma Procede et systeme de gestion d'echanges thermiques entre fluides dans une turbomachine
US20130048134A1 (en) 2011-08-25 2013-02-28 The Boeing Company Stagnant Fuel Thermal Insulation System
CN102517598B (zh) * 2011-12-02 2014-11-26 北京工业大学 一种利用内燃机冷却液能量加热制氢机水罐的装置及方法
US20130255281A1 (en) * 2012-03-29 2013-10-03 General Electric Company System and method for cooling electrical components
EP2724934B1 (en) * 2012-10-26 2016-09-21 AGUSTAWESTLAND S.p.A. Hover-capable aircraft
RU2572513C2 (ru) * 2013-09-11 2016-01-20 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Теплообменный модуль системы кондиционирования воздуха самолета
US10676206B2 (en) 2017-12-08 2020-06-09 Pratt & Whitney Canada Corp. System and method for heat exchanger failure detection
FR3115767A1 (fr) * 2020-10-30 2022-05-06 Airbus Operations Aéronef comportant un moteur et un système de refroidissement du moteur
CN112537453B (zh) * 2020-11-06 2022-04-22 南京航空航天大学 一种用于混合电推进飞行器的能量综合管理系统
US11492970B2 (en) 2020-12-21 2022-11-08 General Electric Company Thermal management system with fuel cooling
US12196136B2 (en) 2020-12-21 2025-01-14 General Electric Company Regenerative fuel heating system
US11560239B2 (en) 2020-12-21 2023-01-24 General Electric Company Regenerative thermal management system
US11761344B1 (en) 2022-04-19 2023-09-19 General Electric Company Thermal management system
US11702985B1 (en) 2022-04-19 2023-07-18 General Electric Company Thermal management system
US11898495B1 (en) 2022-09-16 2024-02-13 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
US11905884B1 (en) 2022-09-16 2024-02-20 General Electric Company Hydrogen fuel system for a gas turbine engine

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4104873A (en) * 1976-11-29 1978-08-08 The United States Of America As Represented By The Administrator Of The United States National Aeronautics And Space Administration Fuel delivery system including heat exchanger means
US4273304A (en) * 1979-01-31 1981-06-16 Frosch Robert A Cooling system for high speed aircraft
US4696156A (en) * 1986-06-03 1987-09-29 United Technologies Corporation Fuel and oil heat management system for a gas turbine engine
US4776536A (en) * 1987-05-19 1988-10-11 Rockwell International Corporation Integrated aircraft fuel thermal management system
US5538201A (en) * 1993-12-14 1996-07-23 Northrop Grumman Corporation Supersonic natural laminar flow wing
US6182435B1 (en) * 1997-06-05 2001-02-06 Hamilton Sundstrand Corporation Thermal and energy management method and apparatus for an aircraft
US6415595B1 (en) * 2000-08-22 2002-07-09 Hamilton Sundstrand Corporation Integrated thermal management and coolant system for an aircraft
GB0029194D0 (en) * 2000-11-30 2001-01-17 Honeywell Normalair Garrett Cooling apparatus
RU2249710C2 (ru) * 2003-07-01 2005-04-10 Федеральное унитарное государственное предприятие "Научно-производственное объединение машиностроения" Способ работы топливной системы летательного аппарата и устройство для его реализации
DE10361653B4 (de) * 2003-12-30 2008-08-07 Airbus Deutschland Gmbh Kühleinrichtung zum Abführen von Wärme von einer im Innenraum eines Flugzeuges angeordneten Wärmequelle
CN1259219C (zh) * 2003-12-30 2006-06-14 上海交通大学 燃氢高速飞机的液氢燃料携带和换热系统
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

Also Published As

Publication number Publication date
FR2923462B1 (fr) 2010-04-02
RU2478805C2 (ru) 2013-04-10
EP2209716B1 (fr) 2019-04-24
CA2705611C (fr) 2016-06-07
EP2209716A2 (fr) 2010-07-28
WO2009068807A3 (fr) 2009-12-03
US8677755B2 (en) 2014-03-25
WO2009068807A2 (fr) 2009-06-04
US20100288244A1 (en) 2010-11-18
CA2705611A1 (fr) 2009-06-04
JP2011502878A (ja) 2011-01-27
FR2923462A1 (fr) 2009-05-15
CN101970298A (zh) 2011-02-09
RU2010123787A (ru) 2011-12-20

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06T Formal requirements before examination [chapter 6.20 patent gazette]
B11E Dismissal acc. art. 34 of ipl - requirements for examination incomplete
B11T Dismissal of application maintained [chapter 11.20 patent gazette]