BRPI0913289A2 - método para refrigerar um dispositivo eletrônico em uma aeronave, dispositivo de refrigeração de aeronave, e, sistema de refrigeração de componente eletrônico de aeronave redundante. - Google Patents

método para refrigerar um dispositivo eletrônico em uma aeronave, dispositivo de refrigeração de aeronave, e, sistema de refrigeração de componente eletrônico de aeronave redundante.

Info

Publication number
BRPI0913289A2
BRPI0913289A2 BRPI0913289A BRPI0913289A BRPI0913289A2 BR PI0913289 A2 BRPI0913289 A2 BR PI0913289A2 BR PI0913289 A BRPI0913289 A BR PI0913289A BR PI0913289 A BRPI0913289 A BR PI0913289A BR PI0913289 A2 BRPI0913289 A2 BR PI0913289A2
Authority
BR
Brazil
Prior art keywords
aircraft
cooling
redundant
electronic component
electronic
Prior art date
Application number
BRPI0913289A
Other languages
English (en)
Inventor
Matthias Reiss
Sebastien Roering
Wilson Willy Casas Noriegas
Original Assignee
Airbus Operations Gmbh
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 Operations Gmbh filed Critical Airbus Operations Gmbh
Publication of BRPI0913289A2 publication Critical patent/BRPI0913289A2/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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00—Constructional details common to different types of electric apparatus
    • H05K7/20—Modifications to facilitate cooling, ventilating, or heating
    • H05K7/2029—Modifications to facilitate cooling, ventilating, or heating using a liquid coolant with phase change in electronic enclosures
    • H05K7/20354—Refrigerating circuit comprising a compressor
    • 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
    • B64D2013/0674—Environmental Control Systems comprising liquid subsystems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • F28D15/0266—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with separate evaporating and condensing chambers connected by at least one conduit; Loop-type heat pipes; with multiple or common evaporating or condensing chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)
BRPI0913289A 2008-05-30 2009-05-13 método para refrigerar um dispositivo eletrônico em uma aeronave, dispositivo de refrigeração de aeronave, e, sistema de refrigeração de componente eletrônico de aeronave redundante. BRPI0913289A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US5740308P 2008-05-30 2008-05-30
DE102008025951A DE102008025951B4 (de) 2008-05-30 2008-05-30 Kühlen einer elektronischen Einrichtung in einem Luftfahrzeug durch eine fallweise einphasige oder zweiphasige Kühlung
PCT/EP2009/003412 WO2009143963A1 (de) 2008-05-30 2009-05-13 Kühlen einer elektronischen einrichtung in einem luftfahrzeug durch eine fallweise einphasige oder zweiphasige kühlung

Publications (1)

Publication Number Publication Date
BRPI0913289A2 true BRPI0913289A2 (pt) 2016-01-26

Family

ID=40823476

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0913289A BRPI0913289A2 (pt) 2008-05-30 2009-05-13 método para refrigerar um dispositivo eletrônico em uma aeronave, dispositivo de refrigeração de aeronave, e, sistema de refrigeração de componente eletrônico de aeronave redundante.

Country Status (9)

Country Link
US (1) US20120000630A1 (pt)
EP (1) EP2289293B1 (pt)
JP (1) JP2011522408A (pt)
CN (1) CN102047776A (pt)
BR (1) BRPI0913289A2 (pt)
CA (1) CA2726436A1 (pt)
DE (1) DE102008025951B4 (pt)
RU (1) RU2010151853A (pt)
WO (1) WO2009143963A1 (pt)

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DE102009039814A1 (de) * 2009-09-02 2011-03-10 Airbus Operations Gmbh System und Verfahren zum Kühlen mindestens einer Wärme erzeugenden Einrichtung in einem Flugzeug
FR2972894B1 (fr) * 2011-03-14 2013-04-26 Converteam Technology Ltd Dispositif de conversion d'energie, notamment pour une station sous marine de compression et de pompage, a moyens de refroidissement perfectionnes
FR2972893B1 (fr) 2011-03-14 2013-04-26 Converteam Technology Ltd Dispositif de conversion d'energie, notamment pour un systeme d'entrainement electrique de station sous-marine de compression et de pompage
US10653044B2 (en) 2013-01-10 2020-05-12 International Business Machines Corporation Energy efficiency based control for a cooling system
DE102013208369A1 (de) * 2013-05-07 2014-11-13 Siemens Aktiengesellschaft Vorrichtung mit einer elektronischen Komponente und einer Kältemaschine zum Kühlen der elektronischen Komponente sowie Verfahren zum Kühlen einer elektronischen Komponente
US9187180B2 (en) * 2013-05-24 2015-11-17 Hamilton Sundstrand Corporation Thermal pneumatic deicing system for an aircraft RAM air heat exchanger
US10364043B2 (en) * 2014-07-02 2019-07-30 Embraer S.A. Passive aircraft cooling systems and methods
DE102016218020A1 (de) * 2016-09-20 2018-04-05 Robert Bosch Gmbh Kühlkreis und Verfahren zum Betreiben eines Kühlkreises
DE102017204526A1 (de) * 2017-03-17 2018-09-20 Robert Bosch Gmbh Verfahren zum Kühlen eines Umrichters, insbesondere eines Frequenzumrichters in einem Wärmepumpenkreislauf
FR3067560B1 (fr) * 2017-06-12 2021-09-03 Safran Electronics & Defense Dispositif de refroidissement de baies avioniques a liquide caloporteur
DE102017211561A1 (de) * 2017-07-06 2019-01-10 Siemens Aktiengesellschaft Flugzeug mit einem Leistungselektronikbauteil
DE102018114353A1 (de) * 2018-06-15 2019-12-19 Airbus Defence and Space GmbH Kühlsystem mit zwei Wärmetauschern und Fahrzeug mit einem Kühlsystem
US11525636B2 (en) * 2019-03-20 2022-12-13 The Government Of The United States Of America, As Represented By The Secretary Of The Navy Method and system for stabilizing loop heat pipe operation with a controllable condenser bypass
DE102020126580B3 (de) * 2020-10-09 2022-01-13 Viessmann Climate Solutions Se Kältekreislaufvorrichtung und Verfahren zum Betrieb einer solchen Kältekreislaufvorrichtung
EP4119444B1 (en) * 2021-07-13 2024-10-30 Airbus Operations, S.L.U. Method for cooling an electrical aircraft propulsion system
DE102022111276A1 (de) 2022-05-06 2023-05-25 Mahle International Gmbh Steckvorrichtung
WO2024023316A1 (en) * 2022-07-29 2024-02-01 Heart Aerospace AB Thermal management system
CN117015220B (zh) * 2023-09-12 2026-06-19 珠海格力电器股份有限公司 液冷设备及其防凝露控制方法

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Also Published As

Publication number Publication date
RU2010151853A (ru) 2012-07-10
JP2011522408A (ja) 2011-07-28
CN102047776A (zh) 2011-05-04
US20120000630A1 (en) 2012-01-05
WO2009143963A1 (de) 2009-12-03
EP2289293B1 (de) 2017-03-01
DE102008025951B4 (de) 2010-10-28
DE102008025951A1 (de) 2010-04-29
CA2726436A1 (en) 2009-12-03
EP2289293A1 (de) 2011-03-02

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Legal Events

Date Code Title Description
B11A Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing
B11Y Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette]