BRPI0418170A - sistema de refrigeração para expelir calor a partir de uma fonte de calor localizada no interior de uma aeronave, e, método para a descarga de calor a partir de uma fonte de calor disposta no interior de uma aeronava - Google Patents
sistema de refrigeração para expelir calor a partir de uma fonte de calor localizada no interior de uma aeronave, e, método para a descarga de calor a partir de uma fonte de calor disposta no interior de uma aeronavaInfo
- Publication number
- BRPI0418170A BRPI0418170A BRPI0418170-0A BRPI0418170A BRPI0418170A BR PI0418170 A BRPI0418170 A BR PI0418170A BR PI0418170 A BRPI0418170 A BR PI0418170A BR PI0418170 A BRPI0418170 A BR PI0418170A
- Authority
- BR
- Brazil
- Prior art keywords
- heat
- aircraft
- heat source
- source
- section
- Prior art date
Links
- 238000001816 cooling Methods 0.000 title abstract 2
- 238000000034 method Methods 0.000 title abstract 2
- 238000007599 discharging Methods 0.000 title 1
- 239000003638 chemical reducing agent Substances 0.000 abstract 2
- 239000007791 liquid phase Substances 0.000 abstract 1
- 239000012071 phase Substances 0.000 abstract 1
- 238000005057 refrigeration Methods 0.000 abstract 1
- 230000007704 transition Effects 0.000 abstract 1
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
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/04—Galleys
-
- 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
-
- 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, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D2013/0603—Environmental Control Systems
- B64D2013/0629—Environmental Control Systems with subsystems for cooling food, catering or special loads
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Abstract
"SISTEMA DE REFRIGERAçãO PARA EXPELIR CALOR A PARTIR DE UMA FONTE DE CALOR LOCALIZADA NO INTERIOR DE UMA AERONAVE E, MéTODO PARA A DESCARGA DE CALOR A PARTIR DE UMA FONTE DE CALOR DISPOSTA NO INTERIOR DE UMA AERONAVE". Com um sistema de refrigeração para expelir calor a partir de uma fonte de calor (30) localizada no interior de uma aeronave para um redutor de calor (322), com um sistema de tubulação (10) selado com relação a atmosfera circundante, o qual é termicamente acoplado com uma seção de entrada de calor (14) com a fonte de calor (38) e com uma seção de saída de calor (22) com o redutor de calor (32), e que preferivelmente tem uma seção de transporte essencialmente adiabática (21), é proposto que o sistema de tubulação (10) seja cheio com um meio de transporte de calor (12) que, quando ele toma calor a partir da fonte de calor (38) na seção de entrada de calor (14), é submetido a uma transição da fase líquida para a fase gasosa, então flui para a seção de saída de calor (22) e aqui, quando da descarga de calor para o dissipador de calor (32), se condensa mais uma vez novamente e flui de volta para a seção de entrada de calor (14).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10361653A DE10361653B4 (de) | 2003-12-30 | 2003-12-30 | Kühleinrichtung zum Abführen von Wärme von einer im Innenraum eines Flugzeuges angeordneten Wärmequelle |
PCT/EP2004/014860 WO2005063566A2 (en) | 2003-12-30 | 2004-12-30 | Cooling system and method for expelling heat from a heat source located in the interior of an aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0418170A true BRPI0418170A (pt) | 2007-04-27 |
Family
ID=34716243
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0418170-0A BRPI0418170A (pt) | 2003-12-30 | 2004-12-30 | sistema de refrigeração para expelir calor a partir de uma fonte de calor localizada no interior de uma aeronave, e, método para a descarga de calor a partir de uma fonte de calor disposta no interior de uma aeronava |
Country Status (9)
Country | Link |
---|---|
US (1) | US7967249B2 (pt) |
EP (1) | EP1700080B1 (pt) |
JP (1) | JP4673856B2 (pt) |
CN (1) | CN100510604C (pt) |
BR (1) | BRPI0418170A (pt) |
CA (1) | CA2552157C (pt) |
DE (2) | DE10361653B4 (pt) |
RU (1) | RU2378596C2 (pt) |
WO (1) | WO2005063566A2 (pt) |
Families Citing this family (35)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10361646B4 (de) * | 2003-12-30 | 2011-01-13 | Airbus Operations Gmbh | Vorrichtung und Verfahren zur Temperaturregelung in einer Flugzeugkabine |
FR2904103B1 (fr) | 2006-07-18 | 2015-05-15 | Airbus France | Dispositif a ecoulement de chaleur |
FR2923462B1 (fr) * | 2007-11-14 | 2010-04-02 | Airbus France | Procede de gestion des rejections thermiques generees par un aeronef et dispositif de refroidissement pour aeronef permettant la mise en oeuvre dudit procede. |
DE102008025951B4 (de) * | 2008-05-30 | 2010-10-28 | Airbus Deutschland Gmbh | Kühlen einer elektronischen Einrichtung in einem Luftfahrzeug durch eine fallweise einphasige oder zweiphasige Kühlung |
DE102008035823A1 (de) * | 2008-07-31 | 2010-02-25 | Airbus Deutschland Gmbh | Wärmeübertrager für die Außenhaut eines Flugzeugs |
US20100071881A1 (en) * | 2008-08-21 | 2010-03-25 | Airbus Operations | Cooling system for aircraft electric or electronic devices |
DE102008044645B3 (de) * | 2008-08-27 | 2010-02-18 | Airbus Deutschland Gmbh | Flugzeugsignalrechnersystem mit einer Mehrzahl von modularen Signalrechnereinheiten |
DE102009039814A1 (de) * | 2009-09-02 | 2011-03-10 | Airbus Operations Gmbh | System und Verfahren zum Kühlen mindestens einer Wärme erzeugenden Einrichtung in einem Flugzeug |
US20120291459A1 (en) * | 2011-05-17 | 2012-11-22 | The Boeing Company | Method and apparatus for aircraft galley cooling |
US20120298337A1 (en) * | 2011-05-24 | 2012-11-29 | Tiwari Punit | Method and apparatus for radiative heat transfer augmentation for aviation electronic equipments cooled by convection |
CN102381479B (zh) * | 2011-09-14 | 2014-07-09 | 中国航空工业集团公司西安飞机设计研究所 | 一种无冲压进气道的综合环控/液冷热能管理系统 |
CN102390537A (zh) * | 2011-09-14 | 2012-03-28 | 中国航空工业集团公司西安飞机设计研究所 | 一种环控系统和液冷系统综合热能管理系统 |
CN102545546B (zh) * | 2011-12-01 | 2014-05-14 | 国家电网公司 | 循环冷却系统及控制循环冷却系统的方法 |
US20140109603A1 (en) | 2011-12-29 | 2014-04-24 | Embraer S.A. | Integrated environmental control systems and methods for controlling environmental temperature of an enclosed space |
US10124894B2 (en) | 2012-03-30 | 2018-11-13 | B/E Aerospace, Inc. | Aircraft galley chilled air distribution system |
EP2653386B1 (en) * | 2012-04-17 | 2014-12-10 | Airbus Operations GmbH | Heat dissipation of power electronics of a cooling unit |
FR2992347B1 (fr) * | 2012-06-22 | 2014-07-18 | Snecma | Recepteur de turbomachine d'aeronef a doublet d'helices contrarotatives non carenees, comprenant une turbine libre exterieure a maintien renforce |
US11220340B2 (en) | 2013-03-28 | 2022-01-11 | Rockwell Collins, Inc. | Galley cart bay rub strip assembly with enhanced airflow |
US10488075B2 (en) | 2013-06-18 | 2019-11-26 | B/E Aerospace, Inc. | Apparatus for pre-heating potable water in aircraft with waste heat |
US11118808B2 (en) | 2013-12-06 | 2021-09-14 | The Boeing Company | Method, system, and device for liquid drainage |
US9988151B2 (en) * | 2014-01-24 | 2018-06-05 | The Boeing Company | Dehumidification system for use in a vehicle and method of assembling thereof |
US10364043B2 (en) * | 2014-07-02 | 2019-07-30 | Embraer S.A. | Passive aircraft cooling systems and methods |
FR3039512B1 (fr) | 2015-07-28 | 2017-12-22 | Thales Sa | Rechauffage d'un premier equipement aeronautique d'aeronef |
FR3039514B1 (fr) * | 2015-07-28 | 2017-09-08 | Thales Sa | Rechauffage pour un equipement aeronautique |
FR3039511B1 (fr) | 2015-07-28 | 2017-09-08 | Thales Sa | Rechauffage pour equipement aeronautique d'aeronef |
JP6090407B1 (ja) * | 2015-10-27 | 2017-03-08 | 三菱電機株式会社 | 保存移動装置 |
US20180170553A1 (en) * | 2016-12-20 | 2018-06-21 | Qualcomm Incorporated | Systems, methods, and apparatus for passive cooling of uavs |
US20180229850A1 (en) * | 2017-02-15 | 2018-08-16 | Pratt & Whitney Canada Corp. | Anti-icing system for gas turbine engine |
DE102017126693A1 (de) * | 2017-11-14 | 2019-05-16 | Airbus Operations Gmbh | Kühlanordnung für eine Bordküche und Bordküche |
JP2020106207A (ja) * | 2018-12-27 | 2020-07-09 | 川崎重工業株式会社 | ループ型ヒートパイプ及び輸送機 |
JP7299017B2 (ja) * | 2018-12-27 | 2023-06-27 | 川崎重工業株式会社 | ループ型ヒートパイプ及び輸送機 |
EP3771644A1 (en) | 2019-07-29 | 2021-02-03 | General Electric Company | Vehicle heat exchanger system |
US11713126B2 (en) * | 2019-08-12 | 2023-08-01 | The Boeing Company | Aircraft air conditioning pack assembly and method of assembling |
US11765871B2 (en) * | 2020-03-26 | 2023-09-19 | Ge Aviation Systems Llc | Aircraft and method for thermal management |
JP7210527B2 (ja) * | 2020-12-14 | 2023-01-23 | Hapsモバイル株式会社 | 飛行体 |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
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US2499736A (en) * | 1946-09-06 | 1950-03-07 | Kleen Nils Erland Af | Aircraft refrigeration |
US3929305A (en) * | 1972-10-27 | 1975-12-30 | Nasa | Heat exchanger system and method |
US4000776A (en) * | 1974-12-03 | 1977-01-04 | The United States Of America As Represented By The Secretary Of The Air Force | Heat pipe system |
US4044396A (en) * | 1975-08-14 | 1977-08-23 | The United States Of America As Represented By The Secretary Of The Air Force | Heat pipe cooling of airborne phased array radar |
SE411949B (sv) * | 1976-07-09 | 1980-02-11 | Ericsson Telefon Ab L M | Kylanordning |
US4057104A (en) * | 1976-08-26 | 1977-11-08 | Westinghouse Electric Corporation | Temperature controlled airborne electronic assembly |
GB1595961A (en) | 1978-01-17 | 1981-08-19 | Thorn Automation Ltd | Cooling electrical equipment |
US4786015A (en) * | 1986-12-31 | 1988-11-22 | Sundstrand Corporation | Structural cooling unit |
US6435454B1 (en) * | 1987-12-14 | 2002-08-20 | Northrop Grumman Corporation | Heat pipe cooling of aircraft skins for infrared radiation matching |
DE3812739C1 (pt) * | 1988-04-16 | 1989-07-06 | Deutsche Lufthansa Ag, 5000 Koeln, De | |
US5267608A (en) * | 1992-07-27 | 1993-12-07 | General Electric Company | Heat exchanger and reactor for aircraft and propulsion systems |
US5423498A (en) * | 1993-04-27 | 1995-06-13 | E-Systems, Inc. | Modular liquid skin heat exchanger |
DE4340317C2 (de) | 1993-11-26 | 1996-03-21 | Daimler Benz Aerospace Airbus | Kühlsystem zur Kühlung von Lebensmitteln in einem Flugzeug |
FR2763117B1 (fr) * | 1997-05-12 | 1999-08-13 | Italinnova Sas | Installation pour la conservation froide avec rechauffage localise de mets sur des plateaux-repas |
SE9702402D0 (sv) * | 1997-06-24 | 1997-06-24 | Electrolux Ab | Absorption refrigerator |
US6658881B1 (en) * | 2000-11-17 | 2003-12-09 | Wesley M. Plattner | Apparatus and method for mounting a condenser in an aircraft |
US6481228B1 (en) * | 2001-08-23 | 2002-11-19 | Industrial Technology Research Institute | Air conditioning module for room partition unit |
US6880351B2 (en) * | 2001-09-05 | 2005-04-19 | Be Intellectual Property, Inc. | Liquid galley refrigeration system for aircraft |
NO320664B1 (no) * | 2001-12-19 | 2006-01-16 | Sinvent As | System for oppvarming og kjoling av kjoretoy |
WO2003054469A1 (en) * | 2001-12-21 | 2003-07-03 | Tth Research, Inc. | Loop heat pipe |
-
2003
- 2003-12-30 DE DE10361653A patent/DE10361653B4/de not_active Expired - Fee Related
-
2004
- 2004-12-30 BR BRPI0418170-0A patent/BRPI0418170A/pt not_active Application Discontinuation
- 2004-12-30 CA CA2552157A patent/CA2552157C/en not_active Expired - Fee Related
- 2004-12-30 RU RU2006122584/06A patent/RU2378596C2/ru not_active IP Right Cessation
- 2004-12-30 WO PCT/EP2004/014860 patent/WO2005063566A2/en active Application Filing
- 2004-12-30 US US10/581,328 patent/US7967249B2/en not_active Expired - Fee Related
- 2004-12-30 CN CNB2004800395212A patent/CN100510604C/zh not_active Expired - Fee Related
- 2004-12-30 EP EP04804445A patent/EP1700080B1/en not_active Not-in-force
- 2004-12-30 DE DE602004023325T patent/DE602004023325D1/de active Active
- 2004-12-30 JP JP2006546123A patent/JP4673856B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
RU2006122584A (ru) | 2008-02-10 |
CN1902454A (zh) | 2007-01-24 |
JP4673856B2 (ja) | 2011-04-20 |
CA2552157C (en) | 2011-04-26 |
CN100510604C (zh) | 2009-07-08 |
CA2552157A1 (en) | 2005-07-14 |
JP2007519555A (ja) | 2007-07-19 |
WO2005063566A3 (en) | 2005-09-22 |
US20070095521A1 (en) | 2007-05-03 |
EP1700080B1 (en) | 2009-09-23 |
WO2005063566A2 (en) | 2005-07-14 |
EP1700080A2 (en) | 2006-09-13 |
RU2378596C2 (ru) | 2010-01-10 |
DE10361653B4 (de) | 2008-08-07 |
DE10361653A1 (de) | 2005-09-22 |
DE602004023325D1 (de) | 2009-11-05 |
US7967249B2 (en) | 2011-06-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B25D | Requested change of name of applicant approved |
Owner name: AIRBUS OPERATIONS GMBH (DE) Free format text: NOME ALTERADO DE: AIRBUS DEUTSCHLAND GMBH |
|
B07A | Application suspended after technical examination (opinion) [chapter 7.1 patent gazette] | ||
B09B | Patent application refused [chapter 9.2 patent gazette] | ||
B09B | Patent application refused [chapter 9.2 patent gazette] |