BRPI0418159A - dispositivo e processo para aquecer uma cabine de aeronave - Google Patents

dispositivo e processo para aquecer uma cabine de aeronave

Info

Publication number
BRPI0418159A
BRPI0418159A BRPI0418159-0A BRPI0418159A BRPI0418159A BR PI0418159 A BRPI0418159 A BR PI0418159A BR PI0418159 A BRPI0418159 A BR PI0418159A BR PI0418159 A BRPI0418159 A BR PI0418159A
Authority
BR
Brazil
Prior art keywords
air supply
supply line
hot air
conditioning unit
aircraft cabin
Prior art date
Application number
BRPI0418159-0A
Other languages
English (en)
Inventor
Jens Beier
Frank Klimpel
Original Assignee
Airbus 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 Gmbh filed Critical Airbus Gmbh
Publication of BRPI0418159A publication Critical patent/BRPI0418159A/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
    • 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
    • B64D13/08—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being conditioned the air being heated or cooled
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Air-Conditioning For Vehicles (AREA)
  • Air Conditioning Control Device (AREA)

Abstract

"DISPOSITIVO E PROCESSO PARA AQUECER UMA CABINE DE AERONAVE". A invenção refere-se a um dispositivo (10) para aquecer uma cabine de aeronave e compreende uma primeira linha de suprimento de ar quente (12) que conduz para uma unidade de condicionamento de ar (14), uma válvula de controle de fluxo (16) que é disposta na primeira linha de suprimento de ar quente (12) a montante da unidade de condicionamento de ar (14), e uma segunda linha de suprimento de ar quente (18) que se bifurca da primeira linha de suprimento de ar quente (12) entre a válvula de controle de fluxo (1 6) e a unidade de condicionamento de ar (14) e contorna a unidade de condicionamento de ar (14). Para assegurar o condicionamento de ar da cabine de aeronave na eventualidade de uma falha da unidade de condicionamento de ar (14), uma terceira linha de suprimento de ar quente (20) se bifurca a partir da primeira linha de suprimento de ar quente (12), a montante da válvula de controle de fluxo (16), terceira linha e suprimento de ar quente (20) esta que conecta a primeira linha de suprimento de ar quente (12) com a segunda linha de suprimento de ar quente (18). Também, um primeiro mecanismo de fechamento completo é disposto na segunda linha de suprimento de ar quente (18), a montante da junção com a terceira linha de suprimento de ar quente (20), primeiro mecanismo de fechamento completo este que, em sua posição fechada, previne que um fluxo da segunda linha de suprimento de ar quente (18) retorne para a primeira linha de suprimento de ar quente (12). Finalmente, um segundo mecanismo de fechamento completo é disposto na terceira linha de suprimento de ar quente (20), a montante da junção com a segunda linha de suprimento de ar quente (18).
BRPI0418159-0A 2003-12-30 2004-12-30 dispositivo e processo para aquecer uma cabine de aeronave BRPI0418159A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10361658A DE10361658B4 (de) 2003-12-30 2003-12-30 Vorrichtung und Verfahren zum Beheizen einer Flugzeugkabine
PCT/EP2004/014855 WO2005063576A1 (en) 2003-12-30 2004-12-30 Device and process for heating an aircraft cabin

Publications (1)

Publication Number Publication Date
BRPI0418159A true BRPI0418159A (pt) 2007-04-17

Family

ID=34716247

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0418159-0A BRPI0418159A (pt) 2003-12-30 2004-12-30 dispositivo e processo para aquecer uma cabine de aeronave

Country Status (9)

Country Link
US (1) US7727057B2 (pt)
EP (1) EP1699694B1 (pt)
JP (1) JP4538005B2 (pt)
CN (1) CN1902089B (pt)
BR (1) BRPI0418159A (pt)
CA (1) CA2551917C (pt)
DE (2) DE10361658B4 (pt)
RU (1) RU2360841C2 (pt)
WO (1) WO2005063576A1 (pt)

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DE102006014572B4 (de) * 2006-03-29 2008-08-28 Airbus Deutschland Gmbh Vorrichtung und Verfahren zur Luftverteilung in einem Frachtflugzeug
DE102006037539B4 (de) * 2006-08-10 2012-04-26 Airbus Operations Gmbh Klimatisierungssystem mit Vereisungsschutz für ein Luftfahrzeug
US9561855B2 (en) * 2008-05-01 2017-02-07 The Boeing Company Alternate directional momentum ventilation nozzle for passenger cabins
DE102008058451B4 (de) * 2008-11-21 2010-11-18 Airbus Deutschland Gmbh Verfahren und System zur Notbelüftung einer Flugzeugkabine im Fall eines Lecks im Bereich eines Luftmischers
CN102639398B (zh) * 2009-09-29 2016-01-20 空中客车作业有限公司 用于冷却和/或加热飞行器设备的系统和方法
EP2555976B1 (en) * 2010-04-09 2016-05-11 Airbus Operations GmbH Mixer assembly for an aircraft air conditioning system
US9062604B2 (en) 2011-01-14 2015-06-23 Hamilton Sundstrand Corporation Low pressure bleed architecture
US9624831B2 (en) * 2011-03-17 2017-04-18 Bombardier Inc. System and method for operating a precooler in an aircraft
US8955794B2 (en) * 2012-01-24 2015-02-17 The Boeing Company Bleed air systems for use with aircrafts and related methods
US8967528B2 (en) * 2012-01-24 2015-03-03 The Boeing Company Bleed air systems for use with aircrafts and related methods
US9381787B2 (en) * 2012-10-26 2016-07-05 Hamilton Sundstrand Corporation Generally wye shaped elbow for cabin air flow system
EP2799343B1 (en) * 2013-04-03 2017-02-15 Airbus Operations GmbH Aircraft air-conditioining system
US9187180B2 (en) * 2013-05-24 2015-11-17 Hamilton Sundstrand Corporation Thermal pneumatic deicing system for an aircraft RAM air heat exchanger
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
US10100744B2 (en) 2015-06-19 2018-10-16 The Boeing Company Aircraft bleed air and engine starter systems and related methods
DE102015216247A1 (de) * 2015-08-26 2017-03-02 Airbus Operations Gmbh Flugzeugklimaanlage zur Verbindung mit einem flugzeugexternen Lufterzeugungsaggregat
DE102016201924A1 (de) * 2016-02-09 2017-08-10 Lufthansa Technik Aktiengesellschaft Flugzeug und Warneinrichtung für ein "Engine Oil Smell" in einer Flugzeugkabine eines Flugzeuges
US10954865B2 (en) 2018-06-19 2021-03-23 The Boeing Company Pressurized air systems for aircraft and related methods
US11465757B2 (en) 2018-12-06 2022-10-11 The Boeing Company Systems and methods to produce aircraft cabin supply air

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US2391838A (en) * 1945-12-25 Air conditioning system
US2562918A (en) * 1949-02-09 1951-08-07 William M Hynes Aircraft cabin air conditioning system and control valve therefor
US2851254A (en) * 1952-09-10 1958-09-09 Lockheed Aircraft Corp High altitude cabin pressurization and air conditioning system
GB954342A (en) 1962-11-02 1964-04-02 Lockheed Aircraft Corp Aircraft heating system
GB976564A (en) * 1962-11-23 1964-11-25 Normalair Ltd Improvements in or relating to air conditioning of supersonic aircraft
US3825212A (en) * 1973-07-10 1974-07-23 Boeing Co Aircraft heating and ventilating system
USRE32100E (en) * 1978-03-06 1986-04-01 United Technologies Corporation Efficiency air cycle environmental control system
US4149389A (en) * 1978-03-06 1979-04-17 The Trane Company Heat pump system selectively operable in a cascade mode and method of operation
US4445342A (en) * 1982-08-26 1984-05-01 United Technologies Corporation Multi-zone temperature control in air cycle refrigeration systems
DE3638802A1 (de) * 1986-11-13 1988-05-26 Sueddeutsche Kuehler Behr Klimaanlage zur kuehlung oder heizung des fahrgastraumes von fahrzeugen
US5299763A (en) * 1991-12-23 1994-04-05 Allied-Signal Inc. Aircraft cabin air conditioning system with improved fresh air supply
US6012515A (en) * 1996-11-27 2000-01-11 Sikorsky Aircraft Corporation System and method for automatically controlling cabin air temperature in an aircraft
RU2111152C1 (ru) 1996-12-03 1998-05-20 Акционерное общество открытого типа "Нижегородский авиастроительный завод "Сокол" Система кондиционирования воздуха кабинного и приборных отсеков маневренного самолета
DE19707858C1 (de) * 1997-02-27 1998-07-02 Daimler Benz Aerospace Airbus Luftmasseregelsystem für ein Passagierflugzeug
US5906111A (en) * 1997-07-11 1999-05-25 Alliedsignal Inc. Liquid cooled high pressure separation for air cycle cooling system
US5956960A (en) * 1997-09-08 1999-09-28 Sundstrand Corporation Multiple mode environmental control system for pressurized aircraft cabin
US6199387B1 (en) * 1999-07-30 2001-03-13 Liebherr-Aerospace Lindenberg Gmbh Air-conditioning system for airplane cabin
US6189324B1 (en) * 1999-10-05 2001-02-20 Samuel B. Williams Environment control unit for turbine engine
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Also Published As

Publication number Publication date
RU2360841C2 (ru) 2009-07-10
US20070144729A1 (en) 2007-06-28
CN1902089B (zh) 2010-11-24
CA2551917C (en) 2010-08-03
RU2006121520A (ru) 2008-02-10
CN1902089A (zh) 2007-01-24
US7727057B2 (en) 2010-06-01
CA2551917A1 (en) 2005-07-14
JP2007516891A (ja) 2007-06-28
DE10361658B4 (de) 2008-05-08
DE10361658A1 (de) 2005-08-04
WO2005063576A1 (en) 2005-07-14
EP1699694A1 (en) 2006-09-13
JP4538005B2 (ja) 2010-09-08
DE602004015155D1 (de) 2008-08-28
EP1699694B1 (en) 2008-07-16
WO2005063576B1 (en) 2005-09-29

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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 Technical examination (opinion): publication of technical examination (opinion)
B09B Decision: refusal
B09B Decision: refusal