FR3037565B1 - AIRCRAFT EQUIPPED WITH A HEAT GENERATING DEVICE - Google Patents

AIRCRAFT EQUIPPED WITH A HEAT GENERATING DEVICE Download PDF

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Publication number
FR3037565B1
FR3037565B1 FR1555689A FR1555689A FR3037565B1 FR 3037565 B1 FR3037565 B1 FR 3037565B1 FR 1555689 A FR1555689 A FR 1555689A FR 1555689 A FR1555689 A FR 1555689A FR 3037565 B1 FR3037565 B1 FR 3037565B1
Authority
FR
France
Prior art keywords
air
generating device
heat
circuit
heat generating
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.)
Active
Application number
FR1555689A
Other languages
French (fr)
Other versions
FR3037565A1 (en
Inventor
Fabien Boudjemaa
Adrien Gasse
Matthieu Baron
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.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
SNECMA 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 Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1555689A priority Critical patent/FR3037565B1/en
Publication of FR3037565A1 publication Critical patent/FR3037565A1/en
Application granted granted Critical
Publication of FR3037565B1 publication Critical patent/FR3037565B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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, 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
    • B64D13/08—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 the air being heated or cooled
    • 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
    • B64D13/02—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being pressurised
    • 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
    • B64D2013/0688—Environmental Control Systems with means for recirculating cabin air
    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • B64D2041/005—Fuel cells
    • 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
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/40—Application of hydrogen technology to transportation, e.g. using fuel cells

Landscapes

  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fuel Cell (AREA)
  • Central Air Conditioning (AREA)

Abstract

Aéronef comportant une zone pressurisée (12) et une zone non pressurisée (14), un système de circulation d'air (20) configuré pour maintenir la pression dans la zone pressurisée. Le système de circulation d'air (20) comporte un circuit d'évacuation d'air (22) permettant à l'air de passer de la zone pressurisée à la zone non pressurisée. L'aéronef comporte également un dispositif générateur de chaleur, un échangeur de chaleur disposé dans le circuit d'évacuation d'air, et un circuit d'évacuation de chaleur. Le circuit d'évacuation de chaleur est configuré pour permettre le transfert d'une chaleur dégagée par le dispositif générateur de chaleur à l'air circulant dans le circuit d'évacuation d'air via l'échangeur de chaleur.An aircraft having a pressurized zone (12) and a non-pressurized zone (14), an air circulation system (20) configured to maintain pressure in the pressurized zone. The air circulation system (20) includes an air exhaust circuit (22) for allowing air to pass from the pressurized zone to the unpressurized zone. The aircraft also comprises a heat generating device, a heat exchanger disposed in the exhaust air circuit, and a heat evacuation circuit. The heat evacuation circuit is configured to allow the transfer of heat generated by the heat generating device to the air circulating in the exhaust air circuit via the heat exchanger.

FR1555689A 2015-06-22 2015-06-22 AIRCRAFT EQUIPPED WITH A HEAT GENERATING DEVICE Active FR3037565B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1555689A FR3037565B1 (en) 2015-06-22 2015-06-22 AIRCRAFT EQUIPPED WITH A HEAT GENERATING DEVICE

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1555689A FR3037565B1 (en) 2015-06-22 2015-06-22 AIRCRAFT EQUIPPED WITH A HEAT GENERATING DEVICE
FR1555689 2015-06-22

Publications (2)

Publication Number Publication Date
FR3037565A1 FR3037565A1 (en) 2016-12-23
FR3037565B1 true FR3037565B1 (en) 2019-01-25

Family

ID=54066057

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1555689A Active FR3037565B1 (en) 2015-06-22 2015-06-22 AIRCRAFT EQUIPPED WITH A HEAT GENERATING DEVICE

Country Status (1)

Country Link
FR (1) FR3037565B1 (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008062038A1 (en) * 2008-12-12 2010-06-17 Liebherr-Aerospace Lindenberg Gmbh Emergency power system for supplying electricity to e.g. air conditioning system in cabin of civilian aircraft, has evaporation system evaporating fuel cell-product water, and heat exchanger whose supply air is cooled down by water
DE102009031880A1 (en) * 2009-07-06 2011-01-20 Airbus Operations Gmbh Cooling concept for a fuel cell emergency power system
DE102010005902B4 (en) * 2010-01-27 2017-09-14 Airbus Operations Gmbh Aircraft having at least one pressurized hull area and at least one non-pressurized area, and methods of venting a non-pressurized area of an aircraft
DE102010051517A1 (en) * 2010-11-16 2012-05-16 Airbus Operations Gmbh An aircraft exterior skin heat exchanger, aircraft cooling system, and method of operating an aircraft exterior skin heat exchanger
FR2971763B1 (en) * 2011-02-22 2013-03-15 Airbus Operations Sas THERMAL EXCHANGER INCORPORATED IN A WALL OF AN AIRCRAFT
FR3008678B1 (en) * 2013-07-16 2015-09-04 Dassault Aviat AIRCRAFT COMPRISING ELECTRICAL POWER EQUIPMENT AND VENTILATION SYSTEM FOR ELECTRICAL POWER EQUIPMENT, INTERNAL ELEMENT AND METHOD THEREOF

Also Published As

Publication number Publication date
FR3037565A1 (en) 2016-12-23

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