CA2882328C - Panneau de carrosserie pour vehicule de transport comprenant un dispositif d'echange thermique et vehicule de transport comprenant un tel panneau de carrosserie - Google Patents

Panneau de carrosserie pour vehicule de transport comprenant un dispositif d'echange thermique et vehicule de transport comprenant un tel panneau de carrosserie Download PDF

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Publication number
CA2882328C
CA2882328C CA2882328A CA2882328A CA2882328C CA 2882328 C CA2882328 C CA 2882328C CA 2882328 A CA2882328 A CA 2882328A CA 2882328 A CA2882328 A CA 2882328A CA 2882328 C CA2882328 C CA 2882328C
Authority
CA
Canada
Prior art keywords
heat exchange
support plate
panel
aircraft
exchange device
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
CA2882328A
Other languages
English (en)
French (fr)
Other versions
CA2882328A1 (fr
Inventor
Bertrand Pelissier
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.)
Liebherr Aerospace Toulouse SAS
Original Assignee
Liebherr Aerospace Toulouse 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 Liebherr Aerospace Toulouse SAS filed Critical Liebherr Aerospace Toulouse SAS
Publication of CA2882328A1 publication Critical patent/CA2882328A1/fr
Application granted granted Critical
Publication of CA2882328C publication Critical patent/CA2882328C/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/40—Sound or heat insulation, e.g. using insulation blankets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • B64D13/006—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being used to cool structural parts of the aircraft
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Laminated Bodies (AREA)
CA2882328A 2012-09-19 2013-09-19 Panneau de carrosserie pour vehicule de transport comprenant un dispositif d'echange thermique et vehicule de transport comprenant un tel panneau de carrosserie Active CA2882328C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1258791A FR2995589B1 (fr) 2012-09-19 2012-09-19 Panneau de carrosserie pour vehicule de transport comprenant un dispositif d'echange thermique et vehicule de transport comprenant un tel panneau de carrosserie
FR12.58791 2012-09-19
PCT/FR2013/052170 WO2014044981A1 (fr) 2012-09-19 2013-09-19 Panneau de carrosserie pour véhicule de transport comprenant un dispositif d'échange thermique et véhicule de transport comprenant un tel panneau de carrosserie

Publications (2)

Publication Number Publication Date
CA2882328A1 CA2882328A1 (fr) 2014-03-27
CA2882328C true CA2882328C (fr) 2019-07-23

Family

ID=47356103

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2882328A Active CA2882328C (fr) 2012-09-19 2013-09-19 Panneau de carrosserie pour vehicule de transport comprenant un dispositif d'echange thermique et vehicule de transport comprenant un tel panneau de carrosserie

Country Status (6)

Country Link
US (1) US9434465B2 (https=)
EP (1) EP2897862B1 (https=)
BR (1) BR112015006170B1 (https=)
CA (1) CA2882328C (https=)
FR (1) FR2995589B1 (https=)
WO (1) WO2014044981A1 (https=)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9499268B2 (en) * 2014-03-27 2016-11-22 Northrop Grumman Systems Corporation Near belly-tangent pod system for an aircraft
US9932831B2 (en) * 2014-05-09 2018-04-03 United Technologies Corporation High temperature compliant metallic elements for low contact stress ceramic support
WO2016024521A1 (ja) 2014-08-13 2016-02-18 株式会社Ihi 航空機の電子機器を冷却する冷却装置
JP6336362B2 (ja) * 2014-09-10 2018-06-06 三菱航空機株式会社 航空機
US10059435B2 (en) * 2014-12-04 2018-08-28 Parker-Hannifin Corporation Low drag skin heat exchanger
US11262142B2 (en) 2016-04-26 2022-03-01 Northrop Grumman Systems Corporation Heat exchangers, weld configurations for heat exchangers and related systems and methods
US10723437B2 (en) * 2017-05-30 2020-07-28 The Boeing Company System for structurally integrated thermal management for thin wing aircraft control surface actuators
US10773787B2 (en) 2017-06-14 2020-09-15 The Boeing Company Wing-to-fuselage joints and aircraft including the same
US10766598B2 (en) * 2017-06-14 2020-09-08 The Boeing Company Wing-to-fuselage joints and aircraft including the same
CN108045546A (zh) * 2017-09-20 2018-05-18 中国水利水电科学研究院 一种轻小型固定翼无人机载荷快速连接与更换装置
EP3771644B1 (en) 2019-07-29 2025-01-08 General Electric Company Vehicle heat exchanger system
DE102019122426A1 (de) 2019-08-21 2021-02-25 Airbus Operations Gmbh Primärstrukturanordnung für einen Flugzeugaußenhautwärmetauscher, Flugzeug mit Primärstrukturanordnung und Verfahren zum Anbringen eines Flugzeugaußenhautwärmetauschers
WO2023022794A2 (en) * 2021-06-25 2023-02-23 Advent Technologies, Llc Fuselage heat exchanger for cooling power source for unmanned aerial vehicles (uavs)
FR3166885A1 (fr) * 2024-09-30 2026-04-03 Airbus Operations (S.A.S.) Dispositif de protection thermique d’un longeron inférieur d’un caisson d’aéronef

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2452251A (en) * 1942-03-19 1948-10-26 North American Aviation Inc Retractable landing gear fairing
US4819720A (en) * 1984-11-09 1989-04-11 Mcdonnell Douglas Corporation Skin heat exchanger
JP2771849B2 (ja) * 1989-06-23 1998-07-02 エス・ティ・エス株式会社 航空電子機器の機体外表面クーラーを利用した冷却装置
US5423498A (en) 1993-04-27 1995-06-13 E-Systems, Inc. Modular liquid skin heat exchanger
US6042315A (en) * 1997-10-06 2000-03-28 United Technologies Corporation Fastener
US6612523B2 (en) * 2001-12-21 2003-09-02 Lockheed Martin Corporation Aircraft structures having improved through-thickness thermal conductivity
US6907920B2 (en) * 2002-01-29 2005-06-21 United Technologies Corporation Heat exchanger panel
FR2871436B1 (fr) * 2004-06-11 2007-09-07 Airbus France Sas Aeronef muni d'un carenage ventral, et carenage ventral.
FR2894225B1 (fr) * 2005-12-07 2008-01-11 Airbus France Sa Sa Mur de cloisonnement pour carenage ventral d'aeronef et aeronef muni d'un carenage ventral
ES2317762B1 (es) * 2006-10-31 2010-02-10 Airbus España, S.L. Carena ventral para un avion.
US8950468B2 (en) * 2007-05-11 2015-02-10 The Boeing Company Cooling system for aerospace vehicle components
DE102008026536A1 (de) 2008-06-03 2009-12-17 Airbus Deutschland Gmbh System und Verfahren zur Kühlung einer wärmebelaste ten Einrichtung in einem Fahrzeug, insbesondere einem Luftfahrzeug

Also Published As

Publication number Publication date
EP2897862B1 (fr) 2016-11-02
US20150246719A1 (en) 2015-09-03
BR112015006170B1 (pt) 2022-04-05
BR112015006170A2 (https=) 2017-08-22
EP2897862A1 (fr) 2015-07-29
FR2995589B1 (fr) 2015-07-31
WO2014044981A1 (fr) 2014-03-27
CA2882328A1 (fr) 2014-03-27
FR2995589A1 (fr) 2014-03-21
US9434465B2 (en) 2016-09-06

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