BR112015006170B1 - Painel de carroceria para veículo de transporte - Google Patents

Painel de carroceria para veículo de transporte Download PDF

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Publication number
BR112015006170B1
BR112015006170B1 BR112015006170-2A BR112015006170A BR112015006170B1 BR 112015006170 B1 BR112015006170 B1 BR 112015006170B1 BR 112015006170 A BR112015006170 A BR 112015006170A BR 112015006170 B1 BR112015006170 B1 BR 112015006170B1
Authority
BR
Brazil
Prior art keywords
heat transfer
transfer device
heat
support plate
aircraft
Prior art date
Application number
BR112015006170-2A
Other languages
English (en)
Portuguese (pt)
Other versions
BR112015006170A2 (https=
Inventor
Bertrand Pelissier
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 BR112015006170A2 publication Critical patent/BR112015006170A2/pt
Publication of BR112015006170B1 publication Critical patent/BR112015006170B1/pt

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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

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  • 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)
BR112015006170-2A 2012-09-19 2013-09-19 Painel de carroceria para veículo de transporte BR112015006170B1 (pt)

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
BR112015006170A2 BR112015006170A2 (https=) 2017-08-22
BR112015006170B1 true BR112015006170B1 (pt) 2022-04-05

Family

ID=47356103

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015006170-2A BR112015006170B1 (pt) 2012-09-19 2013-09-19 Painel de carroceria para veículo de transporte

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
BR112015006170A2 (https=) 2017-08-22
CA2882328C (fr) 2019-07-23
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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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 19/09/2013, OBSERVADAS AS CONDICOES LEGAIS.