WO2011064263A3 - Élément structural composite à transmission électrique de puissance intégrée - Google Patents

Élément structural composite à transmission électrique de puissance intégrée Download PDF

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Publication number
WO2011064263A3
WO2011064263A3 PCT/EP2010/068145 EP2010068145W WO2011064263A3 WO 2011064263 A3 WO2011064263 A3 WO 2011064263A3 EP 2010068145 W EP2010068145 W EP 2010068145W WO 2011064263 A3 WO2011064263 A3 WO 2011064263A3
Authority
WO
WIPO (PCT)
Prior art keywords
structural element
built
power transmission
electrical power
composite structural
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.)
Ceased
Application number
PCT/EP2010/068145
Other languages
English (en)
Other versions
WO2011064263A2 (fr
Inventor
Jesus Aspas Puertolas
Nicolas Maisonnave
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.)
Airbus Group SAS
Original Assignee
European Aeronautic Defence and Space Company EADS France
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 European Aeronautic Defence and Space Company EADS France filed Critical European Aeronautic Defence and Space Company EADS France
Publication of WO2011064263A2 publication Critical patent/WO2011064263A2/fr
Anticipated expiration legal-status Critical
Publication of WO2011064263A3 publication Critical patent/WO2011064263A3/fr
Ceased legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
    • H02G3/36—Installations of cables or lines in walls, floors or ceilings
    • 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
    • B64C1/064—Stringers; Longerons
    • 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
    • B64C1/18—Floors
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
    • H02G3/36—Installations of cables or lines in walls, floors or ceilings
    • H02G3/38—Installations of cables or lines in walls, floors or ceilings the cables or lines being installed in preestablished conduits or ducts
    • H02G3/386—Installations of cables or lines in walls, floors or ceilings the cables or lines being installed in preestablished conduits or ducts in walls

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Laminated Bodies (AREA)
  • Non-Insulated Conductors (AREA)

Abstract

L'invention concerne un élément structural en matériau composite stratifié se présentant sous la forme d'un profilé allongé et comportant, dans une épaisseur de la stratification, trois noyaux constitués d'un matériau électriquement conducteur recouverts d'une enveloppe en matériau électriquement isolant. Les barycentres des trois noyaux sont disposés, selon une section transversale du profilé, aux sommets d'un triangle équilatéral.
PCT/EP2010/068145 2009-11-25 2010-11-24 Élément structural composite à transmission électrique de puissance intégrée Ceased WO2011064263A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0958371 2009-11-25
FR0958371A FR2953093B1 (fr) 2009-11-25 2009-11-25 Element structural composite a transmission electrique de puissance integree

Publications (2)

Publication Number Publication Date
WO2011064263A2 WO2011064263A2 (fr) 2011-06-03
WO2011064263A3 true WO2011064263A3 (fr) 2012-05-31

Family

ID=42270489

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2010/068145 Ceased WO2011064263A2 (fr) 2009-11-25 2010-11-24 Élément structural composite à transmission électrique de puissance intégrée

Country Status (2)

Country Link
FR (1) FR2953093B1 (fr)
WO (1) WO2011064263A2 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11014337B2 (en) 2016-12-14 2021-05-25 The Boeing Company Laminate structures comprising fiber-reinforced thermoplastic prepreg plies
US11077644B2 (en) 2016-12-14 2021-08-03 The Boeing Company Material systems and methods of manufacturing material systems
US11273622B2 (en) 2016-12-14 2022-03-15 The Boeing Company Stiffening elements that comprise integral current flowpaths

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2977733B1 (fr) * 2011-07-05 2018-07-27 European Aeronautic Defence And Space Company Eads France Structure assemblee a continuite electrique
FR2977861B1 (fr) * 2011-07-13 2015-01-16 Eads Europ Aeronautic Defence Traverse de support d'une structure d'un aeronef et aeronef associe
WO2013124854A1 (fr) * 2012-02-24 2013-08-29 Sigment Design Metals Ltd. Élément structurel composite
FR2995464B1 (fr) * 2012-09-08 2021-05-14 Cqfd Composites Poutre comportant des conducteurs electriques et systeme d'electrification utilisant de telles poutres
DE102015213271A1 (de) * 2015-07-15 2017-01-19 Siemens Aktiengesellschaft Flugzeug mit einer Tragstruktur zur Übertragung elektrischer Energie zwischen einer Energiequelle und einem Energieverbraucher
US10053203B2 (en) * 2015-10-13 2018-08-21 The Boeing Company Composite stiffener with integral conductive element
FR3068952B1 (fr) * 2017-07-11 2019-07-26 Airbus Sas Fuselage et aeronef comportant une sous-structure multifonctionnelle de distribution d’air et procede d’assemblage
DE102019109149A1 (de) 2019-04-08 2020-10-08 Airbus Operations Gmbh Schiene zum Befestigen von Ausstattungselementen in Flugzeugen, insbesondere von Sitzen, und Verfahren zur Herstellung

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3531028A1 (de) * 1985-08-30 1987-03-05 Velden Alexander Jacobus Maria Versteifte struktur
WO2006124539A2 (fr) * 2005-05-12 2006-11-23 Armstrong World Industries, Inc. Conductivite electrique dans un systeme de plafond suspendu
DE102006050534A1 (de) * 2006-10-26 2008-04-30 Airbus Deutschland Gmbh Leitungssystem für ein Luftfahrzeug, insbesondere ein Flugzeug

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3531028A1 (de) * 1985-08-30 1987-03-05 Velden Alexander Jacobus Maria Versteifte struktur
WO2006124539A2 (fr) * 2005-05-12 2006-11-23 Armstrong World Industries, Inc. Conductivite electrique dans un systeme de plafond suspendu
DE102006050534A1 (de) * 2006-10-26 2008-04-30 Airbus Deutschland Gmbh Leitungssystem für ein Luftfahrzeug, insbesondere ein Flugzeug

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11014337B2 (en) 2016-12-14 2021-05-25 The Boeing Company Laminate structures comprising fiber-reinforced thermoplastic prepreg plies
US11077644B2 (en) 2016-12-14 2021-08-03 The Boeing Company Material systems and methods of manufacturing material systems
US11273622B2 (en) 2016-12-14 2022-03-15 The Boeing Company Stiffening elements that comprise integral current flowpaths
US12319027B2 (en) 2016-12-14 2025-06-03 The Boeing Company Methods of using stiffening elements that comprise one or more integral current flowpaths
US12370775B2 (en) 2016-12-14 2025-07-29 The Boeing Company Methods of manufacturing material systems
US12472725B2 (en) 2016-12-14 2025-11-18 The Boeing Company Methods of making laminate structures

Also Published As

Publication number Publication date
FR2953093B1 (fr) 2012-11-09
WO2011064263A2 (fr) 2011-06-03
FR2953093A1 (fr) 2011-05-27

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