FR2953092B1 - Raidisseur electro-structural en materiau composite - Google Patents

Raidisseur electro-structural en materiau composite

Info

Publication number
FR2953092B1
FR2953092B1 FR0958370A FR0958370A FR2953092B1 FR 2953092 B1 FR2953092 B1 FR 2953092B1 FR 0958370 A FR0958370 A FR 0958370A FR 0958370 A FR0958370 A FR 0958370A FR 2953092 B1 FR2953092 B1 FR 2953092B1
Authority
FR
France
Prior art keywords
stiffener
layer
composite material
structural
electro
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.)
Expired - Fee Related
Application number
FR0958370A
Other languages
English (en)
Other versions
FR2953092A1 (fr
Inventor
Puertolas Jesus Aspas
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
Priority to FR0958370A priority Critical patent/FR2953092B1/fr
Priority to PCT/EP2010/068141 priority patent/WO2011064261A1/fr
Publication of FR2953092A1 publication Critical patent/FR2953092A1/fr
Application granted granted Critical
Publication of FR2953092B1 publication Critical patent/FR2953092B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • 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
    • 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

Landscapes

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

Abstract

L'invention concerne un raidisseur structural en matériau composite stratifié comportant une tête (11) maintenue à distance d'une semelle par laquelle ledit raidisseur est destiné à être fixé à un panneau. La tête (11 ) comporte un ensemble de couches superposées, dont au moins une couche structurale à base de fibres (111), au moins une couche à propriétés isolantes (118), et au moins une couche conductrice de réseau (113) intercalée entre ladite couche structurale et ladite couche isolante, et comportant un réseau d'éléments conducteurs électriques (120) prenant chacun naissance à une première extrémité à proximité d'une extrémité longitudinale du raidisseur et se terminant à une extrémité opposée à une extrémité longitudinale opposée du raidisseur.
FR0958370A 2009-11-25 2009-11-25 Raidisseur electro-structural en materiau composite Expired - Fee Related FR2953092B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0958370A FR2953092B1 (fr) 2009-11-25 2009-11-25 Raidisseur electro-structural en materiau composite
PCT/EP2010/068141 WO2011064261A1 (fr) 2009-11-25 2010-11-24 Raidisseur électro-structural en matériau composite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0958370A FR2953092B1 (fr) 2009-11-25 2009-11-25 Raidisseur electro-structural en materiau composite

Publications (2)

Publication Number Publication Date
FR2953092A1 FR2953092A1 (fr) 2011-05-27
FR2953092B1 true FR2953092B1 (fr) 2011-12-16

Family

ID=42697526

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0958370A Expired - Fee Related FR2953092B1 (fr) 2009-11-25 2009-11-25 Raidisseur electro-structural en materiau composite

Country Status (2)

Country Link
FR (1) FR2953092B1 (fr)
WO (1) WO2011064261A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3025310B1 (fr) * 2014-09-01 2016-11-04 Zodiac Aerotechnics Jauge de carburant

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2906218B1 (fr) * 2006-09-21 2009-05-15 Airbus France Sas Raidisseur autostabilise autorisant une reprise d'elements
FR2909919B1 (fr) * 2006-12-13 2012-12-07 Eads Ccr Procede de fabrication d'une piece complexe en materiau composite a fibres longues et a matrice thermodurcissable
US20090072098A1 (en) * 2007-09-17 2009-03-19 Inflight Investments Inc. Support bracket for mounting wires to floor beams of an aircraft
FR2924894B1 (fr) * 2007-12-10 2010-12-10 Eads Europ Aeronautic Defence Pieces en materiau composite electro-structural.
DE102007061425B4 (de) * 2007-12-20 2012-11-22 Airbus Operations Gmbh Halter zur bohrungslosen Befestigung von Komponenten, insbesondere von Leitungen innerhalb eines Flugzeugs
US8540833B2 (en) * 2008-05-16 2013-09-24 The Boeing Company Reinforced stiffeners and method for making the same

Also Published As

Publication number Publication date
WO2011064261A1 (fr) 2011-06-03
FR2953092A1 (fr) 2011-05-27

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