FR2686043A1 - Procede de realisation d'un panneau structurel du type sandwich et panneau ainsi obtenu. - Google Patents

Procede de realisation d'un panneau structurel du type sandwich et panneau ainsi obtenu. Download PDF

Info

Publication number
FR2686043A1
FR2686043A1 FR9200308A FR9200308A FR2686043A1 FR 2686043 A1 FR2686043 A1 FR 2686043A1 FR 9200308 A FR9200308 A FR 9200308A FR 9200308 A FR9200308 A FR 9200308A FR 2686043 A1 FR2686043 A1 FR 2686043A1
Authority
FR
France
Prior art keywords
panel
skins
heat
sealable
insert
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.)
Granted
Application number
FR9200308A
Other languages
English (en)
French (fr)
Other versions
FR2686043B1 (enrdf_load_stackoverflow
Inventor
Barbier Alain
Filippi Richard
Hardy Pascal
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.)
INDUPLAST SA
Original Assignee
INDUPLAST SA
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 INDUPLAST SA filed Critical INDUPLAST SA
Priority to FR9200308A priority Critical patent/FR2686043A1/fr
Publication of FR2686043A1 publication Critical patent/FR2686043A1/fr
Application granted granted Critical
Publication of FR2686043B1 publication Critical patent/FR2686043B1/fr
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D24/00Producing articles with hollow walls
    • B29D24/002Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
    • B29D24/005Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/12Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/02Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
    • E04C2/10Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products
    • E04C2/20Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products of plastics
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • E04C2/36Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels
    • E04C2/365Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels by honeycomb structures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00Layers arrangement
    • B32B2250/40Symmetrical or sandwich layers, e.g. ABA, ABCBA, ABCCBA
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/02Cellular or porous
    • B32B2305/024Honeycomb
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2607/00Walls, panels

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Wood Science & Technology (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
FR9200308A 1992-01-14 1992-01-14 Procede de realisation d'un panneau structurel du type sandwich et panneau ainsi obtenu. Granted FR2686043A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9200308A FR2686043A1 (fr) 1992-01-14 1992-01-14 Procede de realisation d'un panneau structurel du type sandwich et panneau ainsi obtenu.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9200308A FR2686043A1 (fr) 1992-01-14 1992-01-14 Procede de realisation d'un panneau structurel du type sandwich et panneau ainsi obtenu.

Publications (2)

Publication Number Publication Date
FR2686043A1 true FR2686043A1 (fr) 1993-07-16
FR2686043B1 FR2686043B1 (enrdf_load_stackoverflow) 1995-04-21

Family

ID=9425608

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9200308A Granted FR2686043A1 (fr) 1992-01-14 1992-01-14 Procede de realisation d'un panneau structurel du type sandwich et panneau ainsi obtenu.

Country Status (1)

Country Link
FR (1) FR2686043A1 (enrdf_load_stackoverflow)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0649736A1 (fr) * 1993-10-22 1995-04-26 Etablissements Manducher Tablette arrière de véhicule automobile et procédé de fabrication
WO1998004398A1 (fr) * 1996-07-30 1998-02-05 Peguform France Formation d'un insert dans un panneau en materiau composite du type sandwich a ame alveolaire
FR2768076A1 (fr) * 1997-09-10 1999-03-12 Peguform France Procede de realisation d'une zone rigidifiee formant insert dans un panneau composite du type sandwich, et panneau comprenant une telle zone
WO1999016660A1 (en) * 1997-09-17 1999-04-08 Ab Volvo Load-carrying vehicle structure of composite material and method for its moulding
WO2005010293A1 (fr) * 2003-07-28 2005-02-03 Xiamen New Technology Integrat Panneau composite a ame alveolaire en papier
WO2006102090A1 (en) * 2005-03-23 2006-09-28 The Boeing Company Integrated aircraft structural floor
RU2286428C2 (ru) * 2005-02-16 2006-10-27 Валериан Маркович Соболев Теплоизоляционный строительный элемент
AT503213B1 (de) * 2006-01-27 2007-10-15 Fischer Gmbh Skikern mit wabenförmigem aufbau
EP2818415A1 (en) * 2013-06-27 2014-12-31 Airbus Operations GmbH Panel member for an airframe
FR3032908A1 (fr) * 2015-02-24 2016-08-26 Airbus Defence & Space Sas Panneau composite renforce
FR3032905A1 (fr) * 2015-02-24 2016-08-26 Airbus Defence & Space Sas Panneau composite muni d'une terminaison d'assemblage perfectionnee et structure comportant un tel panneau
EP3144125A1 (en) * 2015-09-17 2017-03-22 The Boeing Company Panel and associated closeout method

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1513551A (fr) * 1967-01-06 1968-02-16 Procédé de réalisation de parois composites et parois composites ainsi obtenues
GB1475945A (en) * 1974-05-24 1977-06-10 Ver Flugtechnische Werke Cellular panel having reinforcing inserts
US4106962A (en) * 1977-07-14 1978-08-15 Ncr Corporation Method of fastening metal part to plastic part
DE3643688A1 (de) * 1985-12-28 1987-07-02 Sumitomo Light Metal Ind Plattenanordnung mit wabenstruktur
DE3644676A1 (de) * 1986-12-30 1988-07-14 Schladitz Klaus Verfahren zur herstellung von leichtbauteilen

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1513551A (fr) * 1967-01-06 1968-02-16 Procédé de réalisation de parois composites et parois composites ainsi obtenues
GB1475945A (en) * 1974-05-24 1977-06-10 Ver Flugtechnische Werke Cellular panel having reinforcing inserts
US4106962A (en) * 1977-07-14 1978-08-15 Ncr Corporation Method of fastening metal part to plastic part
DE3643688A1 (de) * 1985-12-28 1987-07-02 Sumitomo Light Metal Ind Plattenanordnung mit wabenstruktur
DE3644676A1 (de) * 1986-12-30 1988-07-14 Schladitz Klaus Verfahren zur herstellung von leichtbauteilen

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0649736A1 (fr) * 1993-10-22 1995-04-26 Etablissements Manducher Tablette arrière de véhicule automobile et procédé de fabrication
FR2711573A1 (fr) * 1993-10-22 1995-05-05 Manducher Sa Tablette arrière de véhicule automobile et procédé de fabrication.
WO1998004398A1 (fr) * 1996-07-30 1998-02-05 Peguform France Formation d'un insert dans un panneau en materiau composite du type sandwich a ame alveolaire
FR2751914A1 (fr) * 1996-07-30 1998-02-06 Manducher Sa Formation d'un insert dans un panneau en materiau composite du type sandwich a ame alveolaire
EP0903216A3 (fr) * 1997-09-10 2000-02-09 Peguform France Procédé de fabrication d'un panneau du type sandwich, rigidifié localement, et panneau ainsi obtenu
FR2768076A1 (fr) * 1997-09-10 1999-03-12 Peguform France Procede de realisation d'une zone rigidifiee formant insert dans un panneau composite du type sandwich, et panneau comprenant une telle zone
WO1999016660A1 (en) * 1997-09-17 1999-04-08 Ab Volvo Load-carrying vehicle structure of composite material and method for its moulding
US6482508B1 (en) 1997-09-17 2002-11-19 Ab Volvo Load-carrying vehicle structure of composite material and method for its moulding
WO2005010293A1 (fr) * 2003-07-28 2005-02-03 Xiamen New Technology Integrat Panneau composite a ame alveolaire en papier
RU2286428C2 (ru) * 2005-02-16 2006-10-27 Валериан Маркович Соболев Теплоизоляционный строительный элемент
CN101146710B (zh) * 2005-03-23 2011-08-10 波音公司 集成飞行器结构性地板
WO2006102090A1 (en) * 2005-03-23 2006-09-28 The Boeing Company Integrated aircraft structural floor
US7182291B2 (en) 2005-03-23 2007-02-27 The Boeing Company Integrated aircraft structural floor
JP2008534353A (ja) * 2005-03-23 2008-08-28 ザ・ボーイング・カンパニー 一体化された航空機構造用床材
AT503213B1 (de) * 2006-01-27 2007-10-15 Fischer Gmbh Skikern mit wabenförmigem aufbau
EP2818415A1 (en) * 2013-06-27 2014-12-31 Airbus Operations GmbH Panel member for an airframe
EP3470339A1 (en) * 2013-06-27 2019-04-17 Airbus Operations GmbH Panel member for an airframe
US10814957B2 (en) 2013-06-27 2020-10-27 Airbus Operations Gmbh Panel member for an airframe
FR3032908A1 (fr) * 2015-02-24 2016-08-26 Airbus Defence & Space Sas Panneau composite renforce
FR3032905A1 (fr) * 2015-02-24 2016-08-26 Airbus Defence & Space Sas Panneau composite muni d'une terminaison d'assemblage perfectionnee et structure comportant un tel panneau
WO2016135092A1 (fr) * 2015-02-24 2016-09-01 Airbus Defence And Space Sas Panneau composite muni d'une terminaison d'assemblage perfectionnée et structure comportant un tel panneau
WO2016135103A1 (fr) * 2015-02-24 2016-09-01 Airbus Defence And Space Sas Panneau composite renforcé
EP3144125A1 (en) * 2015-09-17 2017-03-22 The Boeing Company Panel and associated closeout method
US10155355B2 (en) 2015-09-17 2018-12-18 The Boeing Company Panel and associated closeout method

Also Published As

Publication number Publication date
FR2686043B1 (enrdf_load_stackoverflow) 1995-04-21

Similar Documents

Publication Publication Date Title
FR2686043A1 (fr) Procede de realisation d'un panneau structurel du type sandwich et panneau ainsi obtenu.
CA2862686C (fr) Procede de formage par estampage d'un materiau composite thermoplastique a renfort fibreux continu
FR2940176A1 (fr) Procede de fabrication d'un panneau d'attenuation acoustique, notamment pour l'aeronautique
FR2999970A1 (fr) Procede de realisation d'une preforme textile a fibres continues par circulation d'un flux de gaz chaud a travers un ensemble fibreux
EP0551776B1 (fr) Panneau composite structurel du type sandwich et son procédé de fabrication
EP2416946A2 (fr) Procede de fabrication d'un panneau raidi en materiau composite a matrice thermoplastique et panneau ainsi obtenu
FR2980732A1 (fr) Procede et dispositif pour le soudage d'un raidisseur thermoplastique
FR2806019A1 (fr) Procede de moulage-formage d'au moins une piece en un verre metallique
WO2019092371A1 (fr) Procédé de fabrication de panneau structural et/ou acoustique pour nacelle d'ensemble propulsif d'aéronef, et dispositif s'y rapportant
FR3056145A1 (fr) Procede de fabrication ameliore d'une piece de structure hybride de vehicule automobile et piece de structure hybride correspondante
FR2922276A1 (fr) Jonction triedre en materiau composite et procede de fabrication d'une telle jonction
CA2104315C (fr) Procede de fabrication d'assemblages composes de deux pieces collees et comportant une etape de formage
US7588179B2 (en) Bonding of carbon fibers to metal inserts for use in composites
EP3053734B1 (fr) Procede de fabrication de pieces en materiau composite
FR2751914A1 (fr) Formation d'un insert dans un panneau en materiau composite du type sandwich a ame alveolaire
EP4076914B1 (fr) Procédé et outillage pour la fabrication d'une coque quadrangulaire en matériau composite
FR2835216A1 (fr) Structure composite a parement de rigidite elevee, de tres faible epaisseur et integrant un super isolant sous vide
EP3512691A1 (fr) Procédé de fabrication amélioré d'une pièce de structure hybride de véhicule automobile et pièce de structure hybride correspondante
FR2691099A1 (fr) Dispositif pour solidariser entre eux des objets en matériaux composites par application simultanée de chaleur et de pression.
FR2766755A1 (fr) Procede pour realiser une piece en materiau sandwich a ame alveolaire pourvue d'une zone deformee en profondeur
EP1236554B1 (fr) Procédé de fabrication de pièces en matériaux composites
FR2698812A1 (fr) Procédé de fabrication de pièces comportant des espaces creux, et applications du procédé.
FR2890893A1 (fr) Piece de vehicule automobile comprenant une ame alveolaire et une peau
EP0558009A1 (fr) Procédé de fabrication d'un ski
JP3335271B2 (ja) 制振形材の製造方法

Legal Events

Date Code Title Description
CD Change of name or company name
ST Notification of lapse

Effective date: 20100930