FR2986990B1 - Panneau auto-raidi en materiau composite et procede de realisation d'un tel panneau - Google Patents

Panneau auto-raidi en materiau composite et procede de realisation d'un tel panneau

Info

Publication number
FR2986990B1
FR2986990B1 FR1251480A FR1251480A FR2986990B1 FR 2986990 B1 FR2986990 B1 FR 2986990B1 FR 1251480 A FR1251480 A FR 1251480A FR 1251480 A FR1251480 A FR 1251480A FR 2986990 B1 FR2986990 B1 FR 2986990B1
Authority
FR
France
Prior art keywords
panel
raidi
self
producing
composite material
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
FR1251480A
Other languages
English (en)
Other versions
FR2986990A1 (fr
Inventor
Guillaume Gallant
Denis Soula
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 Operations SAS
Original Assignee
Airbus Operations 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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1251480A priority Critical patent/FR2986990B1/fr
Publication of FR2986990A1 publication Critical patent/FR2986990A1/fr
Application granted granted Critical
Publication of FR2986990B1 publication Critical patent/FR2986990B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/302—Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/52—Pultrusion, i.e. forming and compressing by continuously pulling through a die

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
FR1251480A 2012-02-17 2012-02-17 Panneau auto-raidi en materiau composite et procede de realisation d'un tel panneau Active FR2986990B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1251480A FR2986990B1 (fr) 2012-02-17 2012-02-17 Panneau auto-raidi en materiau composite et procede de realisation d'un tel panneau

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1251480A FR2986990B1 (fr) 2012-02-17 2012-02-17 Panneau auto-raidi en materiau composite et procede de realisation d'un tel panneau

Publications (2)

Publication Number Publication Date
FR2986990A1 FR2986990A1 (fr) 2013-08-23
FR2986990B1 true FR2986990B1 (fr) 2014-10-03

Family

ID=46022414

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1251480A Active FR2986990B1 (fr) 2012-02-17 2012-02-17 Panneau auto-raidi en materiau composite et procede de realisation d'un tel panneau

Country Status (1)

Country Link
FR (1) FR2986990B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150217850A1 (en) * 2014-02-06 2015-08-06 The Boeing Company Laminated i-blade stringer
US9856008B2 (en) * 2014-05-19 2018-01-02 The Boeing Company Composite structure and methods of forming thereof
FR3030443B1 (fr) * 2014-12-18 2016-12-09 Airbus Operations Sas Procede de fabrication d'un caisson central de voilure integrant au moins un longeron intermediaire et caisson central de voilure ainsi obtenu
FR3078011A1 (fr) * 2018-02-22 2019-08-23 Airbus Operations Procede de fabrication d'un caisson central de voilure a partir de profiles realises par formage a pression elevee et a basse temperature et caisson central de voilure obtenu a partir de la mise en œuvre dudit procede

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4606961A (en) * 1984-10-09 1986-08-19 The Boeing Company Discretely stiffened composite panel
FR2863197B1 (fr) * 2003-12-04 2006-03-03 Airbus France Procede de mise en place des elements d'un panneau auto-raidi en composite preimpregne
FR2863198B1 (fr) * 2003-12-04 2006-03-03 Airbus France Panneaux auto-raidis en composite pre-impregne et procedes de mise en place des elements de tels panneaux
BRPI0520816B1 (pt) * 2005-12-30 2016-12-13 Airbus Operations Sl “processo para fabricar painéis para estruturas aeronáuticas com membros de enrijecimento em forma de u e membros de enrijecimento em forma de i entre suas almas”
DE102008011410B4 (de) * 2008-02-27 2010-05-12 Airbus Deutschland Gmbh Pultrusionsverfahren zur Herstellung eines profilierten Preforms oder eines profilierten FVK-Bauteils, Pultrusionsanlage sowie Press-Vorrichtung zur Durchführung des Verfahrens

Also Published As

Publication number Publication date
FR2986990A1 (fr) 2013-08-23

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