FR2946009B1 - Panneau structurant composite de bord de fuite pour un element d'aeronef - Google Patents

Panneau structurant composite de bord de fuite pour un element d'aeronef

Info

Publication number
FR2946009B1
FR2946009B1 FR0902579A FR0902579A FR2946009B1 FR 2946009 B1 FR2946009 B1 FR 2946009B1 FR 0902579 A FR0902579 A FR 0902579A FR 0902579 A FR0902579 A FR 0902579A FR 2946009 B1 FR2946009 B1 FR 2946009B1
Authority
FR
France
Prior art keywords
stiffeners
panel
composite
edge
plies
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
FR0902579A
Other languages
English (en)
Other versions
FR2946009A1 (fr
Inventor
Didier Remene
Denis Millepied
Paulo Francisco
Valerian Montagne
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.)
Safran System Aerostructures SAS
Original Assignee
Societe Lorraine de Construction Aeronautique SA SLCA
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
Priority to FR0902579A priority Critical patent/FR2946009B1/fr
Application filed by Societe Lorraine de Construction Aeronautique SA SLCA filed Critical Societe Lorraine de Construction Aeronautique SA SLCA
Priority to PCT/FR2010/051040 priority patent/WO2010136741A2/fr
Priority to RU2011152302/11A priority patent/RU2560194C2/ru
Priority to BRPI1012058-0A priority patent/BRPI1012058B1/pt
Priority to ES10731774T priority patent/ES2739468T3/es
Priority to CA2757910A priority patent/CA2757910C/fr
Priority to EP10731774.5A priority patent/EP2435301B1/fr
Priority to CN201080021411.9A priority patent/CN102427999B/zh
Priority to US13/320,968 priority patent/US8936216B2/en
Publication of FR2946009A1 publication Critical patent/FR2946009A1/fr
Application granted granted Critical
Publication of FR2946009B1 publication Critical patent/FR2946009B1/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
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Laminated Bodies (AREA)
FR0902579A 2009-05-28 2009-05-28 Panneau structurant composite de bord de fuite pour un element d'aeronef Active FR2946009B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR0902579A FR2946009B1 (fr) 2009-05-28 2009-05-28 Panneau structurant composite de bord de fuite pour un element d'aeronef
RU2011152302/11A RU2560194C2 (ru) 2009-05-28 2010-05-28 Композитная конструктивная панель задней кромки элемента летательного аппарата
BRPI1012058-0A BRPI1012058B1 (pt) 2009-05-28 2010-05-28 Método para fabricar um painel de estruturação composto
ES10731774T ES2739468T3 (es) 2009-05-28 2010-05-28 Panel estructural de borde de salida de material compuesto para un elemento de una aeronave
PCT/FR2010/051040 WO2010136741A2 (fr) 2009-05-28 2010-05-28 Panneau structurant composite de bord de fuite pour un élément d'un aéronef
CA2757910A CA2757910C (fr) 2009-05-28 2010-05-28 Procede de fabrication d'un panneau structurant composite de bord de fuite pour un element d'un aeronef
EP10731774.5A EP2435301B1 (fr) 2009-05-28 2010-05-28 Procédé pour la fabrication d'un panneau structurant composite de bord de fuite pour un élément d'un aéronef
CN201080021411.9A CN102427999B (zh) 2009-05-28 2010-05-28 用于飞行器元件尾缘的复合结构面板以及制造该面板的方法
US13/320,968 US8936216B2 (en) 2009-05-28 2010-05-28 Composite structuring panel for the trailing edge of an aircraft element

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0902579A FR2946009B1 (fr) 2009-05-28 2009-05-28 Panneau structurant composite de bord de fuite pour un element d'aeronef

Publications (2)

Publication Number Publication Date
FR2946009A1 FR2946009A1 (fr) 2010-12-03
FR2946009B1 true FR2946009B1 (fr) 2011-07-08

Family

ID=41531614

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0902579A Active FR2946009B1 (fr) 2009-05-28 2009-05-28 Panneau structurant composite de bord de fuite pour un element d'aeronef

Country Status (1)

Country Link
FR (1) FR2946009B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2691962T3 (es) 2013-11-28 2018-11-29 Airbus Operations, S.L. Método para fabricar un borde de salida integrado de material compuesto
ES2889577T3 (es) 2018-07-06 2022-01-12 Airbus Operations Sl Método para fabricar las costillas del borde de salida y las costillas de soporte de los bordes de salida de superficies de elevación de aeronaves

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1264266B (de) * 1963-03-29 1968-03-21 Boelkow Gmbh Verfahren zum Herstellen von Rotorblaettern aus glasfaserverstaerktem Kunststoff
DE1275279B (de) * 1965-10-06 1968-08-14 Boelkow Gmbh Verfahren zum Herstellen eines Verbundbauteils aus glasfaserverstaerktem Kunststoff
US4657615A (en) * 1984-08-20 1987-04-14 The Boeing Company Composite leading edge/spar member for an aircraft control surface
EP1764307A1 (fr) * 2005-09-14 2007-03-21 EADS Construcciones Aeronauticas, S.A. Procédé de fabrication d'un bord d'attaque monolithique

Also Published As

Publication number Publication date
FR2946009A1 (fr) 2010-12-03

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