CA2297266C - Procede de fabrication de pieces en materiau composite a matrice thermoplastique - Google Patents

Procede de fabrication de pieces en materiau composite a matrice thermoplastique Download PDF

Info

Publication number
CA2297266C
CA2297266C CA002297266A CA2297266A CA2297266C CA 2297266 C CA2297266 C CA 2297266C CA 002297266 A CA002297266 A CA 002297266A CA 2297266 A CA2297266 A CA 2297266A CA 2297266 C CA2297266 C CA 2297266C
Authority
CA
Canada
Prior art keywords
blanks
skin
reinforcing elements
elements
manufacture
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
CA002297266A
Other languages
English (en)
French (fr)
Other versions
CA2297266A1 (fr
Inventor
Serge Maison
Serge Meunier
Cedric Thibout
Luc Mouton
Herve Payen
Philippe Vautey
Carole Coiffier-Colas
Joel Delbez
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.)
Dassault Aviation SA
Airbus Group SAS
Airbus Helicopters SAS
Original Assignee
Dassault Aviation SA
Airbus Group SAS
Eurocopter 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 Dassault Aviation SA, Airbus Group SAS, Eurocopter SA filed Critical Dassault Aviation SA
Publication of CA2297266A1 publication Critical patent/CA2297266A1/fr
Application granted granted Critical
Publication of CA2297266C publication Critical patent/CA2297266C/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12Construction or attachment of skin panels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/78Means for handling the parts to be joined, e.g. for making containers or hollow articles, e.g. means for handling sheets, plates, web-like materials, tubular articles, hollow articles or elements to be joined therewith; Means for discharging the joined articles from the joining apparatus
    • B29C65/7858Means for handling the parts to be joined, e.g. for making containers or hollow articles, e.g. means for handling sheets, plates, web-like materials, tubular articles, hollow articles or elements to be joined therewith; Means for discharging the joined articles from the joining apparatus characterised by the feeding movement of the parts to be joined
    • B29C65/7879Means for handling the parts to be joined, e.g. for making containers or hollow articles, e.g. means for handling sheets, plates, web-like materials, tubular articles, hollow articles or elements to be joined therewith; Means for discharging the joined articles from the joining apparatus characterised by the feeding movement of the parts to be joined said parts to be joined moving in a closed path, e.g. a rectangular path
    • B29C65/7882Means for handling the parts to be joined, e.g. for making containers or hollow articles, e.g. means for handling sheets, plates, web-like materials, tubular articles, hollow articles or elements to be joined therewith; Means for discharging the joined articles from the joining apparatus characterised by the feeding movement of the parts to be joined said parts to be joined moving in a closed path, e.g. a rectangular path said parts to be joined moving in a circular path
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112Single lapped joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/13Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
    • B29C66/131Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/301Three-dimensional joints, i.e. the joined area being substantially non-flat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/52Joining tubular articles, bars or profiled elements
    • B29C66/524Joining profiled elements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/61Joining from or joining on the inside
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721Fibre-reinforced materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721Fibre-reinforced materials
    • B29C66/7214Fibre-reinforced materials characterised by the length of the fibres
    • B29C66/72141Fibres of continuous length
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping 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
    • B29C70/32Shaping 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 on a rotating mould, former or core
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/86Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061Frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064Stringers; Longerons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068Fuselage sections
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/40General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/47Joining single elements to sheets, plates or other substantially flat surfaces
    • B29C66/474Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially non-flat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/53Joining single elements to tubular articles, hollow articles or bars
    • B29C66/532Joining single elements to the wall of tubular articles, hollow articles or bars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/71General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721Fibre-reinforced materials
    • B29C66/7212Fibre-reinforced materials characterised by the composition of the fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054Fuselage structures substantially made from particular materials
    • B64C2001/0072Fuselage structures substantially made from particular materials from composite materials
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1089Methods of surface bonding and/or assembly therefor of discrete laminae to single face of additional lamina

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Shaping Of Tube Ends By Bending Or Straightening (AREA)
CA002297266A 1997-07-22 1998-07-20 Procede de fabrication de pieces en materiau composite a matrice thermoplastique Expired - Fee Related CA2297266C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR9709265A FR2766407B1 (fr) 1997-07-22 1997-07-22 Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs
FR97/09265 1997-07-22
PCT/FR1998/001584 WO1999004952A1 (fr) 1997-07-22 1998-07-20 Procede de fabrication de pieces en materiau composite a matrice thermoplastique

Publications (2)

Publication Number Publication Date
CA2297266A1 CA2297266A1 (fr) 1999-02-04
CA2297266C true CA2297266C (fr) 2008-04-29

Family

ID=9509457

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002297266A Expired - Fee Related CA2297266C (fr) 1997-07-22 1998-07-20 Procede de fabrication de pieces en materiau composite a matrice thermoplastique

Country Status (9)

Country Link
US (1) US6613258B1 (enExample)
EP (1) EP0998383B1 (enExample)
JP (1) JP2001510746A (enExample)
CN (1) CN1077842C (enExample)
CA (1) CA2297266C (enExample)
DE (1) DE69809427T2 (enExample)
ES (1) ES2186202T3 (enExample)
FR (1) FR2766407B1 (enExample)
WO (1) WO1999004952A1 (enExample)

Families Citing this family (120)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6344213B1 (en) 1996-03-29 2002-02-05 Emisphere Technologies, Inc. Compounds and compositions for delivering active agents
OA12048A (en) 1999-10-08 2003-08-25 Anthony Khouri Vehicle mounted plastics drum for concrete mixing and methods of manufacture thereof.
US6889937B2 (en) 1999-11-18 2005-05-10 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
US7681835B2 (en) 1999-11-18 2010-03-23 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
US6823578B2 (en) * 2000-11-15 2004-11-30 Toyota Motor Sales, U.S.A., Inc. One-piece closed-shape structure and method of forming same
AUPS275302A0 (en) * 2002-05-31 2002-06-27 Khouri, Anthony Vehicle mounted concrete mixing drum and method of manufacture thereof
US7204951B2 (en) * 2002-07-30 2007-04-17 Rocky Mountain Composites, Inc. Method of assembling a single piece co-cured structure
US6729576B2 (en) * 2002-08-13 2004-05-04 Sikorsky Aircraft Corporation Composite tail cone assembly
MXPA06001791A (es) 2003-08-15 2007-04-17 Mcneilus Truck & Mfg Inc Escotilla de tambor mezclador.
US7744267B2 (en) 2003-08-15 2010-06-29 Mcneilus Truck And Manufacturing, Inc. Mixing drum drive ring
US7802914B2 (en) 2003-08-15 2010-09-28 McNeihus Truck and Manufacturing, Inc. Mixing drum blade support
US7282107B2 (en) * 2003-08-22 2007-10-16 The Boeing Company Multiple head automated composite laminating machine for the fabrication of large barrel section components
US8162529B2 (en) 2004-03-04 2012-04-24 Mcneilus Truck And Manufacturing, Inc. Mixing drum
ES2263324B1 (es) * 2004-03-18 2007-11-01 Manuel Torres Martinez Procedimiento para la fabricacion de fuselajes de aeronaves y dispositivo para llevar a cabo dicho procedimiento.
US7638084B2 (en) * 2004-03-19 2009-12-29 Frankel Kenneth A Methods for forming fiber reinforced composite parts having one or more selectively positioned core, structural insert, or veneer pieces integrally associated therewith
US7159822B2 (en) * 2004-04-06 2007-01-09 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7134629B2 (en) * 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
FR2872782B1 (fr) * 2004-07-08 2007-10-05 Airbus France Sas Plancher pour aeronef
US7325771B2 (en) 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US7503368B2 (en) * 2004-11-24 2009-03-17 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
EP1666353B1 (en) * 2004-12-06 2010-02-10 Saab Ab Method for fabricating a curved beam from composite material
FR2879496B1 (fr) * 2004-12-16 2008-12-12 Eurocopter France Procede et dispositif de fabrication d'une carene de rotor d'helicoptere, et carene obtenue
US7410352B2 (en) 2005-04-13 2008-08-12 The Boeing Company Multi-ring system for fuselage barrel formation
US8632653B2 (en) 2005-05-03 2014-01-21 The Boeing Company Method of manufacturing curved composite structural elements
FR2894869B1 (fr) * 2005-12-20 2009-10-09 Airbus France Sas Procede de fabrication d'un fuselage d'aeronef en materiau composite
EP1800840B1 (en) * 2005-12-20 2008-10-01 Saab Ab A stiffening element and a method for manufacturing of a stiffening element
US7459048B2 (en) * 2006-01-31 2008-12-02 The Boeing Company One-piece inner shell for full barrel composite fuselage
DE102006044683A1 (de) * 2006-02-07 2007-08-23 Grob, Margret Flugzeugkörper und Verfahren zu seiner Herstellung
WO2007113344A1 (es) 2006-03-31 2007-10-11 Airbus España, S.L. Procedimiento de fabricacion de estructuras de material compuesto con un utillaje colapsable de material inerte
CN101448627A (zh) * 2006-03-31 2009-06-03 空客西班牙公司 用可收缩模具制造复合材料结构的方法
DE102006026170B4 (de) 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026169B4 (de) 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026168A1 (de) 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
ES2430554T3 (es) * 2006-08-31 2013-11-21 Airbus Operations S.L. Procedimiento y útil para la fabricación de componentes tubulares para fuselajes aeronáuticos
CN100411856C (zh) * 2006-09-29 2008-08-20 连云港中复连众复合材料集团有限公司 一种玻璃钢曲面模塑格栅的制作工艺
US7871040B2 (en) * 2006-11-10 2011-01-18 The Boeing Company Composite aircraft structures with hat stiffeners
USD615919S1 (en) 2006-12-01 2010-05-18 Airbus Sas Set of partitions for a commercial aircraft passenger cabin
USD621330S1 (en) * 2006-12-01 2010-08-10 Airbus Sas Partition for a commercial aircraft passenger cabin
USD621331S1 (en) * 2006-12-01 2010-08-10 Airbus Sas Partition for a commercial aircraft passenger cabin
USD621329S1 (en) * 2006-12-01 2010-08-10 Airbus Sas Partition for a commercial aircraft passenger cabin
GB0624208D0 (en) * 2006-12-04 2007-01-10 Airbus Uk Ltd Composite structure
EP1932652A1 (en) * 2006-12-11 2008-06-18 Saab Ab A method and apparatus for manufacturing a curved elongated structural element
US8691037B2 (en) * 2006-12-14 2014-04-08 The Boeing Company Method for minimizing fiber distortion during fabrication of one-piece composite barrel section
ES2432567T3 (es) * 2007-01-30 2013-12-04 Airbus Operations S.L. Estructura de material compuesto para fuselaje de aeronave y su procedimiento de fabricación
WO2008104613A2 (es) * 2007-02-27 2008-09-04 Airbus España, S.L. Método para diseñar una pieza de material compuesto de superficie curva
US8388795B2 (en) 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
EP2159038A4 (en) * 2007-05-28 2017-08-02 Airbus Operations S.L. Method and tool for producing composite-material structures
US20080302912A1 (en) * 2007-06-08 2008-12-11 The Boeing Company Bladderless Mold Line Conformal Hat Stringer
US8043554B2 (en) 2007-06-08 2011-10-25 The Boeing Company Manufacturing process using bladderless mold line conformal hat stringer
US8043458B2 (en) * 2007-06-21 2011-10-25 Sikorsky Aircraft Corporation Method of forming panels using an in-situ tape placement process and panels formed therefrom
DE102007037649A1 (de) * 2007-08-09 2009-02-12 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Bauteils sowie faserverstärktes thermoplastisches Bauteil
US8042767B2 (en) 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
FR2928295B1 (fr) * 2008-03-07 2017-12-08 Duqueine Rhone Alpes Procede et dispositif de moulage d'une piece courbe en materiau composite,et piece correspondante.
US9090028B2 (en) 2008-04-17 2015-07-28 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US8932423B2 (en) * 2008-04-17 2015-01-13 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US9278484B2 (en) 2008-04-17 2016-03-08 The Boeing Company Method and apparatus for producing contoured composite structures and structures produced thereby
US8349105B2 (en) * 2008-04-17 2013-01-08 The Boeing Company Curved composite frames and method of making the same
GB0807398D0 (en) * 2008-04-23 2008-05-28 Airbus Uk Ltd Improved method of tape laying of thermoplastic composite materials
ES2352941B1 (es) * 2008-05-16 2012-01-25 Airbus Operations, S.L. Estructura integrada de aeronave en material compuesto
DE102008028865B4 (de) * 2008-06-19 2015-04-02 Airbus Defence and Space GmbH Verfahren zur Herstellung von Faserverbund-Profilbauteilen, sowie Verwendung derartig hergestellter Faserverbund-Profilbauteile
US9238335B2 (en) * 2008-07-10 2016-01-19 The Boeing Company Mandrel for autoclave curing applications
US9327467B2 (en) 2008-07-10 2016-05-03 The Boeing Company Composite mandrel for autoclave curing applications
USD663256S1 (en) 2008-09-29 2012-07-10 Airbus Sas Commercial aircraft passenger cabin seat and partition
DE102008042452A1 (de) 2008-09-29 2010-04-08 Airbus Deutschland Gmbh Faserverbundbauteil zur Energieabsorption im Crash-Fall für ein Luft- oder Raumfahrzeug, Rumpfstrukturabschnitt eines Luft- oder Raumfahrzeugs und Luft- oder Raumfahrzeug
DE102008057247B3 (de) * 2008-11-13 2010-01-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. Paneel in einer Semimonocoque-Bauweise und Herstellungsverfahren dafür
DE102008044229A1 (de) * 2008-12-01 2010-06-10 Airbus Deutschland Gmbh Schalenbauteil für ein Luft- oder Raumfahrzeug
FR2942600A1 (fr) * 2009-02-27 2010-09-03 Airbus France Procede de compactage en cote finie d'une piece composite thermoplastique a fibres continues
ES2390318B1 (es) * 2009-03-10 2013-09-16 Airbus Operations, S.L. Estructura cerrada en material compuesto.
FR2943944A1 (fr) * 2009-04-06 2010-10-08 Eads Europ Aeronautic Defence Procede de fabrication d'un panneau raidi en materiau composite a matrice thermoplastique et panneau ainsi obtenu
DE102009057006A1 (de) 2009-12-04 2011-06-09 Eads Deutschland Gmbh Vorrichtung und Verfahren zur Herstellung eines gekrümmten Verbundbauteils sowie Verbundbauteil
DE102009057009B4 (de) 2009-12-04 2015-01-08 Airbus Defence and Space GmbH Vorrichtung und Verfahren zur Herstellung eines schalenförmigen Verbundbauteils
DE102009056978A1 (de) * 2009-12-07 2011-06-09 Airbus Operations Gmbh Vorrichtung und Verfahren zur Herstellung einer aus einem Faserverbundwerkstoff bestehenden Rumpfschale für ein Luftfahrzeug
DE102009060695A1 (de) * 2009-12-29 2011-07-07 Airbus Operations GmbH, 21129 Flugzeugrumpf und Hautfeld
DE102010008711A1 (de) * 2010-02-19 2011-08-25 GKN Aerospace Services Limited, Isle of Wight Verfahren und Anordnung zur Herstellung eines einstückigen Hohlprofilbauteils mit Faserverbundwerkstoff
DE102010013713A1 (de) 2010-04-02 2011-10-06 Airbus Operations Gmbh Verfahren und Vorrichtung zur Herstellung eines faserverstärkten thermoplastischen Verbundbauteils
DE102010026018A1 (de) * 2010-07-03 2012-03-08 H. Bloeß - H.-J. Bloeß GbR (vertretungsberechtigter Gesellschafter Herr Heye Bloeß, Birkenweg 1, 26789 Leer) Rotorblatt für Windenergieanlagen in Wickeltechnik und unter Infusionsverfahren sowie Verfahren zu dessen Herstellung
FR2962409B1 (fr) * 2010-07-09 2012-09-21 Airbus Operations Sas Procede de realisation d'un caisson central de voilure
GB201013524D0 (en) * 2010-08-12 2010-09-29 Hexcel Composites Ltd Improved composite materials
US10071528B2 (en) 2010-12-08 2018-09-11 Bcomp Sa Stiffened thin-walled fibre composite products and method of making same
FR2975333B1 (fr) * 2011-05-19 2014-03-21 Daher Aerospace Panneau composite raidi double face et procede de realisation d'un tel panneau
US8844873B2 (en) * 2011-09-23 2014-09-30 The Boeing Company Stabilizer torque box assembly and method
US9649820B1 (en) 2012-02-08 2017-05-16 Textron Innovations, Inc. Assembly using skeleton structure
US9051062B1 (en) * 2012-02-08 2015-06-09 Textron Innovations, Inc. Assembly using skeleton structure
FR2987304B1 (fr) 2012-02-29 2018-03-02 Daher Aerospace Procede de formage par estampage d'un materiau composite thermoplastique a renfort fibreux continu
US8844760B2 (en) * 2012-08-08 2014-09-30 CNG Storage Solutions, LLC Storage vessel for compressed fluids
US9333713B2 (en) 2012-10-04 2016-05-10 The Boeing Company Method for co-curing composite skins and stiffeners in an autoclave
FR2998545B1 (fr) * 2012-11-23 2016-10-28 Airbus Operations Sas Nacelle d'aeronef comprenant une liaison renforcee entre une entree d'air et une motorisation
FR3000470B1 (fr) 2012-12-28 2015-12-25 Airbus Operations Sas Peau auto-raidie pour fuselage d'aeronef comprenant des lisses a section fermee et procede de fabrication associe
EP2878432B1 (en) * 2013-11-29 2019-01-02 Airbus Operations GmbH Method and system for producing composite component
CN103644083A (zh) * 2013-12-06 2014-03-19 内蒙古金岗重工有限公司 一种风力发电机的复合材料塔筒及其制备方法和制备模具
FR3015346B1 (fr) * 2013-12-19 2016-06-24 Aerolia Procede de fabrication d'une piece de fuselage d'aeronef, piece de fuselage obtenue par un tel procede et aeronef equipe d'une telle piece de fuselage
WO2015162401A2 (en) 2014-04-24 2015-10-29 Bae Systems Plc Assembly tool production
WO2015162406A2 (en) * 2014-04-24 2015-10-29 Bae Systems Plc Production of airframe components
US10364046B2 (en) 2014-04-24 2019-07-30 Bae Systems Plc Airframe production
RU2568515C1 (ru) * 2014-07-01 2015-11-20 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш") Ленточный препрег для изготовления теплозащитного покрытия силовой оболочки корпуса возвращаемого с гиперзвуковыми скоростями летательного аппарата
DE102014109362B4 (de) * 2014-07-04 2016-03-03 Airbus Operation GmbH Luftfahrzeugstrukturkomponente
PL2979975T3 (pl) * 2014-07-30 2018-01-31 Airbus Helicopters Deutschland GmbH Statek powietrzny ze strukturą ramową, która zawiera co najmniej jedną pustą ramę
GB2532451B (en) 2014-11-19 2018-12-26 Bae Systems Plc Object production
US10005267B1 (en) 2015-09-22 2018-06-26 Textron Innovations, Inc. Formation of complex composite structures using laminate templates
US20170087745A1 (en) * 2015-09-30 2017-03-30 The Boeing Company Fiber-reinforced Thermoplastic Composite Structure and Method for Making the Same
JP6254564B2 (ja) * 2015-11-18 2017-12-27 トヨタ自動車株式会社 タンクの製造方法およびタンク
DE102016201928B4 (de) * 2016-02-09 2024-02-08 Airbus Operations Gmbh Isolationsbauteil
DE102016210079A1 (de) * 2016-06-08 2017-12-14 Airbus Operations Gmbh Verfahren zum Herstellen eines Rumpfabschnitts
US11331867B2 (en) 2016-08-23 2022-05-17 Textron Innovations, Inc. Nested manufacturing of composite structures
EP3406434B1 (en) 2017-05-22 2024-12-25 Ratier-Figeac SAS Composite blade and method of manufacture
US11040512B2 (en) * 2017-11-08 2021-06-22 Northrop Grumman Systems Corporation Composite structures, forming apparatuses and related systems and methods
ES2981087T3 (es) * 2018-06-19 2024-10-07 Airbus Operations Slu Procedimiento de fabricación de una sección trasera de una aeronave y sección trasera de aeronave fabricada según dicho procedimiento
US11358348B2 (en) * 2019-01-02 2022-06-14 The Boeing Company Mold insert for use with a mandrel for forming a composite structure
FR3093947B1 (fr) * 2019-03-21 2021-04-09 Centre Techn Ind Mecanique Méthode et installation de fabrication de pièce de révolution en matériau composite
DE102019108769A1 (de) 2019-04-03 2020-10-08 Airbus Operations Gmbh Versteiftes flächiges Bauteil aus Polymermaterial und Verfahren zum Herstellen desselben
US11344942B2 (en) 2019-05-22 2022-05-31 The Boeing Company Actuator-based compensation for deformation of a mandrel
WO2021081208A1 (en) * 2019-10-22 2021-04-29 Arris Composites Inc. Method and apparatus for continuous fabrication of fiber-bundle-based and tape-base preforms
US11524468B2 (en) * 2020-02-03 2022-12-13 Rohr, Inc. Systems and methods for thermoplastic panel stretch/roll forming
EP4000845B1 (en) 2020-11-18 2024-06-12 The Boeing Company Fabrication systems and methods for fuselage sections
JP2022080868A (ja) 2020-11-18 2022-05-30 ザ・ボーイング・カンパニー 胴体セクションのための製造ライン、システム、及び方法
EP4000910B1 (en) 2020-11-18 2024-02-28 The Boeing Company Fabrication line, systems, and methods for fuselage sections
NL2027417B1 (en) * 2021-01-26 2022-08-26 Boeing Co Fabrication line, systems, and methods for fuselage sections
NL2027415B1 (en) * 2021-01-26 2022-08-26 Boeing Co Fabrication line, systems, and methods for fuselage sections
CN113844078B (zh) * 2021-07-20 2023-07-28 航天材料及工艺研究所 一种超轻质多特征无蒙皮骨架式复合材料壳体制备方法

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3300355A (en) * 1963-06-20 1967-01-24 William E Adams Method of making irregularly shaped hollow plastic bodies
US3906308A (en) * 1973-09-27 1975-09-16 Mc Donnell Douglas Corp Aircraft lightning protection system
DE3341564A1 (de) * 1983-11-17 1985-05-30 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Gekruemmtes flaechenbauteil, insbesondere fuer luftfahrzeuge und vorrichtung zu deren herstellung
US4946526A (en) * 1987-10-29 1990-08-07 Ltv Aerospace And Defense Company Method for compression molding of laminated panels
US4963215A (en) * 1987-12-07 1990-10-16 The Boeing Company Method for debulking precured thermoplastic composite laminae
US4937032A (en) * 1988-05-31 1990-06-26 Phillips Petroleum Company Method for molding a composite with an integrally molded rib
GB2225742A (en) * 1988-12-09 1990-06-13 Westland Helicopters Moulding a fibre reinforced composite, into a hollow structure comprising outer and inner skins connected by ribs
JP2935722B2 (ja) * 1990-02-28 1999-08-16 富士重工業株式会社 航空機の胴体構造およびその成形方法
US5223067A (en) * 1990-02-28 1993-06-29 Fuji Jukogyo Kabushiki Kaisha Method of fabricating aircraft fuselage structure
US5593633A (en) * 1990-05-03 1997-01-14 Dull; Kenneth M. Edge and surface breather for high temperature composite processing
DE4017978C2 (de) * 1990-06-05 1993-09-30 Dornier Luftfahrt Herstellung profilierter Stringer
US5326347A (en) * 1991-08-12 1994-07-05 Cumming J Stuart Intraocular implants
GB9118186D0 (en) * 1991-08-23 1991-10-09 British Aerospace Fusion bonded thermoplastic leading edge for aircraft aerodynamic
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
US5344602A (en) * 1992-08-14 1994-09-06 The Board Of Trustees Of The Leland Stanford Junior University Continuous forming of fiber composite materials
US5560102A (en) 1992-10-13 1996-10-01 The Boeing Company Panel and fuselage assembly

Also Published As

Publication number Publication date
FR2766407A1 (fr) 1999-01-29
EP0998383A1 (fr) 2000-05-10
FR2766407B1 (fr) 1999-10-15
EP0998383B1 (fr) 2002-11-13
CN1077842C (zh) 2002-01-16
WO1999004952A1 (fr) 1999-02-04
ES2186202T3 (es) 2003-05-01
CN1270551A (zh) 2000-10-18
CA2297266A1 (fr) 1999-02-04
DE69809427T2 (de) 2003-09-25
JP2001510746A (ja) 2001-08-07
US6613258B1 (en) 2003-09-02
DE69809427D1 (de) 2002-12-19

Similar Documents

Publication Publication Date Title
CA2297266C (fr) Procede de fabrication de pieces en materiau composite a matrice thermoplastique
CA2862686C (fr) Procede de formage par estampage d'un materiau composite thermoplastique a renfort fibreux continu
EP2064050B1 (fr) Procédé de fabrication d'un panneau en matériau composite thermoplastique
EP2170585B1 (fr) Bielle structurale en materiau composite et procede de realisation d 'une telle bielle
EP2225099B1 (fr) Procede de fabrication d'un panneau comprenant au moins un corps en nid-d'abeilles et une premiere peau realisee en materiau composite
CA2803974C (fr) Procede de realisation d'un caisson central de voilure
FR2661128A1 (fr) Procede et dispositif pour consolider un corps en materiau composite.
EP2709826B1 (fr) Panneau composite et son procédé de réalisation
EP2385894A1 (fr) Procédé de fabrication d'un panneau d'atténuation acoustique, notamment pour l'aéronautique
FR2726500A1 (fr) Procede pour la realisation de panneaux composites de type sandwich et panneaux ainsi obtenus
FR2655291A1 (fr) Procede de formage de pieces profilees convexes non developpables en materiau composite.
FR2635484A1 (fr) Procede et dispositifs de fabrication de pieces planes incurvees en materiau composite
EP2846987A1 (fr) Procédé de fabrication d'une peau en composite formant virole non démoulable
EP3625038A1 (fr) Procédé de réalisation d'une pièce coudée en matériau composite et pièce coudée correspondante
EP2510514A1 (fr) Procédé de fabrication de panneau acoustique pour nacelle d'aéronef
EP3945518B1 (fr) Matériau acoustique en bande à bride intégrée, et paroi interne d'une entrée d`air d`aéronef réalisée avec ce matériau
EP2578383B1 (fr) Procédé et dispositif pour la réalisation d'un trou à bord tombé dans un panneau composite
FR3061070A1 (fr) Procede de realisation d’un panneau auto raidi en materiaux composites et panneau obtenu par ledit procede
WO2025162883A1 (fr) Procédé de fabrication de pièces en matériau composite présentant des variations de section droite, et pièces obtenues par la mise en œuvre du procédé
WO2004067264A1 (fr) Procede de depose sur un support de couches fibreuses inclinees
FR2658116A1 (fr) Procede de raidissement des bordures d'une structure de remplissage en nid d'aveilles d'un panneau en materiau composite, procede de fabrication d'un tel panneau et panneau obtenu selon ce procede.
WO2025224258A1 (fr) Procédé de fabrication d'un élément composite 3d
WO2014199065A2 (fr) Procédé de fabrication d'une pièce composite
FR2988324A1 (fr) Procede pour la fabrication d'un cadre de hublot en materiau composite a renfort fibreux et hublot obtenu par un tel procede

Legal Events

Date Code Title Description
EEER Examination request
MKLA Lapsed