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1. WO2011069899 - METHOD FOR CONNECTING A FIBER COMPOSITE COMPONENT TO A STRUCTURAL COMPONENT OF AN AIR AND SPACECRAFT, AND A CORRESPONDING ARRANGEMENT

Publication Number WO/2011/069899
Publication Date 16.06.2011
International Application No. PCT/EP2010/068802
International Filing Date 03.12.2010
IPC
B29C 65/56 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
65Joining of preformed parts; Apparatus therefor
56using mechanical means
F16B 15/00 2006.01
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
16ENGINEERING ELEMENTS OR UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
15Nails; Staples
B29C 65/50 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
65Joining of preformed parts; Apparatus therefor
48using adhesives
50using adhesive tape
B64C 1/00 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like
B29K 105/06 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D103
105Condition, form or state of moulded material
06containing reinforcements, fillers or inserts
B29K 105/22 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D103
105Condition, form or state of moulded material
06containing reinforcements, fillers or inserts
20Inserts
22metallic
CPC
B23P 13/00
BPERFORMING OPERATIONS; TRANSPORTING
23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
13Making metal objects by operations essentially involving machining but not covered by a single other subclass
B29C 35/02
BPERFORMING OPERATIONS; TRANSPORTING
29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
35Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
02Heating or curing, e.g. crosslinking or vulcanizing ; during moulding, e.g. in a mould
B29C 65/344
BPERFORMING OPERATIONS; TRANSPORTING
29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
65Joining ; or sealing; of preformed parts ; , e.g. welding of plastics materials; Apparatus therefor
02by heating, with or without pressure
34using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
3404characterised by the type of heated elements which remain in the joint
344being a woven or non-woven fabric or being a mesh
B29C 65/3444
BPERFORMING OPERATIONS; TRANSPORTING
29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
65Joining ; or sealing; of preformed parts ; , e.g. welding of plastics materials; Apparatus therefor
02by heating, with or without pressure
34using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
3404characterised by the type of heated elements which remain in the joint
3444being a ribbon, band or strip
B29C 65/3448
BPERFORMING OPERATIONS; TRANSPORTING
29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
65Joining ; or sealing; of preformed parts ; , e.g. welding of plastics materials; Apparatus therefor
02by heating, with or without pressure
34using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
3404characterised by the type of heated elements which remain in the joint
3444being a ribbon, band or strip
3448said ribbon, band or strip being perforated
B29C 65/3476
BPERFORMING OPERATIONS; TRANSPORTING
29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
65Joining ; or sealing; of preformed parts ; , e.g. welding of plastics materials; Apparatus therefor
02by heating, with or without pressure
34using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
3472characterised by the composition of the heated elements which remain in the joint
3476being metallic
Applicants
  • AIRBUS OPERATIONS GMBH [DE]/[DE] (AllExceptUS)
  • PACCHIONE, Marco [IT]/[DE] (UsOnly)
  • FURFARI, Domenico [IT]/[DE] (UsOnly)
Inventors
  • PACCHIONE, Marco
  • FURFARI, Domenico
Agents
  • PECKMANN, Ralf
Priority Data
10 2009 047 671.708.12.2009DE
61/267,64308.12.2009US
Publication Language German (DE)
Filing Language German (DE)
Designated States
Title
(DE) VERFAHREN ZUM ANBINDEN EINES FASERVERBUNDBAUTEILS AN EIN STRUKTURBAUTEIL EINES LUFT- UND RAUMFAHRZEUGES UND EINE ENTSPRECHENDE ANORDNUNG
(EN) METHOD FOR CONNECTING A FIBER COMPOSITE COMPONENT TO A STRUCTURAL COMPONENT OF AN AIR AND SPACECRAFT, AND A CORRESPONDING ARRANGEMENT
(FR) PROCÉDÉ POUR RATTACHER UN ÉLÉMENT COMPOSITE RENFORCÉ PAR DES FIBRES À UN ÉLÉMENT DE STRUCTURE D'UN AÉRONEF ET D'UN VÉHICULE SPATIAL ET UN DISPOSITIF CORRESPONDANT
Abstract
(DE)
Bei einem Verfahren zum Anbinden eines Faserverbundbauteils (2) an ein Strukturbauteil (3) eines Luft- und Raumfahrzeuges, wird eine Metallfolie (4) als Querverstärkungselement zwischen dem Faserverbundbauteil (2) und dem Strukturbauteil (3) vorgesehen. Sie wird mit mindestens einem Verankerungsabschnitt (7), welcher von der dem Faserverbundbauteil (2) zugewandten Oberfläche (9) vorsteht ausgebildet und zwischen das Faserverbundbauteil (2) und dem Strukturbauteil (3) eingefügt. Eine entsprechende Anordnung ist nach diesem Verfahren hergestellt.
(EN)
The invention relates to a method for connecting a fiber composite component (2) to a structural component (3) of an air and spacecraft, wherein a metal foil (4) is provided between the fiber composite component (2) and the structural component (3) as a transverse reinforcement element. Said foil is designed having at least one anchoring segment (7) protruding from the surface (9) facing the fiber composite component (2), and inserted between the fiber composite component (2) and the structural component (3). A corresponding arrangement is produced according to said method.
(FR)
Dans un procédé pour rattacher un élément composite renforcé de fibres (2) à une partie structurale (3) d'un aéronef et d'un véhicule spatial, il est prévu une feuille de métal (4) comme élément de renfort transversal entre l'élément composite renforcé de fibres (2) et la partie structurale (3). Elle est fabriquée avec au moins une partie d'ancrage (7), qui est conçue en dépassant de la surface (9) tournée vers l'élément composite renforcé de fibres (2) et insérée entre l'élément composite renforcé de fibres (2) et la partie structurale (3). Un dispositif correspondant est fabriqué selon ce procédé.
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