DE69200705T2 - Thermoplastische, schmelzverbundene Vorderkante für die aerodynamischen Flächen eines Flugzeuges. - Google Patents

Thermoplastische, schmelzverbundene Vorderkante für die aerodynamischen Flächen eines Flugzeuges.

Info

Publication number
DE69200705T2
DE69200705T2 DE69200705T DE69200705T DE69200705T2 DE 69200705 T2 DE69200705 T2 DE 69200705T2 DE 69200705 T DE69200705 T DE 69200705T DE 69200705 T DE69200705 T DE 69200705T DE 69200705 T2 DE69200705 T2 DE 69200705T2
Authority
DE
Germany
Prior art keywords
aircraft
thermoplastic
melt
leading edge
aerodynamic surfaces
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
DE69200705T
Other languages
English (en)
Other versions
DE69200705D1 (de
Inventor
Christophe Domine
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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Publication of DE69200705D1 publication Critical patent/DE69200705D1/de
Application granted granted Critical
Publication of DE69200705T2 publication Critical patent/DE69200705T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • 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
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/1403—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation characterised by the type of electromagnetic or particle radiation
    • B29C65/1412—Infrared [IR] radiation
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General 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
    • B29C66/72—General 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
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General 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
    • B29C66/73—General 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
    • B29C66/739—General 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
    • B29C66/7392—General 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
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General 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
    • B29C66/74—Joining plastics material to non-plastics material
    • B29C66/742—Joining plastics material to non-plastics material to metals or their alloys
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B29L2031/3085—Wings
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S264/00—Plastic and nonmetallic article shaping or treating: processes
    • Y10S264/64—Processes of using preform in molding
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1028—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1028—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith
    • Y10T156/1031—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith with preshaping of lamina
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1089—Methods of surface bonding and/or assembly therefor of discrete laminae to single face of additional lamina
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1089—Methods of surface bonding and/or assembly therefor of discrete laminae to single face of additional lamina
    • Y10T156/109—Embedding of laminae within face of additional laminae
DE69200705T 1991-08-23 1992-08-18 Thermoplastische, schmelzverbundene Vorderkante für die aerodynamischen Flächen eines Flugzeuges. Expired - Fee Related DE69200705T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB919118186A GB9118186D0 (en) 1991-08-23 1991-08-23 Fusion bonded thermoplastic leading edge for aircraft aerodynamic

Publications (2)

Publication Number Publication Date
DE69200705D1 DE69200705D1 (de) 1995-01-05
DE69200705T2 true DE69200705T2 (de) 1995-03-30

Family

ID=10700410

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69200705T Expired - Fee Related DE69200705T2 (de) 1991-08-23 1992-08-18 Thermoplastische, schmelzverbundene Vorderkante für die aerodynamischen Flächen eines Flugzeuges.

Country Status (5)

Country Link
US (1) US5362347A (de)
EP (1) EP0529917B1 (de)
DE (1) DE69200705T2 (de)
ES (1) ES2064148T3 (de)
GB (1) GB9118186D0 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3733507A1 (de) * 2019-04-29 2020-11-04 Airbus Operations GmbH Vorderkantenbauteil für ein flugzeug

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7126096B1 (en) 1991-04-05 2006-10-24 Th Boeing Company Resistance welding of thermoplastics in aerospace structure
WO1996039326A1 (en) * 1995-06-06 1996-12-12 The Boeing Company Resistance welding of thermoplastics in aerospace structure
US6007894A (en) * 1997-07-10 1999-12-28 Mcdonnell Dougal Corporation Quasi-isotropic composite isogrid structure and method of making same
FR2766407B1 (fr) * 1997-07-22 1999-10-15 Aerospatiale Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs
US8920594B2 (en) * 2005-08-03 2014-12-30 Sikorsky Aircraft Corporation Composite thermoplastic matrix airframe structure and method of manufacture therefore
EP1764307A1 (de) * 2005-09-14 2007-03-21 EADS Construcciones Aeronauticas, S.A. Herstellungsverfahren einer monolithischen Flügelvorderkante
DE102005060958A1 (de) * 2005-12-20 2007-06-21 Airbus Deutschland Gmbh Schutzvorrichtung
DK1925436T3 (da) * 2006-11-23 2012-09-24 Siemens Ag Fremgangsmåde til fremstilling af et fiberforstærket laminat, anvendelse af laminatet, vindmøllevinge samt vindmølle omfattende laminatet
FR2918919B1 (fr) 2007-07-17 2013-03-29 Eurocopter France Procede et dispositif pour coller la coiffe metallique d'un bord d'attaque d'une voiture
FI20080208L (fi) * 2008-03-13 2008-03-27 Patria Aerostructures Oy Ilma-aluksen johtoreunaelementti, menetelmä sen valmistamiseksi sekä siipi ja vakain
US9126374B2 (en) 2010-09-28 2015-09-08 Russell B. Hanson Iso-grid composite component
FR2993857B1 (fr) * 2012-07-26 2015-03-27 Airbus Operations Sas Dispositif de protection d'une structure de longeron avant d'un caisson central d'aile d'aeronef et d'au moins un equipement situe dans ladite aile
EP2886452B1 (de) * 2013-12-18 2017-09-13 Airbus Operations GmbH Strömungskörper, Verfahren zur Herstellung eines Strömungskörpers und Flugzeug mit einem solchen Strömungskörper
GB2571508A (en) * 2017-12-13 2019-09-04 Airbus Operations Ltd Aerofoil structures
US11427302B2 (en) * 2019-04-01 2022-08-30 Yaborã Indústria Aeronáutica S.A. Closure fairings for wing leading edge slat track openings
US11084228B2 (en) 2019-04-08 2021-08-10 Rohr, Inc. Methods of joining and repairing composite components
EP4095031A1 (de) * 2021-05-28 2022-11-30 Airbus Operations GmbH Verfahren zur herstellung einer strukturellen komponente eines fahrzeugs und strukturelle komponente

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2749266A (en) * 1953-05-21 1956-06-05 Gen Tire & Rubber Co Method of making reinforced glass fiber articles
US4086378A (en) * 1975-02-20 1978-04-25 Mcdonnell Douglas Corporation Stiffened composite structural member and method of fabrication
US4492607A (en) * 1983-02-22 1985-01-08 Rockwell International Corporation Method for producing integrally stiffened fiber reinforced plastic panels
US4657615A (en) * 1984-08-20 1987-04-14 The Boeing Company Composite leading edge/spar member for an aircraft control surface
GB8508419D0 (en) * 1985-04-01 1985-05-09 Short Brothers Ltd Moulding fibre reinforced resin
NL8501678A (nl) * 1985-06-11 1987-01-02 Pols Erik Bernard Van Der Een nieuwe vervaardigingsmethode voor rackets.
US4721593A (en) * 1986-05-15 1988-01-26 Canadair Inc. Process for molding and curing a composite skin-stiffeners assembly
US5071500A (en) * 1987-06-23 1991-12-10 Honda Giken Kogyo Kabushiki Kaisha Method of and apparatus for fusing resin members such as bumper beam and bumper face of automobile bumper
US4937032A (en) * 1988-05-31 1990-06-26 Phillips Petroleum Company Method for molding a composite with an integrally molded rib
GB8829993D0 (en) * 1988-12-22 1989-02-15 Westland Helicopters Method for forming components from fibre-reinforced thermoplastic materials
US5064705A (en) * 1989-08-28 1991-11-12 United Technologies Corporation Stabilizing laminate inserts for resin transfer molding
US5096526A (en) * 1989-11-30 1992-03-17 The Boeing Company Core bonding and forming of thermoplastic laminates

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3733507A1 (de) * 2019-04-29 2020-11-04 Airbus Operations GmbH Vorderkantenbauteil für ein flugzeug
US11230365B2 (en) 2019-04-29 2022-01-25 Airbus Operations Gmbh Leading-edge component for an aircraft

Also Published As

Publication number Publication date
GB9118186D0 (en) 1991-10-09
US5362347A (en) 1994-11-08
EP0529917A1 (de) 1993-03-03
DE69200705D1 (de) 1995-01-05
ES2064148T3 (es) 1995-01-16
EP0529917B1 (de) 1994-11-23

Similar Documents

Publication Publication Date Title
DE69200705T2 (de) Thermoplastische, schmelzverbundene Vorderkante für die aerodynamischen Flächen eines Flugzeuges.
DE69015684T2 (de) Gekrümmter Flugwegübergang an Kursänderungspunkten für Flugzeuge.
DE69103018T2 (de) Aerodynamischer scheibenwischer.
DE68915261T2 (de) Windschutzscheibe für Flugzeuge.
ES521508A0 (es) Perfeccionamientos en un conjunto de tobera para un sistema de recubrimiento de articulos.
DE59100233D1 (de) Luftfrachtpalette.
DE69102394T2 (de) Funkensichere Struktur, insbesondere für Flugzeuge.
IT1229647B (it) Cabina per la verniciatura elettrostatica.
DE69102468T4 (de) Flüssigkeitsbehälter für Flugzeuge.
DE69502379T2 (de) Autopilot für hubschrauber mit sollwert für die luftgeschwindigkeit
DE58905892D1 (de) Cockpit, insbesondere für einen Hubschrauber.
NO153325C (no) Dekk, spesielt for fly.
DE69002048T2 (de) Stromlinienverkleidungen für Flugzeug.
AT368104B (de) Lufttransportsystem, insbesondere fuer montageteile
IT8220162A0 (it) Appoggia-gambe, specialmente per veicoli di trasporto e piu'particolarmente per aeronavi.
DE69103311T2 (de) Schleudersitz für Kampfflugzeug.
DE68915000T2 (de) Flügel schubdüse.
DE69101480D1 (de) Rasiergerät.
DE69105902D1 (de) Flugzeugbremse.
DE69106017D1 (de) Versorgungsvorrichtung für Flugzeugbesatzung.
DE69010356T2 (de) Abwerfbares aerodynamisches Ruder.
DE69109437D1 (de) Drehgelenk für Raumfahrzeug mit einem integriertem Stapelsystem.
DE59600481D1 (de) Linearantrieb für die verstellung eines elementes, insbesondere eines flügelelementes an einem flugzeug
DE59202594D1 (de) Verschwenkbare Leseleuchte für Fahrzeuge, insbesondere Flugzeuge.
FI931012A0 (fi) Transport- och/eller hanterings- och/eller bearbetningsanlaeggning foer jord, grus, sand, etc.

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee