DE69200705D1 - Thermoplastische, schmelzverbundene Vorderkante für die aerodynamischen Flächen eines Flugzeuges. - Google Patents
Thermoplastische, schmelzverbundene Vorderkante für die aerodynamischen Flächen eines Flugzeuges.Info
- Publication number
- DE69200705D1 DE69200705D1 DE69200705T DE69200705T DE69200705D1 DE 69200705 D1 DE69200705 D1 DE 69200705D1 DE 69200705 T DE69200705 T DE 69200705T DE 69200705 T DE69200705 T DE 69200705T DE 69200705 D1 DE69200705 D1 DE 69200705D1
- 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
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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Aviation & Aerospace Engineering (AREA)
- Health & Medical Sciences (AREA)
- Toxicology (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
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 true DE69200705D1 (de) | 1995-01-05 |
DE69200705T2 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) |
Families Citing this family (18)
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 |
EP1925436B1 (de) * | 2006-11-23 | 2012-08-29 | Siemens Aktiengesellschaft | Herstellungsverfahren für einen faserverstärkten Schichtstoff, Verwendung dieses Schichtstoffes, Windturbinenschaufel und Windturbine mit solchem Schichtstoff |
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 |
US11230365B2 (en) | 2019-04-29 | 2022-01-25 | Airbus Operations Gmbh | Leading-edge component for an aircraft |
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)
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 |
-
1991
- 1991-08-23 GB GB919118186A patent/GB9118186D0/en active Pending
-
1992
- 1992-08-18 ES ES92307536T patent/ES2064148T3/es not_active Expired - Lifetime
- 1992-08-18 EP EP92307536A patent/EP0529917B1/de not_active Expired - Lifetime
- 1992-08-18 DE DE69200705T patent/DE69200705T2/de not_active Expired - Fee Related
- 1992-08-19 US US07/932,297 patent/US5362347A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0529917B1 (de) | 1994-11-23 |
DE69200705T2 (de) | 1995-03-30 |
ES2064148T3 (es) | 1995-01-16 |
EP0529917A1 (de) | 1993-03-03 |
GB9118186D0 (en) | 1991-10-09 |
US5362347A (en) | 1994-11-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |