ATE324971T1 - Verfahren zur herstellung von versteifungselementen für strukturkomponenten und vorrichtung zur durchführung des verfahrens - Google Patents

Verfahren zur herstellung von versteifungselementen für strukturkomponenten und vorrichtung zur durchführung des verfahrens

Info

Publication number
ATE324971T1
ATE324971T1 AT01963194T AT01963194T ATE324971T1 AT E324971 T1 ATE324971 T1 AT E324971T1 AT 01963194 T AT01963194 T AT 01963194T AT 01963194 T AT01963194 T AT 01963194T AT E324971 T1 ATE324971 T1 AT E324971T1
Authority
AT
Austria
Prior art keywords
implementing
structural components
stiffening elements
structural stiffening
producing
Prior art date
Application number
AT01963194T
Other languages
English (en)
Inventor
Allan Kaye
Original Assignee
Airbus Uk Ltd
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 Airbus Uk Ltd filed Critical Airbus Uk Ltd
Application granted granted Critical
Publication of ATE324971T1 publication Critical patent/ATE324971T1/de

Links

Classifications

    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00—Making preforms
    • B29B11/14—Making preforms characterised by structure or composition
    • B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • 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
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
    • 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
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • 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
    • Y10T156/1007—Running or continuous length work
    • Y10T156/1015—Folding
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/2419—Fold at edge
    • Y10T428/24198—Channel-shaped edge component [e.g., binding, etc.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Civil Engineering (AREA)
  • Architecture (AREA)
  • Textile Engineering (AREA)
  • Structural Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Rod-Shaped Construction Members (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Glass Compositions (AREA)
  • Treatment Of Steel In Its Molten State (AREA)
  • Heat Treatment Of Sheet Steel (AREA)
AT01963194T 2000-09-07 2001-08-31 Verfahren zur herstellung von versteifungselementen für strukturkomponenten und vorrichtung zur durchführung des verfahrens ATE324971T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0021955.0A GB0021955D0 (en) 2000-09-07 2000-09-07 Stiffening means for structural components

Publications (1)

Publication Number Publication Date
ATE324971T1 true ATE324971T1 (de) 2006-06-15

Family

ID=9899026

Family Applications (1)

Application Number Title Priority Date Filing Date
AT01963194T ATE324971T1 (de) 2000-09-07 2001-08-31 Verfahren zur herstellung von versteifungselementen für strukturkomponenten und vorrichtung zur durchführung des verfahrens

Country Status (10)

Country Link
US (1) US7546864B2 (de)
EP (1) EP1315609B1 (de)
AT (1) ATE324971T1 (de)
AU (1) AU2001284226A1 (de)
CA (1) CA2421455C (de)
DE (1) DE60119345T2 (de)
ES (1) ES2258544T3 (de)
GB (1) GB0021955D0 (de)
NO (1) NO323283B1 (de)
WO (1) WO2002020248A1 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006026167B3 (de) * 2006-06-06 2007-12-13 Airbus Deutschland Gmbh Leichtbau-Strukturpanel
GB0715303D0 (en) * 2007-08-08 2007-09-19 Airbus Uk Ltd Composite laminate structure
US8192169B2 (en) * 2010-04-09 2012-06-05 Frederick W Piasecki Highly reliable, low cost wind turbine rotor blade
DE102012206020A1 (de) 2012-04-12 2013-10-17 Airbus Operations Gmbh Verfahren und Vorrichtung zum Herstellen eines textilen Vorformlings
EP2808156B1 (de) 2013-05-28 2017-07-12 Airbus Operations GmbH Schalensegment eines Flugzeugs und Herstellungsverfahren
EP3007969B1 (de) * 2013-06-10 2020-01-01 Saab Ab Herstellungsverfahren einer stringerverstärkte verbundhaut und vorrichtung
WO2015094059A1 (en) * 2013-12-20 2015-06-25 Saab Ab Stiffening element and reinforced structure
EP3040191B1 (de) * 2014-12-30 2019-08-07 Airbus Operations, S.L. Verfahren zur Herstellung von Eckfüllungen aus Verbundwerkstoff
US9809297B2 (en) * 2015-08-26 2017-11-07 The Boeing Company Structures containing stiffeners having transition portions
FR3054160B1 (fr) * 2016-07-21 2019-05-17 Safran Nacelles Procede de drapage automatique de rubans de fibres seches

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1313234A (en) * 1919-08-12 john g
US2708648A (en) * 1950-11-15 1955-05-17 Eastman Kodak Co Method of sealing edges of wrapping material
US2822575A (en) * 1954-07-29 1958-02-11 Imbert Rene Process and machine for the continuous production of sections from synthetic resins
US2914108A (en) * 1955-02-07 1959-11-24 Bemis Bro Bag Co Seaming apparatus
US3928105A (en) * 1973-05-04 1975-12-23 Fiberglas Canada Ltd Automated apparatus and process for making match molded covering
US4151031A (en) 1977-07-05 1979-04-24 General Dynamics Corporation Apparatus for continuously forming composite shapes
FR2440831A1 (fr) 1978-11-07 1980-06-06 Dassault Avions Panneaux a base de fibres a haute resistance, particulierement applicables a la construction des avions
US4299871A (en) * 1979-09-04 1981-11-10 Grumman Aerospace Corporation Stitch bond fastening of composite structures
GB2072579B (en) 1980-04-01 1984-06-06 British Aerospace Stiffened panel of fibre reinforced plastics materials
US4966802A (en) 1985-05-10 1990-10-30 The Boeing Company Composites made of fiber reinforced resin elements joined by adhesive
US4749155A (en) 1985-09-30 1988-06-07 The Boeing Company Method of making wing box cover panel
FR2638673B1 (fr) 1988-11-08 1991-03-22 Aerospatiale Outillage pour le moulage de panneaux auto-raidis en materiau composite
WO1993004861A1 (en) * 1991-09-10 1993-03-18 Ralph Warwick Skoien Apparatus and method for making reflective batts
DE19529476C2 (de) 1995-08-11 2000-08-10 Deutsch Zentr Luft & Raumfahrt Flügel mit schubsteifen Flügelschalen aus Faserverbundwerkstoffen für Luftfahrzeuge
GB9810528D0 (en) * 1998-05-15 1998-07-15 British Aerospace Manufacture of stiffened composite structures
DE19832441C1 (de) * 1998-07-18 2000-01-05 Daimler Chrysler Aerospace Verfahren zur Herstellung einer stringerversteiften Schale in Faserverbundbauweise
US6620484B1 (en) * 2000-06-06 2003-09-16 The Boeing Company Variable density stitched-composite structural elements for energy absorption

Also Published As

Publication number Publication date
CA2421455A1 (en) 2002-03-14
NO20031059L (no) 2003-05-07
DE60119345T2 (de) 2006-08-31
ES2258544T3 (es) 2006-09-01
GB0021955D0 (en) 2000-10-25
US7546864B2 (en) 2009-06-16
EP1315609A1 (de) 2003-06-04
US20030180501A1 (en) 2003-09-25
DE60119345D1 (de) 2006-06-08
NO20031059D0 (no) 2003-03-07
NO323283B1 (no) 2007-02-26
CA2421455C (en) 2007-05-01
EP1315609B1 (de) 2006-05-03
WO2002020248A1 (en) 2002-03-14
AU2001284226A1 (en) 2002-03-22

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Legal Events

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