WO2009010357A3 - Verfahren und werkzeug zur herstellung eines t-stringers - Google Patents

Verfahren und werkzeug zur herstellung eines t-stringers Download PDF

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Publication number
WO2009010357A3
WO2009010357A3 PCT/EP2008/057608 EP2008057608W WO2009010357A3 WO 2009010357 A3 WO2009010357 A3 WO 2009010357A3 EP 2008057608 W EP2008057608 W EP 2008057608W WO 2009010357 A3 WO2009010357 A3 WO 2009010357A3
Authority
WO
WIPO (PCT)
Prior art keywords
stringer
sections
intermediate strips
producing
clamping device
Prior art date
Application number
PCT/EP2008/057608
Other languages
English (en)
French (fr)
Other versions
WO2009010357A4 (de
WO2009010357A2 (de
Inventor
Hauke Lengsfeld
Christian Luebbering
Original Assignee
Airbus Gmbh
Hauke Lengsfeld
Christian Luebbering
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 Gmbh, Hauke Lengsfeld, Christian Luebbering filed Critical Airbus Gmbh
Priority to US12/667,780 priority Critical patent/US8545659B2/en
Publication of WO2009010357A2 publication Critical patent/WO2009010357A2/de
Publication of WO2009010357A3 publication Critical patent/WO2009010357A3/de
Publication of WO2009010357A4 publication Critical patent/WO2009010357A4/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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/462—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • 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
    • B64C1/064—Stringers; Longerons
    • 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
    • Y10T156/1043—Subsequent to assembly
    • Y10T156/1049—Folding only

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

Die vorliegende Erfindung schafft ein Verfahren sowie ein Werkzeug (1, 48) zur Herstellung eines T-Stringers, insbesondere im Luft- und Raumfahrtbereich. Das Verfahren zeichnet sich dadurch aus, dass zwei Vorgelegestreifen {3, 4) aufeinander gelegt werden, wobei einem ausbildenden Stringerfuß (60) zugeordnete Abschnitte (5, 6) der Vorgelegestreifen (3, 4) voneinander mittels Trennfolien (7, 8) beabstandet werden und einem Stringersteg (61) zugeordnete Abschnitte (14, 15) der Vorgelegestreifen (3, 4) direkt, insbesondere stoffschlüssig, miteinander in Anlage gebracht werden. In einem weiteren Verfahrensschritt werden die Vorgelegestreifen (3, 4) an den dem auszubildenden Stringersteg (61) zugeordneten Abschnitten (5, 6) in eine Einspanneinrichtung (1) eingespannt. In einem noch weiteren Verfahrensschritt werden die dem ausbildenden Stringerfuß (60) zugeordneten Abschnitte (5, 6) in entgegengesetzte Richtung (28, 29) mittels eines Auffaltdorns (25) gefaltet und mittels einer Andrückwalze (37) gegen entsprechende Druckflächen (23, 24) der Einspanneinrichtung (1) gepresst, so dass die Abschnitte (5, 6) sauber fluchten. Abschließend werden die nun gefalteten Vorgelegestreifen (3, 4) zu dem herzustellenden T-Stringer ausgehärtet. Das erfindungsgemäße Verfahren weist gegenüber bekannten Verfahren zur Herstellung von T-Stringern den Vorteil auf, dass eine geringere Anzahl von Schritten erforderlich ist, um einen T-Stringer herzustellen, und dass sich diese einfach automatisieren lassen.
PCT/EP2008/057608 2007-07-13 2008-06-17 Verfahren und werkzeug zur herstellung eines t-stringers WO2009010357A2 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US12/667,780 US8545659B2 (en) 2007-07-13 2008-06-17 Method for producing a T-stringer

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US95937707P 2007-07-13 2007-07-13
US60/959,377 2007-07-13
DE102007032819.4 2007-07-13
DE102007032819.4A DE102007032819B4 (de) 2007-07-13 2007-07-13 Verfahren und Werkzeug zur Herstellung eines T-Stringers

Publications (3)

Publication Number Publication Date
WO2009010357A2 WO2009010357A2 (de) 2009-01-22
WO2009010357A3 true WO2009010357A3 (de) 2009-03-12
WO2009010357A4 WO2009010357A4 (de) 2009-04-30

Family

ID=40121515

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2008/057608 WO2009010357A2 (de) 2007-07-13 2008-06-17 Verfahren und werkzeug zur herstellung eines t-stringers

Country Status (3)

Country Link
US (1) US8545659B2 (de)
DE (1) DE102007032819B4 (de)
WO (1) WO2009010357A2 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2400129B1 (es) * 2011-05-30 2014-06-18 Airbus Operations, S.L. Método de fabricación de larguerillos con forma de "t" con un ángulo diferente de 90� entre el alma y el pie
US20170151719A1 (en) 2011-08-29 2017-06-01 Impossible Objects Llc Methods and Apparatus for Three-Dimensional Printed Composites Based on Folded Substrate Sheets
ES2413189B1 (es) * 2012-01-10 2015-02-11 Manuel Torres Martínez Instalacion para fabricar larguerillos de fibra para estructuras aeroespaciales
ES2529601B1 (es) * 2013-07-23 2015-10-09 Manuel Torres Martinez Molde para fabricar larguerillos de fibra para estructuras aeroespaciales y proceso para fabricar larguerillos de fibra con dicho molde
US9937998B2 (en) * 2015-02-19 2018-04-10 Rohr, Inc. Method for manufacturing a nacelle strake
DE102015211670A1 (de) * 2015-06-24 2016-12-29 Airbus Operations Gmbh Verfahren und Vorrichtung zur Serienfertigung von Bauteilen aus einem faserverstärkten Verbundmaterial
DE102016125958A1 (de) * 2016-12-30 2018-07-05 Airbus Operations Gmbh Werkzeug zum Formen eines T-förmigen Halbzeugs
US10780971B2 (en) * 2018-04-26 2020-09-22 The Boeing Company Methods of manufacturing a panel having a composite stringer for a vehicle
WO2021058350A1 (de) 2019-09-23 2021-04-01 Airbus Operations Gmbh Vorrichtungen und verfahren zur herstellung eines t-förmigen halbzeugs aus einem mehrlagigen gelege
DE102019125494A1 (de) * 2019-09-23 2021-03-25 Airbus Operations Gmbh Vorrichtung und Verfahren zur Herstellung eines T-förmigen Halbzeugs aus einem mehrlagigen Gelege

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6730184B2 (en) * 2000-05-01 2004-05-04 Honda Giken Kogyo Kabushiki Kaisha Method for producing fiber-reinforced composite semi-hardened product having joggle, and method for producing preformed structure using same
EP1481790A2 (de) * 2003-05-30 2004-12-01 Kawasaki Jukogyo Kabushiki Kaisha Verfahren und Vorrichtung zum Formen eines Profilstabs aus Verbundwerkstoff und geformter I-förmiger Profiltrager

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4287263A (en) * 1978-05-12 1981-09-01 Gaf Corporation Heat bondable asphaltic sound deadener
US6315759B1 (en) * 1999-12-21 2001-11-13 Travis Peterson Protective cover for intravenous lines and other elongated members

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6730184B2 (en) * 2000-05-01 2004-05-04 Honda Giken Kogyo Kabushiki Kaisha Method for producing fiber-reinforced composite semi-hardened product having joggle, and method for producing preformed structure using same
EP1481790A2 (de) * 2003-05-30 2004-12-01 Kawasaki Jukogyo Kabushiki Kaisha Verfahren und Vorrichtung zum Formen eines Profilstabs aus Verbundwerkstoff und geformter I-förmiger Profiltrager

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
ERMANNI, PAOLO: "Skript zur ETH-Vorlesung 151-0307-00L", August 2007, ETH ZÜRICH, ZÜRICH, XP002508229 *
ERMANNI, PAOLO: "WS 2005/06 - Composites Technologien - CFK-Rumpf in Nasswickel- und Prepregtechnik", 30 November 2005, ETH ZÜRICH, ZÜRICH, XP002508228 *

Also Published As

Publication number Publication date
DE102007032819A1 (de) 2009-01-15
WO2009010357A4 (de) 2009-04-30
DE102007032819B4 (de) 2014-08-28
US8545659B2 (en) 2013-10-01
US20100200156A1 (en) 2010-08-12
WO2009010357A2 (de) 2009-01-22

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