ATE307755T1 - Ein verfahren für die abmontierbare und/oder feste zugkompressionsverbindung zur anwendung bei verbundmaterialien - Google Patents

Ein verfahren für die abmontierbare und/oder feste zugkompressionsverbindung zur anwendung bei verbundmaterialien

Info

Publication number
ATE307755T1
ATE307755T1 AT99500147T AT99500147T ATE307755T1 AT E307755 T1 ATE307755 T1 AT E307755T1 AT 99500147 T AT99500147 T AT 99500147T AT 99500147 T AT99500147 T AT 99500147T AT E307755 T1 ATE307755 T1 AT E307755T1
Authority
AT
Austria
Prior art keywords
skirt
laminate
composite materials
removable
application
Prior art date
Application number
AT99500147T
Other languages
English (en)
Inventor
Casado Rafael Dominguez
Perez Antonio Perez
Garcia Manuel Huertas
Castro Nodal Manuel De
Pancorbo Carlos Cerezo
Sacristan Bonifacio Robledo
Diez Cesar Grueso
Vara Enrique Redondo
Original Assignee
Airbus Espana Sl
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 Espana Sl filed Critical Airbus Espana Sl
Application granted granted Critical
Publication of ATE307755T1 publication Critical patent/ATE307755T1/de

Links

Classifications

    • 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
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S29/00—Metal working
    • Y10S29/003—Method or apparatus with bending
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49904—Assembling a subassembly, then assembling with a second subassembly
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49906—Metal deforming with nonmetallic bonding
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49947—Assembling or joining by applying separate fastener
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49947—Assembling or joining by applying separate fastener
    • Y10T29/49948—Multipart cooperating fastener [e.g., bolt and nut]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Connection Of Plates (AREA)
AT99500147T 1998-12-18 1999-08-17 Ein verfahren für die abmontierbare und/oder feste zugkompressionsverbindung zur anwendung bei verbundmaterialien ATE307755T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES009802635A ES2168027B1 (es) 1998-12-18 1998-12-18 Un procedimiento de union a traccion-compresion de caracter desmontable y/o fijo para aplicar a materiales compuestos.

Publications (1)

Publication Number Publication Date
ATE307755T1 true ATE307755T1 (de) 2005-11-15

Family

ID=8306137

Family Applications (1)

Application Number Title Priority Date Filing Date
AT99500147T ATE307755T1 (de) 1998-12-18 1999-08-17 Ein verfahren für die abmontierbare und/oder feste zugkompressionsverbindung zur anwendung bei verbundmaterialien

Country Status (6)

Country Link
US (1) US6415496B1 (de)
EP (1) EP1010615B1 (de)
AT (1) ATE307755T1 (de)
CA (1) CA2281130C (de)
DE (1) DE69927915T2 (de)
ES (1) ES2168027B1 (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2168027B1 (es) * 1998-12-18 2003-10-01 Airbus Espana Sl Un procedimiento de union a traccion-compresion de caracter desmontable y/o fijo para aplicar a materiales compuestos.
US6568744B2 (en) * 2001-05-29 2003-05-27 Terex Corporation Joint isolation system and a dump body incorporating the same
US6749155B2 (en) * 2002-09-13 2004-06-15 The Boeing Company Composite assembly with integrated composite joints
GB0609166D0 (en) * 2006-05-09 2006-06-21 Airbus Uk Ltd Apparatus for and method of inhibiting delamination
FR2903732B1 (fr) * 2006-07-12 2008-09-12 Airbus France Sas Entree d'air pour turbomoteur d'aeronef.
GB0619512D0 (en) * 2006-10-03 2006-11-15 Airbus Uk Ltd Fitting
FI119979B (fi) * 2007-03-12 2009-05-29 Patria Aerostructures Oy Ilma-aluksen kaarielementti ja komposiittilaippa
US8940213B2 (en) 2010-06-25 2015-01-27 The Boeing Company Resin infusion of composite parts using a perforated caul sheet
US9682514B2 (en) 2010-06-25 2017-06-20 The Boeing Company Method of manufacturing resin infused composite parts using a perforated caul sheet
US8636252B2 (en) * 2010-06-25 2014-01-28 The Boeing Company Composite structures having integrated stiffeners with smooth runouts and method of making the same
US8628717B2 (en) 2010-06-25 2014-01-14 The Boeing Company Composite structures having integrated stiffeners and method of making the same
US8679616B2 (en) * 2010-12-14 2014-03-25 The Boeing Company Skew-angle radius filler
FR2975970B1 (fr) * 2011-05-30 2013-05-17 Aircelle Sa Ensemble pour une nacelle d'aeronef
US10086922B2 (en) 2013-11-15 2018-10-02 The Boeing Company Low stress stiffener runout in Pi bonded structure
GB2528076B (en) * 2014-07-08 2020-07-29 Airbus Operations Ltd Rib foot
GB2528078B (en) * 2014-07-08 2020-07-29 Airbus Operations Ltd Structure
FR3081946B1 (fr) 2018-05-31 2020-09-04 Skf Aerospace France Ensemble de liaison comportant une piece de liaison et au moins deux pieces d'appui
US11180238B2 (en) * 2018-11-19 2021-11-23 The Boeing Company Shear ties for aircraft wing

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR863511A (fr) * 1940-02-22 1941-04-03 Bois Et Derives Sa Mode de liaison en bout de pièces peu épaisses
US4113910A (en) * 1977-04-27 1978-09-12 Rockwell International Corporation Composite load coupler for reinforcing composite structural joints
DE2721651C3 (de) 1977-05-13 1981-02-12 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Tragflügelhauptanschluß für Luft- und Raumfahrzeuge
US4219980A (en) * 1977-08-26 1980-09-02 Rockwell International Corporation Reinforced composite structure and method of fabrication thereof
US4331495A (en) * 1978-01-19 1982-05-25 Rockwell International Corporation Method of fabricating a reinforced composite structure
US4331723A (en) * 1980-11-05 1982-05-25 The Boeing Company Advanced composite
GB2105254B (en) * 1981-06-24 1984-05-10 Permabond Adhesives Top-hat stiffeners for grp and other panels of synethetic plastics materials
US4556592A (en) * 1981-09-25 1985-12-03 The Boeing Company Conductive joint seals for composite aircraft
US4966802A (en) * 1985-05-10 1990-10-30 The Boeing Company Composites made of fiber reinforced resin elements joined by adhesive
JPH0699288A (ja) * 1992-03-19 1994-04-12 Nippon Koku Uchu Kogyokai 金属基複合材料の接合方法
GB9215827D0 (en) * 1992-07-24 1992-09-09 British Aerospace A lightning shield
DE4329744C1 (de) 1993-09-03 1994-09-08 Deutsche Forsch Luft Raumfahrt Flügel mit Flügelschalen aus Faserverbundwerkstoffen, insbesondere CFK, für Luftfahrzeuge
DE19509340C2 (de) 1995-03-15 1998-12-03 Daimler Benz Aerospace Airbus Strukturelement
US5833786A (en) * 1996-05-16 1998-11-10 The Boeing Company Titanium radius filler for use in composite interfaces
ES2168027B1 (es) * 1998-12-18 2003-10-01 Airbus Espana Sl Un procedimiento de union a traccion-compresion de caracter desmontable y/o fijo para aplicar a materiales compuestos.

Also Published As

Publication number Publication date
DE69927915T2 (de) 2006-07-20
ES2168027A1 (es) 2002-05-16
US6415496B1 (en) 2002-07-09
EP1010615A3 (de) 2002-05-22
DE69927915D1 (de) 2005-12-01
CA2281130A1 (en) 2000-06-18
EP1010615B1 (de) 2005-10-26
EP1010615A2 (de) 2000-06-21
ES2168027B1 (es) 2003-10-01
CA2281130C (en) 2008-07-08

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