ES2168027B1 - Un procedimiento de union a traccion-compresion de caracter desmontable y/o fijo para aplicar a materiales compuestos. - Google Patents

Un procedimiento de union a traccion-compresion de caracter desmontable y/o fijo para aplicar a materiales compuestos.

Info

Publication number
ES2168027B1
ES2168027B1 ES009802635A ES9802635A ES2168027B1 ES 2168027 B1 ES2168027 B1 ES 2168027B1 ES 009802635 A ES009802635 A ES 009802635A ES 9802635 A ES9802635 A ES 9802635A ES 2168027 B1 ES2168027 B1 ES 2168027B1
Authority
ES
Spain
Prior art keywords
skirt
laminate
composite materials
removal
application
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
ES009802635A
Other languages
English (en)
Other versions
ES2168027A1 (es
Inventor
Casado Rafael Dominguez
Perez Antonio Perez
Garcia Manuel Huertas
Castro Nodal Manuel De
Pancorbo Carlos Cerezo
Sacristan Bonifacio Robledo
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.)
Airbus Operations SL
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
Priority to ES009802635A priority Critical patent/ES2168027B1/es
Priority to US09/354,804 priority patent/US6415496B1/en
Priority to EP99500147A priority patent/EP1010615B1/en
Priority to AT99500147T priority patent/ATE307755T1/de
Priority to DE69927915T priority patent/DE69927915T2/de
Priority to CA002281130A priority patent/CA2281130C/en
Publication of ES2168027A1 publication Critical patent/ES2168027A1/es
Application granted granted Critical
Publication of ES2168027B1 publication Critical patent/ES2168027B1/es
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
    • 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)

Abstract

Un procedimiento de unión a tracción-compresión de carácter desmontable y/o fijo para aplicar a materiales compuestos, en el que se pliega al menos una vez un laminado básico (1) de material compuesto para obtener al menos una faldilla (2) que forma un ángulo próximo a 90º con el resto del laminado, utilizando un radio de transición entre la faldilla y el resto del laminado, se aplica sobre el laminado básico un conjunto de placas de distribución (5, 6) para estabilizar la faldilla y producir una distribución de cargas de carácter uniforme, se practican taladros en cada conjunto de faldilla-placas de distribución y se introducen en dichos taladros unos bulones de tracción (4) con una pretensión inicial, produciéndose así la conexión entre los elementos que deben ser unidos. La invención es aplicable a estructuras aerodinámicas de aviones.
ES009802635A 1998-12-18 1998-12-18 Un procedimiento de union a traccion-compresion de caracter desmontable y/o fijo para aplicar a materiales compuestos. Expired - Fee Related ES2168027B1 (es)

Priority Applications (6)

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.
US09/354,804 US6415496B1 (en) 1998-12-18 1999-07-16 Process for making a dismountable and/or fixed traction-compression coupling to be applied to composite materials
EP99500147A EP1010615B1 (en) 1998-12-18 1999-08-17 A process for making a dismountable and/or fixed traction-compression joint to be applied to composite materials
AT99500147T ATE307755T1 (de) 1998-12-18 1999-08-17 Ein verfahren für die abmontierbare und/oder feste zugkompressionsverbindung zur anwendung bei verbundmaterialien
DE69927915T DE69927915T2 (de) 1998-12-18 1999-08-17 Ein Verfahren für die abmontierbare und/oder feste Zugkompressionsverbindung zur Anwendung bei Verbundmaterialien
CA002281130A CA2281130C (en) 1998-12-18 1999-08-30 A process for making a dismountable and/or fixed traction-compression coupling to be applied to composite materials

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 (2)

Publication Number Publication Date
ES2168027A1 ES2168027A1 (es) 2002-05-16
ES2168027B1 true ES2168027B1 (es) 2003-10-01

Family

ID=8306137

Family Applications (1)

Application Number Title Priority Date Filing Date
ES009802635A Expired - Fee Related 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.

Country Status (6)

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

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
US9682514B2 (en) 2010-06-25 2017-06-20 The Boeing Company Method of manufacturing resin infused composite parts using a perforated caul sheet
US8628717B2 (en) 2010-06-25 2014-01-14 The Boeing Company Composite structures having integrated stiffeners and method of making the same
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
US8940213B2 (en) 2010-06-25 2015-01-27 The Boeing Company Resin infusion of composite parts using a perforated caul sheet
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
EP1010615A2 (en) 2000-06-21
ES2168027A1 (es) 2002-05-16
DE69927915D1 (de) 2005-12-01
EP1010615A3 (en) 2002-05-22
US6415496B1 (en) 2002-07-09
CA2281130A1 (en) 2000-06-18
ATE307755T1 (de) 2005-11-15
CA2281130C (en) 2008-07-08
DE69927915T2 (de) 2006-07-20
EP1010615B1 (en) 2005-10-26

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Legal Events

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Effective date: 20110804

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Effective date: 20180921