ES2436728B2 - Pieza y método para la reparación de elementos longitudinales fabricados en material compuesto - Google Patents

Pieza y método para la reparación de elementos longitudinales fabricados en material compuesto Download PDF

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Publication number
ES2436728B2
ES2436728B2 ES201231009A ES201231009A ES2436728B2 ES 2436728 B2 ES2436728 B2 ES 2436728B2 ES 201231009 A ES201231009 A ES 201231009A ES 201231009 A ES201231009 A ES 201231009A ES 2436728 B2 ES2436728 B2 ES 2436728B2
Authority
ES
Spain
Prior art keywords
repair
composite material
holes
longitudinal elements
fragment
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.)
Active
Application number
ES201231009A
Other languages
English (en)
Other versions
ES2436728R1 (es
ES2436728A2 (es
Inventor
Alberto BALSA GONZÁLEZ
José Javier Almendros Gómez
Narciso RODRÍGUEZ GARCÍA
María Rocío FERNANDO MAGARZO
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 Operations 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 Operations SL filed Critical Airbus Operations SL
Priority to ES201231009A priority Critical patent/ES2436728B2/es
Priority to US13/928,047 priority patent/US20140017445A1/en
Publication of ES2436728A2 publication Critical patent/ES2436728A2/es
Publication of ES2436728R1 publication Critical patent/ES2436728R1/es
Application granted granted Critical
Publication of ES2436728B2 publication Critical patent/ES2436728B2/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • B29C73/04—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements
    • B29C73/10—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements using patches sealing on the surface of the article
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00—Restoring or reconditioning objects
    • 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
    • B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • B29C73/04—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements
    • 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
    • B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • B29C73/24—Apparatus or accessories not otherwise provided for
    • B29C73/26—Apparatus or accessories not otherwise provided for for mechanical pretreatment
    • B29C2073/268—Apparatus or accessories not otherwise provided for for mechanical pretreatment for drilling holes in the area to be repaired
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/04—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of riveting
    • 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
    • Y10T29/49718—Repairing
    • Y10T29/49732—Repairing by attaching repair preform, e.g., remaking, restoring, or patching
    • 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
    • Y10T29/49718—Repairing
    • Y10T29/49732—Repairing by attaching repair preform, e.g., remaking, restoring, or patching
    • Y10T29/49739—Mechanically attaching preform by 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
    • Y10T428/24322—Composite web or sheet

Abstract

Pieza y método para la reparación de elementos longitudinales fabricados en material compuesto.#La presente invención está dirigida a una pieza y a un método de reparación. La pieza de reparación es una pieza alargada, fabricada en material compuesto, que comprende dos porciones unidas formando un ángulo y una pluralidad de orificios en cada porción, dispuestos en la dirección de la línea de unión entre ambas porciones. El método de reparación comprende: proporcionar un fragmento de una pieza de reparación, de longitud suficiente para cubrir la zona dañada de la pieza a reparar manteniendo un margen para la fijación del fragmento de pieza de reparación; realizar orificios en ambas porciones de la pieza a reparar, de modo que la distancia entre los centros de orificios de reparación consecutivos sea la misma que entre los centros de los orificios consecutivos; y unir el fragmento de pieza de reparación a la pieza a reparar.

Description

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Claims (1)

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ES201231009A 2012-06-29 2012-06-29 Pieza y método para la reparación de elementos longitudinales fabricados en material compuesto Active ES2436728B2 (es)

Priority Applications (2)

Application Number Priority Date Filing Date Title
ES201231009A ES2436728B2 (es) 2012-06-29 2012-06-29 Pieza y método para la reparación de elementos longitudinales fabricados en material compuesto
US13/928,047 US20140017445A1 (en) 2012-06-29 2013-06-26 Repair part and repair method for repairing longitudinal elements made of a composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES201231009A ES2436728B2 (es) 2012-06-29 2012-06-29 Pieza y método para la reparación de elementos longitudinales fabricados en material compuesto

Publications (3)

Publication Number Publication Date
ES2436728A2 ES2436728A2 (es) 2014-01-03
ES2436728R1 ES2436728R1 (es) 2014-03-19
ES2436728B2 true ES2436728B2 (es) 2015-04-06

Family

ID=49767433

Family Applications (1)

Application Number Title Priority Date Filing Date
ES201231009A Active ES2436728B2 (es) 2012-06-29 2012-06-29 Pieza y método para la reparación de elementos longitudinales fabricados en material compuesto

Country Status (2)

Country Link
US (1) US20140017445A1 (es)
ES (1) ES2436728B2 (es)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2953812B1 (fr) * 2009-12-11 2012-09-07 Airbus Operations Sas Procede de reparation d'un fuselage d'aeronef
CN109789650A (zh) * 2016-09-27 2019-05-21 庞巴迪公司 用复合修复帽修复复合桁条的方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5374388A (en) * 1993-04-22 1994-12-20 Lockheed Corporation Method of forming contoured repair patches
US8540909B2 (en) * 2009-03-09 2013-09-24 The Boeing Company Method of reworking an area of a composite structure containing an inconsistency
FR2949208B1 (fr) * 2009-08-18 2014-02-21 Eads Europ Aeronautic Defence Procede de fabrication de pieces composites permettant une reparabilite desdites pieces
FR2953812B1 (fr) * 2009-12-11 2012-09-07 Airbus Operations Sas Procede de reparation d'un fuselage d'aeronef

Also Published As

Publication number Publication date
ES2436728R1 (es) 2014-03-19
ES2436728A2 (es) 2014-01-03
US20140017445A1 (en) 2014-01-16

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