ES2082036T3 - Aparato y procedimiento para efectuar reparaciones de estructuras de aviones dañadas no sometidas a esfuerzos. - Google Patents

Aparato y procedimiento para efectuar reparaciones de estructuras de aviones dañadas no sometidas a esfuerzos.

Info

Publication number
ES2082036T3
ES2082036T3 ES91107530T ES91107530T ES2082036T3 ES 2082036 T3 ES2082036 T3 ES 2082036T3 ES 91107530 T ES91107530 T ES 91107530T ES 91107530 T ES91107530 T ES 91107530T ES 2082036 T3 ES2082036 T3 ES 2082036T3
Authority
ES
Spain
Prior art keywords
patch
sheet
cargo
pressure
tedlar
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 - Lifetime
Application number
ES91107530T
Other languages
English (en)
Inventor
Michael D Stewart
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of ES2082036T3 publication Critical patent/ES2082036T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/40—Maintaining or repairing aircraft
    • 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
    • Y10S428/00—Stock material or miscellaneous articles
    • Y10S428/92—Fire or heat protection feature
    • 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
    • Y10S428/00—Stock material or miscellaneous articles
    • Y10S428/92—Fire or heat protection feature
    • Y10S428/921—Fire or flameproofing
    • 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
    • Y10T428/14—Layer or component removable to expose adhesive
    • Y10T428/1424—Halogen containing compound
    • Y10T428/1429—Fluorine
    • 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
    • Y10T428/20—Patched hole or depression
    • 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.]
    • Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • Y10T428/2495—Thickness [relative or absolute]
    • 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.]
    • Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • Y10T428/2495—Thickness [relative or absolute]
    • Y10T428/24959—Thickness [relative or absolute] of adhesive layers
    • 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
    • Y10T428/28—Web or sheet containing structurally defined element or component and having an adhesive outermost layer
    • Y10T428/2848—Three or more layers
    • 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
    • Y10T428/28—Web or sheet containing structurally defined element or component and having an adhesive outermost layer
    • Y10T428/2852—Adhesive compositions
    • 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
    • Y10T428/28—Web or sheet containing structurally defined element or component and having an adhesive outermost layer
    • Y10T428/2852—Adhesive compositions
    • Y10T428/2857—Adhesive compositions including metal or compound thereof or natural rubber
    • 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
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/3154—Of fluorinated addition polymer from unsaturated monomers
    • 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
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31678—Of metal

Abstract

SE DESCRIBE UN APARATO Y METODO PARA EFECTUAR REPARACIONES EN LA ESTRUCTURA DAÑADA DE UN AVION QUE NO HA SIDO SOMETIDA A ESFUERZO. UNA LAMINA DE MATERIAL COMPUESTO DE TEJIDO DE VIDRIO HILADO IMPREGNADO CON UNA RESINA CURADA BAJO TEMPERATURA Y PRESION, FORMA EL PARCHE BASICO. UN LADO DEL PARCHE TIENE UN RECUBRIMIENTO TEDLAR ELEVADO * UNIDO A LA CARA DE LA LAMINA, EN UNA REALIZACION PREFERENTE. ESTE MATERIAL DE PARCHE CUMPLE CON LAS REGLAS DE AVIACION FEDERAL (FAR 25.855) QUE SE REQUIEREN PARA DOTAR A UN AVION DE TRANSPORTE CON MATERIAL IGNIFUGO. HAY UNA PELICULA SENSIBLE A LA PRESION UNIDA AL LADO OPUESTO DEL RECUBRIMIENTO DE TEDLAR ELEVADO *. ESTA COMBINACION DE LAMINA DE VIDRIO Y PELICULA SENSIBLE A LA PRESION, SE UNE POR PRESION A LA ESTRUCTURA DAÑADA Y SE MANTIENE MAS ADELANTE EN SU SITIO MEDIANTE UNOS SUJETADORES MECANICOS QUE PUEDEN SOPORTAR UNA TEMPERATURA DE POR LO MENOS 1.700 PRIMARIAS DE ESTA INVENCION ES EN LA REPARACION DE LINEAS DE CARGA DE AVIONES DE TRANSPORTE. UN JUEGO EN UNCOMPARTIMENTO DE CARGA DEBE DE MANTENERSE EN ESE AREA Y NO DEJARLE QUE SE EXTIENDA AL AVION DEBIDO AL DAÑO EN LA LINEA DE CARGA.
ES91107530T 1990-08-20 1991-05-08 Aparato y procedimiento para efectuar reparaciones de estructuras de aviones dañadas no sometidas a esfuerzos. Expired - Lifetime ES2082036T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US56955190A 1990-08-20 1990-08-20

Publications (1)

Publication Number Publication Date
ES2082036T3 true ES2082036T3 (es) 1996-03-16

Family

ID=24275902

Family Applications (1)

Application Number Title Priority Date Filing Date
ES91107530T Expired - Lifetime ES2082036T3 (es) 1990-08-20 1991-05-08 Aparato y procedimiento para efectuar reparaciones de estructuras de aviones dañadas no sometidas a esfuerzos.

Country Status (4)

Country Link
US (1) US5424105A (es)
EP (1) EP0471923B1 (es)
DE (1) DE69115792T2 (es)
ES (1) ES2082036T3 (es)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5626934A (en) * 1995-10-20 1997-05-06 United States Of America Enhancing damage tolerance of adhesive bonds
US6136116A (en) 1998-11-12 2000-10-24 Northrop Grumman Corporation Gap standardization technique for specialized fillers
US6174392B1 (en) 1999-03-04 2001-01-16 Northrop Grumman Corporation Composite structure repair process
US20040041356A1 (en) * 2000-05-12 2004-03-04 Aviation Devices And Electronic Components, Llc. Gasket material having a PTFE core and a method of making a using the same
US6656299B1 (en) * 2001-12-19 2003-12-02 Lockheed Martin Corporation Method and apparatus for structural repair
US6758924B1 (en) 2002-04-15 2004-07-06 The United States Of America As Represented By The Secretary Of The Air Force Method of repairing cracked aircraft structures
US8790485B2 (en) 2005-02-25 2014-07-29 Bell Helicopter Textron Inc. Single vacuum debulk composite panel repair
US20090193644A1 (en) * 2008-01-31 2009-08-06 Michael James Malloy Double nut bolted connection with cheese plate for reinforcing existing riveted or bolted structures under load
WO2009134299A2 (en) * 2008-03-14 2009-11-05 Kaneka Corporation Fire barrier protection for airplanes comprising graphite films
US20090289032A1 (en) * 2008-05-23 2009-11-26 General Electric Company Method and kit for surface preparation
FR2953812B1 (fr) * 2009-12-11 2012-09-07 Airbus Operations Sas Procede de reparation d'un fuselage d'aeronef
JPWO2011105540A1 (ja) * 2010-02-26 2013-06-20 三菱重工業株式会社 複合材の修理方法およびこれを用いた複合材
FR2970238B1 (fr) 2011-01-07 2013-01-25 Airbus Operations Sas Piece et procede de reparation d'une structure endommagee, en particulier de peau d'aeronef, ainsi qu'un kit de reparation de mise en oeuvre
DE102011004775B4 (de) * 2011-02-25 2012-10-25 Airbus Operations Gmbh Verfahren zum Herstellen einer Verbindung, Verbindung sowie Luft- oder Raumfahrzeug
US9388791B2 (en) * 2013-03-15 2016-07-12 Frontier Wind, Llc Mounting arrangement for load compensating device
DE102013216778A1 (de) * 2013-08-23 2015-02-26 Tesa Se Stanzling insbesondere zum dauerhaften Verschließen von Löchern
DE102013216782A1 (de) * 2013-08-23 2015-02-26 Tesa Se Stanzling insbesondere zum dauerhaften Verschließen von Löchern
GB2517954B (en) * 2013-09-05 2018-07-04 Airbus Operations Ltd Repair of a damaged composite aircraft wing
CN103803099B (zh) * 2014-02-21 2015-12-09 山东太古飞机工程有限公司 地板快速修理工艺
US20170348926A1 (en) * 2014-10-13 2017-12-07 Sikorsky Aircraft Corporation Repair and reinforcement method for an aircraft
JP6541742B2 (ja) * 2017-10-13 2019-07-10 三菱重工業株式会社 風車翼の補修方法
US20190152003A1 (en) * 2017-11-22 2019-05-23 Scott Gungel Strengthening Repair Wrap
US11312507B2 (en) * 2019-09-03 2022-04-26 The Boeing Company Repair assembly to repair an area on a member of a vehicle
US11919111B1 (en) * 2020-01-15 2024-03-05 Touchstone Research Laboratory Ltd. Method for repairing defects in metal structures

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3470048A (en) * 1964-11-25 1969-09-30 Carol J Jones Method of patching car bodies
US3850718A (en) * 1971-07-06 1974-11-26 S Trapani Metal patching plate and method of applying the same to damaged surfaces
US4147576A (en) * 1977-03-02 1979-04-03 Beem Lewis W Method of repairing a vehicle body
DE2718238C2 (de) * 1977-04-23 1982-06-16 Hoechst Ag, 6000 Frankfurt Verfahren zum Ausbessern von Schadstellen an emaillierten Behältern
US4407619A (en) * 1979-09-20 1983-10-04 Olympic Fastening Systems Blind fastener with deformable clamping means
US4517038A (en) * 1983-05-10 1985-05-14 Miller Robert W Method of repairing ballistic damage
US4473419A (en) * 1983-10-21 1984-09-25 Hardy Michael J Method of forming and bonding a panel repair patch
US4759812A (en) * 1985-07-11 1988-07-26 Miller Robert W Method and apparatus for effecting field repairs in stress carrying structures
US4661182A (en) * 1985-07-31 1987-04-28 Color Communications, Inc. Method and composition for repairing minor surface damage to coated surfaces
US4978404A (en) * 1986-07-21 1990-12-18 The Boeing Company Method for repairing a hole in a structural wall of composite material
US4732633A (en) * 1986-08-01 1988-03-22 Minnesota Mining And Manufacturing Company Method of patching damaged sheet material
US4726101A (en) * 1986-09-25 1988-02-23 United Technologies Corporation Turbine vane nozzle reclassification
AT386565B (de) * 1986-10-03 1988-09-12 Isovolta Reparier-laminat und seine verwendung
US4855182A (en) * 1986-10-03 1989-08-08 Isovolta Osterreichische Isolierstoffwerke Aktiengesellschaft Repair laminate
US4707391A (en) * 1987-01-27 1987-11-17 Pro Patch Systems, Inc. Vehicle body surface repair patch assembly
US4824500A (en) * 1987-11-03 1989-04-25 The Dow Chemical Company Method for repairing damaged composite articles
US4858853A (en) * 1988-02-17 1989-08-22 The Boeing Company Bolted repair for curved surfaces

Also Published As

Publication number Publication date
EP0471923A2 (en) 1992-02-26
DE69115792T2 (de) 1996-08-08
US5424105A (en) 1995-06-13
DE69115792D1 (de) 1996-02-08
EP0471923B1 (en) 1995-12-27
EP0471923A3 (en) 1992-10-28

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