ES2108275T3 - Laminado empalmado para fuselaje de aeronave. - Google Patents

Laminado empalmado para fuselaje de aeronave.

Info

Publication number
ES2108275T3
ES2108275T3 ES93910695T ES93910695T ES2108275T3 ES 2108275 T3 ES2108275 T3 ES 2108275T3 ES 93910695 T ES93910695 T ES 93910695T ES 93910695 T ES93910695 T ES 93910695T ES 2108275 T3 ES2108275 T3 ES 2108275T3
Authority
ES
Spain
Prior art keywords
joint
line
aircraft
metal layer
fuseling
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
ES93910695T
Other languages
English (en)
Inventor
Carl E Garesche
Gerardus H J J Roebroeks
Vuwe V Wimersma Greidanus
Rob C V Oost
Jan W Gunnink
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.)
Structural Laminates Co
Original Assignee
Structural Laminates Co
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 Structural Laminates Co filed Critical Structural Laminates Co
Application granted granted Critical
Publication of ES2108275T3 publication Critical patent/ES2108275T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/18—Layered products comprising a layer of metal comprising iron or steel
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2309/00—Parameters for the laminating or treatment process; Apparatus details
    • B32B2309/08—Dimensions, e.g. volume
    • B32B2309/10—Dimensions, e.g. volume linear, e.g. length, distance, width
    • B32B2309/105—Thickness
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00—Vehicles
    • B32B2605/18—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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/17—Surface bonding means and/or assemblymeans with work feeding or handling means
    • Y10T156/1702—For plural parts or plural areas of single part
    • Y10T156/1712—Indefinite or running length work
    • Y10T156/1722—Means applying fluent adhesive or adhesive activator material between 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
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24752—Laterally noncoextensive components

Abstract

UN PANEL DE CUERPO LAMINADO, PARA APLICACIONES EN AVIONES, COMPRENDE PRIMERA Y SEGUNDA CAPAS METALICAS Y UNA CAPA ADHESIVA. LAS SECCIONES PRIMERA Y SEGUNDA EN CADA CAPA METALICA SON GENERALMENTE COPLANARES Y SEPARADAS POR UNA LINEA DE JUNTA. UNA PRIMERA LINEA DE JUNTA EN UNA PRIMERA CAPA METALICA ES GENERALMENTE PARALELA A UNA SEGUNDA LINEA DE JUNTA EN UNA SEGUNDA CAPA METALICA, Y ESPACIADA LATERALMENTE DE LA SEGUNDA LINEA DE JUNTA. UNA CAPA ADHESIVA ENTRE LAS CAPAS METALICAS CONTIENE PREFERENTEMENTE FIBRAS DE REFORZAMIENTO PUENTEANDO LAS LINEAS DE JUNTA. UN FUSELAJE DE AVION, O ALA, O PLANOS DE COLA, HECHOS CON PANELES DE CUERPO EMPALMADOS DE LA INVENCION, TIENE MENOS JUNTAS Y PESOS MENORES QUE UNO HECHO CON PANELES DE CUERPO MAS ESTRECHOS, CONTENIENDO CAPAS METALICAS NO EMPALMADAS.
ES93910695T 1992-07-09 1993-04-20 Laminado empalmado para fuselaje de aeronave. Expired - Lifetime ES2108275T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/910,938 US5429326A (en) 1992-07-09 1992-07-09 Spliced laminate for aircraft fuselage

Publications (1)

Publication Number Publication Date
ES2108275T3 true ES2108275T3 (es) 1997-12-16

Family

ID=25429531

Family Applications (1)

Application Number Title Priority Date Filing Date
ES93910695T Expired - Lifetime ES2108275T3 (es) 1992-07-09 1993-04-20 Laminado empalmado para fuselaje de aeronave.

Country Status (7)

Country Link
US (1) US5429326A (es)
EP (1) EP0649373B1 (es)
JP (1) JP3212605B2 (es)
CA (1) CA2139856C (es)
DE (1) DE69314175T2 (es)
ES (1) ES2108275T3 (es)
WO (1) WO1994001277A1 (es)

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Also Published As

Publication number Publication date
DE69314175D1 (de) 1997-10-30
EP0649373B1 (en) 1997-09-24
US5429326A (en) 1995-07-04
EP0649373A1 (en) 1995-04-26
WO1994001277A1 (en) 1994-01-20
DE69314175T2 (de) 1998-03-12
JPH08502217A (ja) 1996-03-12
JP3212605B2 (ja) 2001-09-25
CA2139856C (en) 2004-01-27
CA2139856A1 (en) 1994-01-20

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