DE69314175T2 - Gespleisste laminate für flugzeugrumpf - Google Patents

Gespleisste laminate für flugzeugrumpf

Info

Publication number
DE69314175T2
DE69314175T2 DE69314175T DE69314175T DE69314175T2 DE 69314175 T2 DE69314175 T2 DE 69314175T2 DE 69314175 T DE69314175 T DE 69314175T DE 69314175 T DE69314175 T DE 69314175T DE 69314175 T2 DE69314175 T2 DE 69314175T2
Authority
DE
Germany
Prior art keywords
laminates
split
aircraft fuselage
fuselage
aircraft
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
DE69314175T
Other languages
English (en)
Other versions
DE69314175D1 (de
Inventor
Carl E Garesche
Gerardus 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
Publication of DE69314175D1 publication Critical patent/DE69314175D1/de
Application granted granted Critical
Publication of DE69314175T2 publication Critical patent/DE69314175T2/de
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
DE69314175T 1992-07-09 1993-04-20 Gespleisste laminate für flugzeugrumpf Expired - Lifetime DE69314175T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/910,938 US5429326A (en) 1992-07-09 1992-07-09 Spliced laminate for aircraft fuselage
PCT/US1993/003750 WO1994001277A1 (en) 1992-07-09 1993-04-20 Spliced laminate for aircraft fuselage

Publications (2)

Publication Number Publication Date
DE69314175D1 DE69314175D1 (de) 1997-10-30
DE69314175T2 true DE69314175T2 (de) 1998-03-12

Family

ID=25429531

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69314175T Expired - Lifetime DE69314175T2 (de) 1992-07-09 1993-04-20 Gespleisste laminate für flugzeugrumpf

Country Status (7)

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

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007019716A1 (de) * 2007-04-26 2008-10-30 Airbus Deutschland Gmbh Faser-Metall-Laminat-Panel
US7803453B2 (en) 2006-05-17 2010-09-28 Airbus Deutschland Gmbh Laminated structure and method for producing a laminated structure
DE102012000508A1 (de) * 2012-01-13 2013-07-18 BOB Engineering GmbH Automation und Produktentwicklung Verfahren zur Herstellung eines GLARE-Bauteils
DE102012217543A1 (de) * 2012-09-27 2014-03-27 Siemens Aktiengesellschaft Verbundwerkstoff mit Faserverstärkung, Verwendung dazu und Elektromotor
US8783610B2 (en) 2007-10-31 2014-07-22 Airbus Operations Gmbh Transverse splicing plate for creating a fuselage, and a method for connecting two, in particular wound, CFP fuselage sections

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US7803453B2 (en) 2006-05-17 2010-09-28 Airbus Deutschland Gmbh Laminated structure and method for producing a laminated structure
DE102006023210B4 (de) * 2006-05-17 2012-12-13 Airbus Operations Gmbh Verfahren zum Herstellen einer Laminatstruktur, Laminatstruktur und deren Verwendung
DE102007019716A1 (de) * 2007-04-26 2008-10-30 Airbus Deutschland Gmbh Faser-Metall-Laminat-Panel
US8101284B2 (en) 2007-04-26 2012-01-24 Airbus Operations Gmbh Fibre metal laminate panel
US8783610B2 (en) 2007-10-31 2014-07-22 Airbus Operations Gmbh Transverse splicing plate for creating a fuselage, and a method for connecting two, in particular wound, CFP fuselage sections
DE102012000508A1 (de) * 2012-01-13 2013-07-18 BOB Engineering GmbH Automation und Produktentwicklung Verfahren zur Herstellung eines GLARE-Bauteils
DE102012217543A1 (de) * 2012-09-27 2014-03-27 Siemens Aktiengesellschaft Verbundwerkstoff mit Faserverstärkung, Verwendung dazu und Elektromotor

Also Published As

Publication number Publication date
DE69314175D1 (de) 1997-10-30
JP3212605B2 (ja) 2001-09-25
EP0649373B1 (de) 1997-09-24
ES2108275T3 (es) 1997-12-16
JPH08502217A (ja) 1996-03-12
WO1994001277A1 (en) 1994-01-20
US5429326A (en) 1995-07-04
EP0649373A1 (de) 1995-04-26
CA2139856C (en) 2004-01-27
CA2139856A1 (en) 1994-01-20

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