ATE385462T1 - Verfahren zur verstärkung einer doppelschalenkonstruktion - Google Patents

Verfahren zur verstärkung einer doppelschalenkonstruktion

Info

Publication number
ATE385462T1
ATE385462T1 AT02793614T AT02793614T ATE385462T1 AT E385462 T1 ATE385462 T1 AT E385462T1 AT 02793614 T AT02793614 T AT 02793614T AT 02793614 T AT02793614 T AT 02793614T AT E385462 T1 ATE385462 T1 AT E385462T1
Authority
AT
Austria
Prior art keywords
cavity
shell
reinforcing
shell construction
double shell
Prior art date
Application number
AT02793614T
Other languages
English (en)
Inventor
Anders Westerdahl
Max Krogager
Nils-Gunnar Jaktlund
Lars Loefgren
Original Assignee
Saab Ab
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 Saab Ab filed Critical Saab Ab
Application granted granted Critical
Publication of ATE385462T1 publication Critical patent/ATE385462T1/de

Links

Classifications

    • 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
    • B32B43/00—Operations specially adapted for layered products and not otherwise provided for, e.g. repairing; Apparatus therefor
    • 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
    • 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 shape; Layered products comprising a layer 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 shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • 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 shape; Layered products comprising a layer 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 shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/18—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by an internal layer formed of separate pieces of material which are juxtaposed side-by-side
    • B32B3/20—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by an internal layer formed of separate pieces of material which are juxtaposed side-by-side of hollow pieces, e.g. tubes; of pieces with channels or cavities
    • 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
    • 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
    • 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

Landscapes

  • Working Measures On Existing Buildindgs (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Laminated Bodies (AREA)
AT02793614T 2001-12-13 2002-12-09 Verfahren zur verstärkung einer doppelschalenkonstruktion ATE385462T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0104196A SE523364C2 (sv) 2001-12-13 2001-12-13 Metod för att förstärka en dubbelskalskonstruktion samt användning av metoden

Publications (1)

Publication Number Publication Date
ATE385462T1 true ATE385462T1 (de) 2008-02-15

Family

ID=20286306

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02793614T ATE385462T1 (de) 2001-12-13 2002-12-09 Verfahren zur verstärkung einer doppelschalenkonstruktion

Country Status (8)

Country Link
US (1) US7118640B2 (de)
EP (1) EP1458569B1 (de)
AT (1) ATE385462T1 (de)
AU (1) AU2002359107A1 (de)
DE (1) DE60224946T2 (de)
ES (1) ES2300501T3 (de)
SE (1) SE523364C2 (de)
WO (1) WO2003053693A1 (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2932346B2 (ja) * 1994-07-22 1999-08-09 富士通株式会社 印刷装置並びに印刷装置における印刷制御方法及び文字フォントパターン管理方法
EP1658924A1 (de) * 2004-11-22 2006-05-24 Siemens Aktiengesellschaft Bauteil mit einer aufgefüllten Vertiefung
US8108979B2 (en) * 2007-04-24 2012-02-07 United Technologies Corporation Using a stiffener to repair a part for an aircraft engine
US8091229B2 (en) * 2011-03-08 2012-01-10 General Electric Company Method of repairing a subsurface void or damage for a wind turbine blade

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB876106A (en) * 1959-11-11 1961-08-30 Frederick William Rohe An improved nut fastener for use with sandwich-type panels
US4978404A (en) 1986-07-21 1990-12-18 The Boeing Company Method for repairing a hole in a structural wall of composite material
US5207541A (en) * 1988-12-13 1993-05-04 The Boeing Company Scarfing apparatus
US5190611A (en) * 1991-02-13 1993-03-02 The Boeing Company Bearing load restoration method for composite structures

Also Published As

Publication number Publication date
WO2003053693A1 (en) 2003-07-03
SE0104196L (sv) 2003-06-14
US7118640B2 (en) 2006-10-10
EP1458569B1 (de) 2008-02-06
DE60224946T2 (de) 2009-01-29
SE0104196D0 (sv) 2001-12-13
ES2300501T3 (es) 2008-06-16
US20050109447A1 (en) 2005-05-26
AU2002359107A1 (en) 2003-07-09
SE523364C2 (sv) 2004-04-13
DE60224946D1 (de) 2008-03-20
EP1458569A1 (de) 2004-09-22

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Legal Events

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