DE60216454D1 - Flugzeugpaneel - Google Patents

Flugzeugpaneel

Info

Publication number
DE60216454D1
DE60216454D1 DE60216454T DE60216454T DE60216454D1 DE 60216454 D1 DE60216454 D1 DE 60216454D1 DE 60216454 T DE60216454 T DE 60216454T DE 60216454 T DE60216454 T DE 60216454T DE 60216454 D1 DE60216454 D1 DE 60216454D1
Authority
DE
Germany
Prior art keywords
high strength
aircraft panel
core material
strength material
grid
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
DE60216454T
Other languages
English (en)
Other versions
DE60216454T2 (de
Inventor
Mats Folkesson
Stefan Thuresson
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.)
Saab AB
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 DE60216454D1 publication Critical patent/DE60216454D1/de
Publication of DE60216454T2 publication Critical patent/DE60216454T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/18—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed 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
    • 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
    • B32B15/046—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 foam
    • 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
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • 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
    • B32B2250/00—Layers arrangement
    • B32B2250/03—3 layers
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/30—Properties of the layers or laminate having particular thermal properties
    • B32B2307/304—Insulating
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/56—Damping, energy absorption
    • 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
    • B32B2311/00—Metals, their alloys or their compounds
    • B32B2311/24—Aluminium
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
DE60216454T 2001-06-07 2002-04-30 Flugzeugpaneel Expired - Lifetime DE60216454T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE0102083 2001-06-07
SE0102083A SE519185C2 (sv) 2001-06-07 2001-06-07 Flygplanspanel
PCT/SE2002/000843 WO2002098734A1 (en) 2001-06-07 2002-04-30 Aircraft panel

Publications (2)

Publication Number Publication Date
DE60216454D1 true DE60216454D1 (de) 2007-01-11
DE60216454T2 DE60216454T2 (de) 2007-09-27

Family

ID=20284451

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60216454T Expired - Lifetime DE60216454T2 (de) 2001-06-07 2002-04-30 Flugzeugpaneel

Country Status (7)

Country Link
US (1) US7025305B2 (de)
EP (1) EP1399362B1 (de)
AT (1) ATE346789T1 (de)
DE (1) DE60216454T2 (de)
ES (1) ES2276935T3 (de)
SE (1) SE519185C2 (de)
WO (1) WO2002098734A1 (de)

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DE602004032122D1 (de) * 2003-02-24 2011-05-19 Bell Helicopter Textron Inc Kontaktversteifer für konstruktionshaut
NL1023811C2 (nl) * 2003-07-03 2005-01-04 Stork Fokker Aesp Bv Laminaat met plaatselijke versterking.
DE502004007968D1 (de) * 2003-07-08 2008-10-16 Airbus Gmbh Leichtbaustruktur
US7159822B2 (en) * 2004-04-06 2007-01-09 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7134629B2 (en) * 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7527222B2 (en) 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
DE102004018579A1 (de) * 2004-04-16 2005-11-03 Airbus Deutschland Gmbh Verkleidung für eine Struktur eines Flugzeugs
US8276847B2 (en) * 2004-04-16 2012-10-02 Airbus Operations Gmbh Cover for an aircraft structure
FR2872780B1 (fr) * 2004-07-08 2006-11-17 Airbus France Sas Plancher pour aeronef
US7325771B2 (en) 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US7503368B2 (en) * 2004-11-24 2009-03-17 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US7210655B2 (en) * 2004-12-03 2007-05-01 The Boeing Company Reconfigurable interior sidewall
DE102005038851A1 (de) * 2005-08-17 2007-03-01 Airbus Deutschland Gmbh Fachwerk-Mittelkasten für einen Flügel
GB2428417B (en) * 2005-10-27 2007-09-12 Hal Errikos Calamvokis Aircraft fuselage structure
US7766277B2 (en) * 2006-01-19 2010-08-03 The Boeing Company Deformable forward pressure bulkhead for an aircraft
DE102006026168A1 (de) 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026170B4 (de) * 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026169B4 (de) * 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
FR2906008B1 (fr) * 2006-09-15 2008-11-07 Airbus France Sa Eclisse de lisses et dispositif de jonction orbitale
DE102007003278B4 (de) * 2007-01-23 2013-10-31 Airbus Operations Gmbh Rumpfstrukturbauteil eines Luft- oder Raumfahrzeuges mit einer Schaumstoffschicht als thermische Isolierung
DE102007003275B4 (de) * 2007-01-23 2013-11-28 Airbus Operations Gmbh Schalenelement als Teil eines Flugzeugrumpfes
DE102007003277B4 (de) * 2007-01-23 2012-08-02 Airbus Operations Gmbh Rumpf eines Luft- oder Raumfahrzeuges in CFK-Metall Hybridbauweise mit einem Metallrahmen
DE102007019821B4 (de) 2007-04-26 2012-11-22 Airbus Operations Gmbh Strukturelement eines Flugzeugrumpfs
US8388795B2 (en) * 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
DE102007030026A1 (de) * 2007-06-29 2009-01-02 Airbus Deutschland Gmbh Strukturbauteil mit Spant- und Querträgerelement
US8042767B2 (en) * 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
ES2342866B1 (es) 2007-11-30 2011-05-18 Airbus España, S.L. Fuselaje de aeronave resistente a impactos.
US8038099B2 (en) * 2008-04-30 2011-10-18 The Boeing Company Bonded metal fuselage and method for making the same
US20100155533A1 (en) * 2008-12-23 2010-06-24 Spirit Aerosystems, Inc. Composite forward pressure bulkhead
FR2943311B1 (fr) * 2009-03-19 2011-03-04 Airbus France Raidisseurs sous bavette pour aeronef
DE102009015856B4 (de) 2009-04-01 2012-01-26 Airbus Operations Gmbh Rumpfsegment und Verfahren zur Herstellung des Rumpfsegments
ES2396328B1 (es) * 2010-06-30 2014-02-06 Airbus Operations, S.L. Fuselaje de aeronave en material compuesto y procedimientos para su fabricación.
EP2404824B1 (de) * 2010-07-08 2015-09-09 Airbus Opérations SAS Luftfahrzeugstruktur und Herstellungsverfahren für eine solche Struktur
GB201012552D0 (en) * 2010-07-23 2010-11-17 Bae Systems Plc Aircraft thermal insulation
DE102010038408B4 (de) 2010-07-26 2020-11-19 Airbus Operations Gmbh Strukturelement für ein Luft- und Raumfahrzeug und Verfahren zum Herstellen eines derartigen Strukturelementes
JP5535957B2 (ja) * 2011-02-21 2014-07-02 三菱航空機株式会社 翼パネルの形成方法
US8851422B2 (en) * 2012-08-28 2014-10-07 The Boeing Company Bonded composite aircraft wing
US8985512B1 (en) 2012-09-21 2015-03-24 The Boeing Company Aircraft, fuselages, and associated methods
EP2842865B1 (de) * 2013-08-28 2019-12-18 Airbus Operations GmbH Fensterscheibe für ein flugwerk und verfahren zur herstellung davon
GB2528080A (en) * 2014-07-08 2016-01-13 Airbus Operations Ltd Structure
WO2017064646A1 (en) * 2015-10-16 2017-04-20 Bombardier Inc. Stringer-less fuselage structure and method of manufacture
EP3281861B1 (de) 2016-08-11 2019-10-02 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Drehflügler mit einem rumpf mit mindestens einem strukturell versteiften paneel
DE102018207763A1 (de) 2018-05-17 2019-11-21 Airbus Operations Gmbh Rumpfstruktur für ein Luftfahrzeug
US11180238B2 (en) * 2018-11-19 2021-11-23 The Boeing Company Shear ties for aircraft wing
CN113601112B (zh) * 2021-07-27 2023-08-18 上海航天精密机械研究所 贮箱筒段超长壁板精密制造方法和系统

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US3146148A (en) * 1957-11-08 1964-08-25 Gen Dynamics Corp Apparatus for fabricating composite structures
US3020986A (en) * 1958-08-18 1962-02-13 Gen Dynamics Corp Composite structural panel
US2997262A (en) * 1960-01-21 1961-08-22 Gen Dynamics Corp Aircraft wing structure
US3135486A (en) * 1962-04-19 1964-06-02 Kirk Wing Company Airfoil construction and method for making the same
US3816952A (en) * 1969-02-19 1974-06-18 Ethyl Corp Preparation of metal foams with viscosity increasing gases
US4038118A (en) * 1974-06-14 1977-07-26 The Boeing Company Three dimensional composite structure and method for incorporating fittings
US4086378A (en) * 1975-02-20 1978-04-25 Mcdonnell Douglas Corporation Stiffened composite structural member and method of fabrication
US4032683A (en) * 1976-09-27 1977-06-28 Phillips Petroleum Company Structural member and method of making same
US4206895A (en) * 1978-03-30 1980-06-10 Olez Nejat A Loop-tension joint
US4416349A (en) * 1981-09-30 1983-11-22 The Boeing Company Viscoelastically damped reinforced skin structures
US4498325A (en) * 1982-09-29 1985-02-12 Walter Eckold Gmbh & Co. Kg Method for shaping panels by a bending operation, in particular panels for aircraft fuselage skin, and apparatus for implementing such method
US4674712A (en) * 1985-01-22 1987-06-23 The Boeing Company Double-lobe fuselage composite airplane
US4751979A (en) * 1985-05-16 1988-06-21 Airborne Express, Inc. Engine noise suppression kit for the nacelles of a jet aircraft
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
US5288538A (en) * 1992-12-16 1994-02-22 Reynolds Metals Company Expandable honeycomb core structural member
DE19529476C2 (de) * 1995-08-11 2000-08-10 Deutsch Zentr Luft & Raumfahrt Flügel mit schubsteifen Flügelschalen aus Faserverbundwerkstoffen für Luftfahrzeuge
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
US6085965A (en) * 1997-02-04 2000-07-11 Mcdonnel & Douglas Corporation Pressure bonding and densification process for manufacturing low density core metal parts
DE19715529C1 (de) * 1997-04-14 1998-08-06 Daimler Benz Aerospace Airbus Sandwichstruktur für Strukturbauteile eines Flugzeuges

Also Published As

Publication number Publication date
US20040155148A1 (en) 2004-08-12
SE0102083L (sv) 2002-12-08
DE60216454T2 (de) 2007-09-27
EP1399362B1 (de) 2006-11-29
SE519185C2 (sv) 2003-01-28
ES2276935T3 (es) 2007-07-01
SE0102083D0 (sv) 2001-06-07
ATE346789T1 (de) 2006-12-15
EP1399362A1 (de) 2004-03-24
WO2002098734A1 (en) 2002-12-12
US7025305B2 (en) 2006-04-11

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition