BRPI0810668A2 - Painel laminado de metal em fibra - Google Patents

Painel laminado de metal em fibra

Info

Publication number: BRPI0810668A2
Authority: BR; Brazil
Prior art keywords: metal panel; laminated fiber; fiber metal; laminated; panel
Prior art date: 2007-04-26

Application number

BRPI0810668-1A2A

Other languages

English (en)

Inventor

Valentin Popp

Thomas Beumler

Original Assignee

Airbus Operations Gmbh

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.)

2007-04-26

Filing date

2008-04-16

Publication date

2014-10-21

2008-04-16 Application filed by Airbus Operations Gmbh filed Critical Airbus Operations Gmbh

2014-10-21 Publication of BRPI0810668A2 publication Critical patent/BRPI0810668A2/pt

Links

239000000835 fiber Substances 0.000 title 1
239000002184 metal Substances 0.000 title 1

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
- 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
- B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
- 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
- B32B3/02—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 features of form at particular places, e.g. in edge regions
- B32B3/06—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 features of form at particular places, e.g. in edge regions for securing layers together; for attaching the product to another member, e.g. to a support, or to another product, e.g. groove/tongue, interlocking
- 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
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12375—All metal or with adjacent metals having member which crosses the plane of another member [e.g., T or X cross section, etc.]
- 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
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12444—Embodying fibers interengaged or between layers [e.g., paper, etc.]
- 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
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12486—Laterally noncoextensive components [e.g., embedded, etc.]

BRPI0810668-1A2A 2007-04-26 2008-04-16 Painel laminado de metal em fibra BRPI0810668A2 (pt)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
DE102007019716A DE102007019716A1 (de)	2007-04-26	2007-04-26	Faser-Metall-Laminat-Panel
PCT/EP2008/054581 WO2008132050A1 (en)	2007-04-26	2008-04-16	Fibre metal laminate panel

Publications (1)

Publication Number	Publication Date
BRPI0810668A2 true BRPI0810668A2 (pt)	2014-10-21

Family

ID=39714171

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BRPI0810668-1A2A BRPI0810668A2 (pt)	2007-04-26	2008-04-16	Painel laminado de metal em fibra

Country Status (9)

Country	Link
US (1)	US8101284B2 (pt)
EP (1)	EP2139759B1 (pt)
JP (1)	JP2010524767A (pt)
CN (1)	CN101711212B (pt)
BR (1)	BRPI0810668A2 (pt)
CA (1)	CA2680369A1 (pt)
DE (1)	DE102007019716A1 (pt)
RU (1)	RU2009134152A (pt)
WO (1)	WO2008132050A1 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
NL2000232C2 (nl) *	2006-09-12	2008-03-13	Gtm Consulting B V	Huidpaneel voor een vliegtuigromp.
DE102007019716A1 (de)	2007-04-26	2008-10-30	Airbus Deutschland Gmbh	Faser-Metall-Laminat-Panel
DE102010048365B4 (de) *	2010-10-13	2012-08-23	Airbus Operations Gmbh	Flächengebilde und Flugzeugrumpf mit einem derartigen Flächengebilde
US8790777B2 (en) *	2012-04-19	2014-07-29	The Boeing Company	Composite articles having fibers with longitudinally-varying geometry
EP2907654B1 (en)	2014-02-13	2024-06-26	Airbus Operations GmbH	Joints in fibre metal laminates
GB2545494A (en) *	2015-12-18	2017-06-21	Airbus Operations Ltd	A structure formed from composite material
GB2545655A (en) *	2015-12-18	2017-06-28	Airbus Operations Ltd	A structure formed from composite material
DE102017201834A1 (de) *	2017-02-06	2018-08-09	Thyssenkrupp Ag	Halbzeug mit unterschiedlichen Eigenschaften
JP7377722B2 (ja) *	2020-01-10	2023-11-10	三菱重工業株式会社	接合構造体及び接合構造体の製造方法
GB2605430A (en) *	2021-03-31	2022-10-05	Airbus Operations Ltd	Load-bearing structures

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US4310132A (en) *	1978-02-16	1982-01-12	Nasa	Fuselage structure using advanced technology fiber reinforced composites
JP2769390B2 (ja) *	1990-11-23	1998-06-25	アクロ − ファイアガードプロダクツ，インコーポレイテッド	補修用耐火パッチおよびこれを使った補修方法
US5429326A (en)	1992-07-09	1995-07-04	Structural Laminates Company	Spliced laminate for aircraft fuselage
US5567535A (en) *	1992-11-18	1996-10-22	Mcdonnell Douglas Corporation	Fiber/metal laminate splice
US5866272A (en) *	1996-01-11	1999-02-02	The Boeing Company	Titanium-polymer hybrid laminates
US6736919B1 (en) *	1997-05-28	2004-05-18	Structural Laminates Company	Method for making a laminate and laminate obtainable by said method
NL1015141C2 (nl) *	2000-05-09	2001-11-13	Fokker Aerostructures Bv	Verbindingsconstructie in een laminaat uit metalen en kunststof lagen.
DE10031510A1 (de) *	2000-06-28	2002-01-17	Airbus Gmbh	Strukturbauteil für ein Flugzeug
NL1018120C2 (nl)	2001-05-21	2002-12-03	Fokker Aerostructures Bv	Werkwijze voor het vervaardigen van een gevormd laminaat.
EP1336469A1 (en) *	2002-02-19	2003-08-20	Alenia Aeronautica S.P.A.	Methods of manufacturing a stiffening element for an aircraft skin panel and a skin panel provided with the stiffening element
NL1023854C2 (nl) *	2003-07-08	2005-01-11	Stork Fokker Aesp Bv	Laminaat met vullaag.
NL1024479C2 (nl) *	2003-10-07	2005-04-08	Stork Fokker Aesp Bv	Verbindingsconstructie in een laminaat met een plaatselijke versterking.
JP3709485B1 (ja) *	2004-10-08	2005-10-26	株式会社昭和	ライニング構造
US7686905B2 (en) *	2005-09-06	2010-03-30	The Boeing Company	Copper grid repair technique for lightning strike protection
DE102006031436B4 (de) *	2006-07-07	2012-12-06	Airbus Operations Gmbh	Strukturelement, Verfahren zur Herstellung eines derartigen Strukturelements und Flugzeug mit einem derartigen Strukturelement
US7687129B2 (en) *	2007-01-08	2010-03-30	Lockheed Martin Corporation	Splice seam
DE102007019716A1 (de)	2007-04-26	2008-10-30	Airbus Deutschland Gmbh	Faser-Metall-Laminat-Panel

2007
- 2007-04-26 DE DE102007019716A patent/DE102007019716A1/de not_active Ceased
2008
- 2008-04-16 CA CA002680369A patent/CA2680369A1/en not_active Abandoned
- 2008-04-16 JP JP2010504625A patent/JP2010524767A/ja active Pending
- 2008-04-16 RU RU2009134152/11A patent/RU2009134152A/ru not_active Application Discontinuation
- 2008-04-16 BR BRPI0810668-1A2A patent/BRPI0810668A2/pt not_active IP Right Cessation
- 2008-04-16 CN CN200880013511.XA patent/CN101711212B/zh active Active
- 2008-04-16 WO PCT/EP2008/054581 patent/WO2008132050A1/en not_active Ceased
- 2008-04-16 EP EP08736261.2A patent/EP2139759B1/en active Active
2009
- 2009-10-06 US US12/574,141 patent/US8101284B2/en active Active

Also Published As

Publication number	Publication date
WO2008132050A1 (en)	2008-11-06
CN101711212A (zh)	2010-05-19
US8101284B2 (en)	2012-01-24
EP2139759A1 (en)	2010-01-06
JP2010524767A (ja)	2010-07-22
DE102007019716A1 (de)	2008-10-30
EP2139759B1 (en)	2016-10-26
CA2680369A1 (en)	2008-11-06
US20100086804A1 (en)	2010-04-08
CN101711212B (zh)	2016-07-13
RU2009134152A (ru)	2011-03-20

Legal Events

Date	Code	Title	Description
2015-08-25	B08F	Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]	Free format text: REFERENTE AS 6A E 7A ANUIDADES.
2016-05-10	B08K	Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]	Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2329 DE 25-08-2015 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.
2022-07-12	B350	Update of information on the portal [chapter 15.35 patent gazette]

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FI20086002A0 (fi)	2008-10-23	Paneeli
FR2922250B1 (fr)	2011-09-02	Volet battant isolant
FR2936181B1 (fr)	2012-09-07	Panneau sandwich composite renforce
ATE482319T1 (de)	2010-10-15	Akustik-mehrschichtplatte
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