BRPI0402617A - Estrutura de construção leve - Google Patents
Estrutura de construção leveInfo
- Publication number
- BRPI0402617A BRPI0402617A BRPI0402617A BRPI0402617A BR PI0402617 A BRPI0402617 A BR PI0402617A BR PI0402617 A BRPI0402617 A BR PI0402617A BR PI0402617 A BRPI0402617 A BR PI0402617A
- Authority
- BR
- Brazil
- Prior art keywords
- consist
- outer shell
- elements
- structural elements
- lightweight structure
- Prior art date
Links
- 239000000463 material Substances 0.000 abstract 2
- 229910000838 Al alloy Inorganic materials 0.000 abstract 1
- JFBZPFYRPYOZCQ-UHFFFAOYSA-N [Li].[Al] Chemical compound [Li].[Al] JFBZPFYRPYOZCQ-UHFFFAOYSA-N 0.000 abstract 1
- 238000004026 adhesive bonding Methods 0.000 abstract 1
- 230000003014 reinforcing effect Effects 0.000 abstract 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
- B32B15/092—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 comprising epoxy resins
-
- 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
- B32B3/08—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 characterised by added members at particular parts
-
- 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
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/38—Layered products comprising a layer of synthetic resin comprising epoxy resins
-
- 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
- B32B3/14—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 face layer formed of separate pieces of material which are juxtaposed side-by-side
-
- 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—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
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/08—Reinforcements
-
- 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
- B32B2311/18—Titanium
-
- 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
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
Landscapes
- Laminated Bodies (AREA)
Abstract
"ESTRUTURA DE CONSTRUçãO LEVE". A presente invenção refere-se a uma estrutura de construção leve que consiste em um revestimento externo assim como em elementos estruturais unidos a esse, sendo que são colocados sobre o revestimento externo, sempre entre os elementos estruturais, por colagem, elementos adicionais em forma de tiras de uma estrutura de reforço os quais consistem em material com tolerância ao dano e os quais formam uma estrutura em treliça. Os elementos adicionais podem consistir em um material composto de uma liga monolítica de alumínio e lítio.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10330709 | 2003-07-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0402617A true BRPI0402617A (pt) | 2005-05-17 |
Family
ID=33441650
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0402617 BRPI0402617A (pt) | 2003-07-08 | 2004-07-06 | Estrutura de construção leve |
Country Status (5)
Country | Link |
---|---|
US (1) | US7285326B2 (pt) |
EP (1) | EP1495858B1 (pt) |
BR (1) | BRPI0402617A (pt) |
CA (1) | CA2473346C (pt) |
RU (1) | RU2354557C2 (pt) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10238460B3 (de) * | 2002-08-22 | 2004-03-11 | Airbus Deutschland Gmbh | Leichtbaustruktur aus dünnen Metallblechlagen |
EP1495859B1 (de) * | 2003-07-08 | 2008-09-03 | Airbus Deutschland GmbH | Leichtbaustruktur |
DE10360808B4 (de) * | 2003-12-19 | 2005-10-27 | Airbus Deutschland Gmbh | Faserverstärkter metallischer Verbundwerkstoff |
NL1030029C2 (nl) * | 2005-09-26 | 2007-03-27 | Gtm Consulting B V | Werkwijze en inrichting voor het verlijmen van componenten tot een samengesteld vormdeel. |
NL1030066C2 (nl) * | 2005-09-29 | 2007-03-30 | Gtm Consulting B V | Werkwijze voor het vervaardigen van een vormdeel uit een samengesteld materiaal. |
DE102005060958A1 (de) * | 2005-12-20 | 2007-06-21 | Airbus Deutschland Gmbh | Schutzvorrichtung |
DE102006003160A1 (de) * | 2006-01-24 | 2007-09-06 | Airbus Deutschland Gmbh | Flächendichtung sowie Verfahren zur Herstellung von abgedichteten Fügeverbindungen mit der Flächendichtung |
DE102006007428A1 (de) | 2006-02-17 | 2007-08-30 | Airbus Deutschland Gmbh | Verstärkungsmaterial zur lokalen Verstärkung eines mit einem Verbundmaterial gebildeten Bauteils sowie Verfahren |
WO2008054876A2 (en) * | 2006-05-15 | 2008-05-08 | Alcoa Inc. | Reinforced hybrid structures and methods thereof |
NL2000100C2 (nl) * | 2006-06-13 | 2007-12-14 | Gtm Consulting B V | Laminaat uit metaalplaten en kunststof. |
NL2000232C2 (nl) * | 2006-09-12 | 2008-03-13 | Gtm Consulting B V | Huidpaneel voor een vliegtuigromp. |
US20090211697A1 (en) * | 2007-05-15 | 2009-08-27 | Heinimann Markus B | Reinforced hybrid structures and methods thereof |
US20090188748A1 (en) * | 2008-01-24 | 2009-07-30 | Honeywell International Inc. | Noise suppression panels and repair methods therefor |
DE102008042782A1 (de) * | 2008-10-13 | 2010-04-29 | Airbus Deutschland Gmbh | Strukturelement zur Verstärkung einer Rumpfzelle eines Flugzeugs |
US8776375B2 (en) * | 2011-05-19 | 2014-07-15 | The Boeing Company | Aircraft structure for high capacity pull off |
GB201116287D0 (en) * | 2011-09-21 | 2011-11-02 | Airbus Operations Ltd | Method and device for removing a sleeve from a bore |
FR2983772B1 (fr) * | 2011-12-13 | 2014-01-10 | Airbus Operations Sas | Paroi en materiau composite renforcee de maniere a limiter la propagation d'une crique selon une direction |
CN103388113B (zh) * | 2013-07-25 | 2015-06-10 | 辽宁工程技术大学 | 一种玄武岩纤维增强镁合金复合材料及其制备方法 |
JP5959558B2 (ja) * | 2014-03-13 | 2016-08-02 | アイシン高丘株式会社 | 複合構造体及びその製造方法 |
CN105842067B (zh) * | 2015-01-15 | 2019-11-08 | 中国石油天然气股份有限公司 | 应力变化与裂缝扩展方向测试装置及方法 |
CN106182912A (zh) * | 2016-06-24 | 2016-12-07 | 廖兴池 | 一种低密度复合型保温金属材料 |
GB2582148A (en) * | 2019-03-12 | 2020-09-16 | Airbus Operations Ltd | Impact resistant panels |
CN111114821B (zh) * | 2019-12-24 | 2024-01-12 | 中国特种飞行器研究所 | 一种先进增强结构的结构处理方法 |
US11549391B2 (en) | 2021-03-22 | 2023-01-10 | General Electric Company | Component formed from hybrid material |
US12055054B2 (en) | 2021-04-19 | 2024-08-06 | General Electric Company | Light weight fan casing configurations for energy absorption |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3058704A (en) * | 1958-01-16 | 1962-10-16 | Johnson & Johnson | Laminated adhesive sheeting for aircraft |
US3401025A (en) * | 1965-05-03 | 1968-09-10 | Boeing Co | Bonded article comprising two metallic members joined by an intermediate layer |
US4052523A (en) * | 1976-09-14 | 1977-10-04 | The United States Of America As Represented By The National Aeronautics And Space Administration | Composite sandwich lattice structure |
NL8100087A (nl) * | 1981-01-09 | 1982-08-02 | Tech Hogeschool Delft Afdeling | Laminaat uit metalen platen en daarmede verbonden draden. |
US4411380A (en) * | 1981-06-30 | 1983-10-25 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Metal matrix composite structural panel construction |
JPS6199655A (ja) * | 1984-10-18 | 1986-05-17 | Toyota Motor Corp | 鉱物繊維強化金属複合材料 |
US5151311A (en) * | 1987-11-02 | 1992-09-29 | Grumman Aerospace Corporation | Acoustic attenuating liner and method of making same |
US5106668A (en) * | 1989-06-07 | 1992-04-21 | Hexcel Corporation | Multi-layer honeycomb structure |
US6086975A (en) | 1991-01-16 | 2000-07-11 | The Boeing Company | Lighting protection for electrically conductive or insulating skin and core for honeycomb structure |
GB9101354D0 (en) | 1991-01-22 | 1991-03-06 | Short Brothers Plc | Noise attentuation panel |
GB2253185A (en) * | 1991-03-01 | 1992-09-02 | Secr Defence | Reinforced alloy laminates |
US5352529A (en) * | 1991-05-13 | 1994-10-04 | Auto-Air Composites, Inc. | Lightweight thrust vectoring panel |
US5429326A (en) * | 1992-07-09 | 1995-07-04 | Structural Laminates Company | Spliced laminate for aircraft fuselage |
FR2719553B1 (fr) * | 1994-05-04 | 1996-07-26 | Eurocopter France | Dispositif anti-couple à rotor arrière et stator redresseur carénés pour hélicoptère. |
US5667866A (en) * | 1995-05-02 | 1997-09-16 | The Nordam Group, Inc. | Multi-layered, unbalanced sandwich panel |
US5895699A (en) * | 1996-03-15 | 1999-04-20 | The Boeing Company | Tiedown ply for reducing core crush in composite honeycomb sandwich structure |
WO1997025198A1 (en) | 1996-01-11 | 1997-07-17 | The Boeing Company | Composite honeycomb sandwich structure |
US5866272A (en) * | 1996-01-11 | 1999-02-02 | The Boeing Company | Titanium-polymer hybrid laminates |
US5902756A (en) * | 1996-07-25 | 1999-05-11 | Northrop Grumman Corporation | Ceramic matrix composites with integrated topcoat layers |
US5804278A (en) * | 1997-01-03 | 1998-09-08 | Fixtures Manufacturing Corporation | Laminated panel construction with honeycomb grid core |
AU8435298A (en) * | 1997-05-28 | 1998-12-30 | Akzo Nobel N.V. | Method for making a laminate and laminate obtainable by said method |
KR100217487B1 (ko) * | 1997-06-03 | 1999-09-01 | 맹섭 | 골프채의 헤드커버 |
DE10238460B3 (de) * | 2002-08-22 | 2004-03-11 | Airbus Deutschland Gmbh | Leichtbaustruktur aus dünnen Metallblechlagen |
EP1495859B1 (de) * | 2003-07-08 | 2008-09-03 | Airbus Deutschland GmbH | Leichtbaustruktur |
-
2004
- 2004-06-30 EP EP04015293.6A patent/EP1495858B1/de not_active Expired - Lifetime
- 2004-07-06 BR BRPI0402617 patent/BRPI0402617A/pt active Search and Examination
- 2004-07-07 RU RU2004120842A patent/RU2354557C2/ru not_active IP Right Cessation
- 2004-07-08 CA CA 2473346 patent/CA2473346C/en not_active Expired - Fee Related
- 2004-07-08 US US10/888,566 patent/US7285326B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP1495858A1 (de) | 2005-01-12 |
RU2354557C2 (ru) | 2009-05-10 |
RU2004120842A (ru) | 2006-01-10 |
US7285326B2 (en) | 2007-10-23 |
CA2473346C (en) | 2011-05-10 |
US20050112348A1 (en) | 2005-05-26 |
EP1495858B1 (de) | 2019-08-07 |
CA2473346A1 (en) | 2005-01-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B03H | Publication of an application: rectification [chapter 3.8 patent gazette] | ||
B25D | Requested change of name of applicant approved |
Owner name: AIRBUS OPERATIONS GMBH (DE) Free format text: NOME ALTERADO DE: AIRBUS DEUTSCHLAND GMBH |
|
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B11D | Dismissal acc. art. 38, par 2 of ipl - failure to pay fee after grant in time |