BRPI0716761A2 - painel de revestimento para uma fuselagem de aeronave - Google Patents
painel de revestimento para uma fuselagem de aeronaveInfo
- Publication number
- BRPI0716761A2 BRPI0716761A2 BRPI0716761-0A2A BRPI0716761A BRPI0716761A2 BR PI0716761 A2 BRPI0716761 A2 BR PI0716761A2 BR PI0716761 A BRPI0716761 A BR PI0716761A BR PI0716761 A2 BRPI0716761 A2 BR PI0716761A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft fuselage
- cladding panel
- cladding
- panel
- fuselage
- Prior art date
Links
- 238000005253 cladding Methods 0.000 title 1
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
-
- 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.]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NL2000232A NL2000232C2 (nl) | 2006-09-12 | 2006-09-12 | Huidpaneel voor een vliegtuigromp. |
| PCT/NL2007/050418 WO2008033017A1 (en) | 2006-09-12 | 2007-08-24 | Skin panel for an aircraft fuselage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BRPI0716761A2 true BRPI0716761A2 (pt) | 2013-09-17 |
Family
ID=37891731
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0716761-0A2A BRPI0716761A2 (pt) | 2006-09-12 | 2007-08-24 | painel de revestimento para uma fuselagem de aeronave |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US20100133380A1 (pt) |
| EP (1) | EP2061697A1 (pt) |
| CN (1) | CN101522518A (pt) |
| BR (1) | BRPI0716761A2 (pt) |
| NL (1) | NL2000232C2 (pt) |
| WO (1) | WO2008033017A1 (pt) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12410728B2 (en) | 2021-03-24 | 2025-09-09 | General Electric Company | Hybrid composite components |
Families Citing this family (43)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7837147B2 (en) * | 2005-03-18 | 2010-11-23 | The Boeing Company | Systems and methods for reducing noise in aircraft fuselages and other structures |
| DE102006026169B4 (de) * | 2006-06-06 | 2012-06-21 | Airbus Operations Gmbh | Flugzeugrumpfstruktur und Verfahren zu deren Herstellung |
| 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 |
| NL2000100C2 (nl) | 2006-06-13 | 2007-12-14 | Gtm Consulting B V | Laminaat uit metaalplaten en kunststof. |
| DE102006051989B4 (de) * | 2006-11-03 | 2010-09-30 | Airbus Deutschland Gmbh | Versteifte Beplankung für ein Luft- oder Raumfahrzeug mit einem Laminat-Stringer hoher Steifigkeit |
| US9511571B2 (en) | 2007-01-23 | 2016-12-06 | The Boeing Company | Composite laminate having a damping interlayer and method of making the same |
| ES2352941B1 (es) * | 2008-05-16 | 2012-01-25 | Airbus Operations, S.L. | Estructura integrada de aeronave en material compuesto |
| DE102008042782A1 (de) * | 2008-10-13 | 2010-04-29 | Airbus Deutschland Gmbh | Strukturelement zur Verstärkung einer Rumpfzelle eines Flugzeugs |
| NL2002289C2 (en) * | 2008-12-04 | 2010-06-07 | Gtm Holding B V | Sandwich panel, support member for use in a sandwich panel and aircraft provided with such a sandwich panel. |
| DE102009009491A1 (de) * | 2009-02-18 | 2010-09-09 | Airbus Deutschland Gmbh | Verfahren zum Herstellen eines Schalenkörpers |
| US8425710B2 (en) | 2009-03-13 | 2013-04-23 | The Boeing Company | Automated placement of vibration damping materials |
| JP5592672B2 (ja) * | 2009-03-27 | 2014-09-17 | ホンダ・パテンツ・アンド・テクノロジーズ・ノース・アメリカ・エルエルシー | 航空機用スキッドレール及びその製造方法 |
| ES2382765B1 (es) * | 2009-06-29 | 2013-05-03 | Airbus Operations, S.L. | Diseño de cuadernas de aeronave |
| PT2646242E (pt) * | 2010-11-29 | 2015-09-03 | Gtm Advanced Structures B V | Laminado compósito reforçado com fibra e folha de metal |
| JP5808111B2 (ja) * | 2011-02-04 | 2015-11-10 | 三菱重工業株式会社 | 航空機用複合材構造体、これを備えた航空機主翼および航空機胴体 |
| US9016042B2 (en) | 2011-05-20 | 2015-04-28 | Rohr, Inc. | Reinforcement members for aircraft propulsion system components configured to address delamination of the inner fixed structure |
| JP5972376B2 (ja) * | 2011-08-17 | 2016-08-17 | ビー イー エアロスペイス,インク. | 埋込みインサートを備えた高強度航空機インテリアパネル |
| 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 |
| US8790777B2 (en) * | 2012-04-19 | 2014-07-29 | The Boeing Company | Composite articles having fibers with longitudinally-varying geometry |
| US9120276B2 (en) * | 2012-07-25 | 2015-09-01 | The Boeing Company | Laminated composite bending and stiffening members with reinforcement by inter-laminar metal sheets |
| CN102963075A (zh) * | 2012-11-28 | 2013-03-13 | 常熟市东涛金属复合材料有限公司 | 一种耐热复合金属材料 |
| FR3000018B1 (fr) * | 2012-12-21 | 2016-12-09 | Airbus Operations Sas | Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur |
| FR3001199B1 (fr) * | 2013-01-23 | 2016-07-15 | Snecma | Capot de moteur incorporant un circuit de ventilation d'equipement |
| US9253823B2 (en) | 2013-02-10 | 2016-02-02 | The Boeing Company | Metal matrix composite used as a heating element |
| CN104210176A (zh) * | 2013-05-31 | 2014-12-17 | 周奇迪 | 防爆车辆用防爆板及防爆车辆 |
| NL2012889B1 (en) * | 2014-05-26 | 2016-05-03 | Gtm Advanced Products B V | Laminate of a metal sheet and an adhesive layer bonded thereto. |
| EP2962840A1 (en) * | 2014-06-30 | 2016-01-06 | Airbus Operations, S.L. | A leading edge for an aircraft lifting surface and manufacturing method thereof |
| CN105419325A (zh) * | 2014-08-21 | 2016-03-23 | 黑龙江鑫达企业集团有限公司 | 一种高强度、耐高温聚酰亚胺复合材料的制备 |
| CN104191731B (zh) * | 2014-09-06 | 2017-12-15 | 宁波甬凌新材料科技有限公司 | 一种高硬度耐热复合金属材料及其成型方法 |
| US9919791B2 (en) * | 2015-04-15 | 2018-03-20 | Gulfstream Aerospace Corporation | Stiffening structures, wing structures, and methods for manufacturing stiffening structures |
| US10053203B2 (en) * | 2015-10-13 | 2018-08-21 | The Boeing Company | Composite stiffener with integral conductive element |
| EP3178638A1 (de) * | 2015-12-11 | 2017-06-14 | Voestalpine Stahl GmbH | Verfahren zur herstellung eines halbzeugs oder bauteils aus metall und faserverbund |
| GB2545655A (en) * | 2015-12-18 | 2017-06-28 | Airbus Operations Ltd | A structure formed from composite material |
| EP3228539B1 (en) * | 2016-04-06 | 2020-03-04 | Safran Landing Systems UK Limited | Aircraft landing gear assembly |
| US10220935B2 (en) * | 2016-09-13 | 2019-03-05 | The Boeing Company | Open-channel stiffener |
| GB2581951B (en) * | 2019-01-17 | 2022-11-30 | Rayne Damian | An aircraft |
| US11155056B2 (en) * | 2019-04-08 | 2021-10-26 | The Boeing Company | Methods of making laminated metallic structures |
| US20220234308A1 (en) * | 2019-06-21 | 2022-07-28 | Sabic Global Technologies B.V. | Fiber reinforced profiled object |
| CN111347736B (zh) * | 2020-03-13 | 2022-01-18 | 西安泰利达新材料科技有限公司 | 一种具有夹层芯材的复合金属结构及其制备方法 |
| US11985781B2 (en) * | 2020-09-23 | 2024-05-14 | Apple Inc. | Surface treatment for metallic components |
| US20250320884A1 (en) * | 2024-04-10 | 2025-10-16 | Textron Aviation, Inc. | Method for forming a reinforced aluminum component and reinforced aluminum component |
| CN119304519B (zh) * | 2024-10-09 | 2025-11-18 | 陕西飞机工业有限责任公司 | 一种多特征垫板的数控加工方法 |
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|---|---|---|---|---|
| US2466735A (en) * | 1946-10-23 | 1949-04-12 | Shellmar Products Corp | Heat-sealing device |
| US3580795A (en) * | 1966-10-05 | 1971-05-25 | John E Eichenlaub | Apparatus for welding heat sealable sheet material |
| GB1539180A (en) * | 1974-12-09 | 1979-01-31 | Lilly Industries Ltd | 1-cyclopentene-1-propanoic acid derivatives |
| US4197360A (en) * | 1978-05-01 | 1980-04-08 | The United States Of America As Represented By The Secretary Of The Army | Multilayer laminate of improved resistance to fatigue cracking |
| WO1980002254A1 (en) * | 1979-04-16 | 1980-10-30 | H Forsch | Stitch bond fastening of composite structures |
| NL8100088A (nl) * | 1981-01-09 | 1982-08-02 | Tech Hogeschool Delft Afdeling | Laminaat uit metalen platen en daarmede verbonden draden, alsmede werkwijzen ter vervaardiging daarvan. |
| NL8100087A (nl) * | 1981-01-09 | 1982-08-02 | Tech Hogeschool Delft Afdeling | Laminaat uit metalen platen en daarmede verbonden draden. |
| DE3148198A1 (de) * | 1981-12-05 | 1983-06-09 | Brown, Boveri & Cie Ag, 6800 Mannheim | "hochtemperaturschutzschicht" |
| US4502092A (en) * | 1982-09-30 | 1985-02-26 | The Boeing Company | Integral lightning protection system for composite aircraft skins |
| US4543140A (en) * | 1984-07-09 | 1985-09-24 | Price John G | Steam sack vulcanizing method |
| US4792374B1 (en) * | 1987-04-03 | 1995-02-14 | Fischer Ag Georg | Apparatus for fusion joining plastic pipe |
| DE3876371T2 (de) * | 1987-10-14 | 1993-05-13 | Structural Laminates Co | Schichtstoff aus metallschichten und aus durchgehendem,faserverstaerkten,synthetischen,thermoplastischen material und verfahren zu seiner herstellung. |
| ATE61970T1 (de) * | 1987-10-14 | 1991-04-15 | Akzo Nv | Schichtstoff aus metallschichten und aus durchgehendem faserverstaerktem synthetischem material. |
| EP0322947B1 (en) * | 1987-12-31 | 1992-07-15 | Structural Laminates Company | Composite laminate of metal sheets and continuous filaments-reinforced synthetic layers |
| GB2237239B (en) * | 1989-10-27 | 1993-09-01 | Reifenhaeuser Masch | A process for the production of a ribbon of synthetic thermoplastic material in sheet form |
| US5160771A (en) * | 1990-09-27 | 1992-11-03 | Structural Laminates Company | Joining metal-polymer-metal laminate sections |
| US5284996A (en) * | 1992-02-28 | 1994-02-08 | Mcdonnell Douglas Corporation | Waste gas storage |
| US5429326A (en) * | 1992-07-09 | 1995-07-04 | Structural Laminates Company | Spliced laminate for aircraft fuselage |
| US5429879A (en) * | 1993-06-18 | 1995-07-04 | The United States Of America As Represented By The United States Department Of Energy | Laminated metal composite formed from low flow stress layers and high flow stress layers using flow constraining elements and making same |
| US5547735A (en) * | 1994-10-26 | 1996-08-20 | Structural Laminates Company | Impact resistant laminate |
| US5814175A (en) * | 1995-06-07 | 1998-09-29 | Edlon Inc. | Welded thermoplastic polymer article and a method and apparatus for making same |
| 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 |
| DE10015614B4 (de) * | 2000-03-29 | 2009-02-19 | Ceramtec Ag | Gesinterter Formkörper mit poröser Schicht auf der Oberfläche sowie Verfahren zu seiner Herstellung und seine Verwendungen |
| JP4526698B2 (ja) * | 2000-12-22 | 2010-08-18 | 富士重工業株式会社 | 複合材成形品及びその製造方法 |
| US6648273B2 (en) * | 2001-10-30 | 2003-11-18 | The Boeing Company | Light weight and high strength fuselage |
| 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 |
| US7192501B2 (en) * | 2002-10-29 | 2007-03-20 | The Boeing Company | Method for improving crack resistance in fiber-metal-laminate structures |
| EP1495858B1 (de) * | 2003-07-08 | 2019-08-07 | Airbus Operations GmbH | Leichtbaustruktur aus metallischen schichtwerkstoffen |
| NL1024076C2 (nl) * | 2003-08-08 | 2005-02-10 | Stork Fokker Aesp Bv | Werkwijze voor het vormen van een laminaat met een uitsparing. |
| US7325771B2 (en) * | 2004-09-23 | 2008-02-05 | The Boeing Company | Splice joints for composite aircraft fuselages and other structures |
| 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. |
| US20070175583A1 (en) * | 2006-01-31 | 2007-08-02 | Mosallam Ayman S | Technique for prestressing composite members and related apparatuses |
| DE102007019716A1 (de) * | 2007-04-26 | 2008-10-30 | Airbus Deutschland Gmbh | Faser-Metall-Laminat-Panel |
| US20090211697A1 (en) * | 2007-05-15 | 2009-08-27 | Heinimann Markus B | Reinforced hybrid structures and methods thereof |
-
2006
- 2006-09-12 NL NL2000232A patent/NL2000232C2/nl not_active IP Right Cessation
-
2007
- 2007-08-24 CN CN200780038347.3A patent/CN101522518A/zh active Pending
- 2007-08-24 EP EP07808551A patent/EP2061697A1/en not_active Withdrawn
- 2007-08-24 WO PCT/NL2007/050418 patent/WO2008033017A1/en not_active Ceased
- 2007-08-24 US US12/440,574 patent/US20100133380A1/en not_active Abandoned
- 2007-08-24 BR BRPI0716761-0A2A patent/BRPI0716761A2/pt not_active Application Discontinuation
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12410728B2 (en) | 2021-03-24 | 2025-09-09 | General Electric Company | Hybrid composite components |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101522518A (zh) | 2009-09-02 |
| WO2008033017A1 (en) | 2008-03-20 |
| US20100133380A1 (en) | 2010-06-03 |
| EP2061697A1 (en) | 2009-05-27 |
| NL2000232C2 (nl) | 2008-03-13 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B11A | Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing | ||
| B11Y | Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette] |