BRPI0620070A2 - união e método para a produção de uma união para uso na construção de aeronaves - Google Patents
união e método para a produção de uma união para uso na construção de aeronaves Download PDFInfo
- Publication number
- BRPI0620070A2 BRPI0620070A2 BRPI0620070-2A BRPI0620070A BRPI0620070A2 BR PI0620070 A2 BRPI0620070 A2 BR PI0620070A2 BR PI0620070 A BRPI0620070 A BR PI0620070A BR PI0620070 A2 BRPI0620070 A2 BR PI0620070A2
- Authority
- BR
- Brazil
- Prior art keywords
- butt joint
- joint
- liner
- distal
- wing
- Prior art date
Links
- 238000010276 construction Methods 0.000 title claims abstract description 10
- 238000004519 manufacturing process Methods 0.000 title description 3
- 230000000295 complement effect Effects 0.000 claims abstract description 10
- 210000001503 joint Anatomy 0.000 claims description 109
- 238000000034 method Methods 0.000 claims description 12
- 238000000465 moulding Methods 0.000 claims description 12
- 239000011248 coating agent Substances 0.000 claims description 8
- 238000000576 coating method Methods 0.000 claims description 8
- 239000002131 composite material Substances 0.000 claims description 7
- 239000000945 filler Substances 0.000 claims description 7
- 238000003754 machining Methods 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 4
- 239000003381 stabilizer Substances 0.000 claims description 4
- 230000001419 dependent effect Effects 0.000 claims description 2
- 230000008878 coupling Effects 0.000 claims 2
- 238000010168 coupling process Methods 0.000 claims 2
- 238000005859 coupling reaction Methods 0.000 claims 2
- 229910000831 Steel Inorganic materials 0.000 claims 1
- 239000007769 metal material Substances 0.000 claims 1
- 239000010959 steel Substances 0.000 claims 1
- 230000003628 erosive effect Effects 0.000 description 5
- 238000005304 joining Methods 0.000 description 4
- 241000251730 Chondrichthyes Species 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 229910000906 Bronze Inorganic materials 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 239000011324 bead Substances 0.000 description 2
- 239000010974 bronze Substances 0.000 description 2
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 230000000717 retained effect Effects 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 239000011800 void material Substances 0.000 description 2
- 238000005253 cladding Methods 0.000 description 1
- 230000032798 delamination Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 238000011417 postcuring Methods 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 230000011514 reflex Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000004584 weight gain Effects 0.000 description 1
- 235000019786 weight gain Nutrition 0.000 description 1
- 230000037303 wrinkles Effects 0.000 description 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
- Joining Of Building Structures In Genera (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Adhesives Or Adhesive Processes (AREA)
- Road Paving Structures (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB0525896.7A GB0525896D0 (en) | 2005-12-20 | 2005-12-20 | A joint for use in aircraft construction |
| GB0525896.7 | 2005-12-20 | ||
| PCT/GB2006/004439 WO2007071905A1 (en) | 2005-12-20 | 2006-11-28 | A joint for use in aircraft construction |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BRPI0620070A2 true BRPI0620070A2 (pt) | 2011-11-01 |
Family
ID=35840772
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0620070-2A BRPI0620070A2 (pt) | 2005-12-20 | 2006-11-28 | união e método para a produção de uma união para uso na construção de aeronaves |
Country Status (11)
| Country | Link |
|---|---|
| US (2) | USRE47738E1 (enExample) |
| EP (1) | EP1963178B1 (enExample) |
| JP (1) | JP2009519861A (enExample) |
| CN (1) | CN101341070A (enExample) |
| AT (1) | ATE476359T1 (enExample) |
| BR (1) | BRPI0620070A2 (enExample) |
| CA (1) | CA2633106C (enExample) |
| DE (1) | DE602006016006D1 (enExample) |
| GB (1) | GB0525896D0 (enExample) |
| RU (1) | RU2427500C2 (enExample) |
| WO (1) | WO2007071905A1 (enExample) |
Families Citing this family (65)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0609166D0 (en) * | 2006-05-09 | 2006-06-21 | Airbus Uk Ltd | Apparatus for and method of inhibiting delamination |
| JP4657194B2 (ja) * | 2006-11-20 | 2011-03-23 | 本田技研工業株式会社 | 前縁スキンの段差調整構造および前縁スキンの組付方法 |
| FR2916424B1 (fr) * | 2007-05-23 | 2009-08-21 | Airbus France Sa | Mat d'accrochage de moteur pour aeronef comprenant une cale biaise pour la fixation de l'attache moteur avant |
| RU2476348C2 (ru) * | 2007-05-31 | 2013-02-27 | Эйрбас Оператионс Гмбх | Способ производства составной обшивки в области авиационной и космической промышленности |
| US8398027B2 (en) * | 2007-09-17 | 2013-03-19 | The Boeing Company | Method and apparatus for reinforcing composite structures |
| US8490920B2 (en) * | 2007-10-12 | 2013-07-23 | Abe Karem | Composite bulkhead and skin construction |
| DE102008013365B4 (de) * | 2008-03-10 | 2011-03-17 | Airbus Operations Gmbh | Querstoßverbindung zwischen zwei Rumpfsektionen |
| GB0805268D0 (en) * | 2008-03-25 | 2008-04-30 | Airbus Uk Ltd | Composite joint protection |
| GB0805963D0 (en) * | 2008-04-02 | 2008-05-07 | Airbus Uk Ltd | Aircraft structure |
| IT1390909B1 (it) * | 2008-07-16 | 2011-10-19 | Alenia Aeronautica Spa | Elemento strutturale a rigidezza calcolata, con caratteristiche di assorbimento di spostamenti e copertura interstizi |
| FR2936495B1 (fr) * | 2008-09-30 | 2011-06-03 | Airbus France | Assemblage de panneaux pour fuselage d'aeronef. |
| GB0901640D0 (en) * | 2009-02-03 | 2009-03-11 | Airbus Uk Ltd | Joint |
| ES2384920B1 (es) * | 2009-03-31 | 2013-05-21 | Airbus Operations, S.L. | Pieza de material con una rampa entre dos zonas. |
| GB0905818D0 (en) * | 2009-04-06 | 2009-05-20 | Airbus Uk Ltd | Coupling assembly |
| US8282042B2 (en) * | 2009-06-22 | 2012-10-09 | The Boeing Company | Skin panel joint for improved airflow |
| GB0910938D0 (en) * | 2009-06-25 | 2009-08-05 | Airbus Operations Ltd | Method of manufacturing a structure |
| EP2316629B1 (en) * | 2009-10-27 | 2012-05-23 | Lm Glasfiber A/S | Modular mould system for manufacturing a shell part |
| DE102009060693A1 (de) * | 2009-12-29 | 2011-06-30 | Airbus Operations GmbH, 21129 | Versteifungselement für ein Luftfahrzeug und Flächengebilde mit einem derartigen Versteifungselement |
| ES2396327B1 (es) * | 2010-06-10 | 2014-02-06 | Airbus Operations, S.L. | Procedimiento para la fabricación de piezas grandes de material compuesto controlando el espesor de sus bordes |
| DE102010026839A1 (de) | 2010-07-12 | 2012-01-12 | Airbus Operations Gmbh | Aerodynamische Verkleidungsvorrichtung, Flugzeug-Bauteilanordnung mit einer aerodynamischen Verkleidungsvorrichtung sowie Verfahren zur Montage eines solchen Verkleidungsteils |
| US8333345B2 (en) * | 2010-08-26 | 2012-12-18 | The Boeing Company | Composite aircraft joint |
| GB201016279D0 (en) | 2010-09-28 | 2010-11-10 | Airbus Operations Ltd | Stiffener run-out |
| ES2396881B1 (es) * | 2010-11-30 | 2014-01-29 | Airbus Operations, S.L. | Disposición de interfaz entre dos componentes de una estructura de una aeronave usando una pieza de sellado. |
| ES2396882B1 (es) * | 2010-11-30 | 2014-01-29 | Airbus Operations, S.L. | Disposición de interfaz entre dos componentes de una estructura de una aeronave. |
| ES2403361B1 (es) * | 2010-12-17 | 2014-04-29 | Airbus Operations, S.L. | Optimización de estructuras sometidas a corrientes de gases calientes. |
| FR2970463B1 (fr) * | 2011-01-17 | 2013-02-15 | Airbus Operations Sas | Dispositif d'eclissage a tenue mecanique amelioree. |
| RU2475425C1 (ru) * | 2011-10-06 | 2013-02-20 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" | Устройство металлизации корпуса изделия |
| US20130114994A1 (en) | 2011-11-04 | 2013-05-09 | Robert Erik Grip | Truss end pad fitting |
| US9574587B2 (en) | 2011-11-04 | 2017-02-21 | The Boeing Company | Preloading a fastener of a mechanical fitting |
| GB201200912D0 (en) * | 2012-01-19 | 2012-02-29 | Airbus Operations Ltd | Fastener receptacle strip |
| GB201205079D0 (en) * | 2012-03-22 | 2012-05-09 | Airbus Operations Ltd | Seal assembly for an aircraft wing |
| US9180956B1 (en) * | 2012-04-11 | 2015-11-10 | The Boeing Company | Methods and apparatus for attaching an aircraft wing assembly to an aircraft body |
| ES2426111B1 (es) * | 2012-04-17 | 2015-03-24 | Airbus Operations S.L. | Interfaz para superficie de sustentación de aeronave |
| EP2653376B1 (en) * | 2012-04-18 | 2016-03-23 | Airbus Operations, S.L. | Bolted joint of the cover of an access opening in an aircraft lifting surface |
| GB201209437D0 (en) * | 2012-05-28 | 2012-07-11 | Kitchener Renato | Power supply and battery charger |
| US8985514B2 (en) * | 2012-06-20 | 2015-03-24 | The Boeing Company | Composite structural panels and aircraft fuselages |
| US8857765B2 (en) * | 2012-10-16 | 2014-10-14 | The Boeing Company | Method and apparatus for attaching an aircraft fuselage frame to a wing box |
| EP2909486B1 (en) * | 2012-10-22 | 2018-12-12 | BAE SYSTEMS plc | Hybrid joint manufacutring |
| US9415853B2 (en) * | 2013-01-30 | 2016-08-16 | The Boeing Company | Surface sealing system |
| FR3015433B1 (fr) | 2013-12-23 | 2016-02-12 | Airbus Operations Sas | Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage |
| US9399507B2 (en) | 2014-01-22 | 2016-07-26 | The Boeing Company | Joints between a composite skin and a load-bearing component and methods of forming same |
| US9676469B2 (en) | 2014-04-10 | 2017-06-13 | Lockheed Martin Corporation | System and method for fastening structures |
| US10603888B2 (en) * | 2014-04-10 | 2020-03-31 | The Boeing Company | Filling and leveling methods and apparatus for building tight tolerance surfaces |
| US9896190B1 (en) * | 2014-05-07 | 2018-02-20 | The Boeing Company | Wing leading edge architecture suitable for laminar flow |
| EP3142923B1 (en) * | 2014-05-15 | 2020-05-06 | Sikorsky Aircraft Corporation | Metallic dimpled doubler |
| US10329009B2 (en) * | 2014-09-17 | 2019-06-25 | The Boeing Company | Composite wing edge attachment and method |
| US9925625B2 (en) * | 2015-05-04 | 2018-03-27 | The Boeing Company | Assembly of an aircraft structure assembly without shimming, locating fixtures or final-hole-size drill jigs |
| DE102016210325B4 (de) * | 2016-06-10 | 2021-07-15 | Airbus Operations Gmbh | Bauteilanordnung zur Ausbildung einer Tragstruktur eines Luft- oder Raumfahrzeugs |
| CN106697327B (zh) * | 2016-12-19 | 2019-10-18 | 中航成飞民用飞机有限责任公司 | 飞机壁板对接结构 |
| US10773789B2 (en) * | 2017-07-07 | 2020-09-15 | The Boeing Company | Skin-panel interface of an aircraft |
| CN109677586A (zh) * | 2019-01-18 | 2019-04-26 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | 一种腹板、飞机机翼和飞机 |
| US11884055B2 (en) * | 2019-03-26 | 2024-01-30 | The Boeing Company | Laminated hybrid metallized polymer films, system, and method for erosion protection of composite structures |
| US11383820B2 (en) * | 2019-06-11 | 2022-07-12 | The Boeing Company | Aerodynamic surface lap splice |
| CN110466734B (zh) * | 2019-08-26 | 2022-08-19 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种锯齿缝对接蒙皮的带板 |
| US11524762B2 (en) * | 2020-02-21 | 2022-12-13 | The Boeing Company | Fuselage structure splice |
| US11572152B2 (en) | 2020-05-21 | 2023-02-07 | The Boeing Company | Structural composite airfoils with a single spar, and related methods |
| US11401026B2 (en) | 2020-05-21 | 2022-08-02 | The Boeing Company | Structural composite airfoils with a single spar, and related methods |
| US11554848B2 (en) | 2020-05-21 | 2023-01-17 | The Boeing Company | Structural composite airfoils with a single spar, and related methods |
| US11453476B2 (en) * | 2020-05-21 | 2022-09-27 | The Boeing Company | Structural composite airfoils with an improved leading edge, and related methods |
| CN114771802A (zh) | 2021-01-22 | 2022-07-22 | 波音公司 | 空气动力学结构以及形成空气动力学结构的方法 |
| EP4053014B1 (en) * | 2021-03-05 | 2024-12-18 | The Boeing Company | Assembly and method connecting an aircraft wing aft spar root to an aircraft body fuselage |
| CN113376044B (zh) * | 2021-06-10 | 2022-07-12 | 中国兵器工业第五九研究所 | 一种高温高压气体冲刷实验装置 |
| CN114684346A (zh) * | 2021-12-31 | 2022-07-01 | 中国航空工业集团公司西安飞机设计研究所 | 一种长桁接头 |
| EP4303120A1 (en) * | 2022-07-07 | 2024-01-10 | Airbus Operations S.L.U. | Composite multi-spar aircraft lifting surface |
| CN119489923A (zh) * | 2024-12-25 | 2025-02-21 | 中国航空工业集团公司西安飞机设计研究所 | 一种加筋壁板对接结构及设计方法 |
Family Cites Families (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE704327C (de) * | 1939-02-09 | 1941-03-28 | Henschel Flugzeug Werke A G | Flugzeugfluegel |
| GB1022131A (en) * | 1963-06-10 | 1966-03-09 | Monte Copter Inc | Sectional airfoil |
| IL63240A (en) | 1980-07-11 | 1984-12-31 | Weecan Marine | Method and apparatus for manufacturing an integral shell formed body |
| US4507011A (en) * | 1982-05-03 | 1985-03-26 | The Boeing Company | Reinforced elastomer attachment joint |
| SU1420823A1 (ru) * | 1987-01-30 | 1996-09-20 | Е.А. Бычковский | Хвостовая часть крыла самолета |
| JPS63240494A (ja) * | 1987-03-26 | 1988-10-06 | 川崎重工業株式会社 | 航空機用翼の前縁保護構造 |
| US4888451A (en) | 1988-11-29 | 1989-12-19 | United Technologies Corporation | Electrical continuity means for composite joints |
| US5803406A (en) * | 1996-04-22 | 1998-09-08 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Integrated thermal insulation system for spacecraft |
| US6375120B1 (en) * | 1997-07-14 | 2002-04-23 | Jason M. Wolnek | Method and apparatus for building a metal/composite hybrid airplane component |
| RU12819U1 (ru) * | 1999-04-28 | 2000-02-10 | Егер Владимир Сергеевич | Композитное кессонное крыло легкого самолета |
| WO2002014147A1 (en) * | 2000-08-11 | 2002-02-21 | Dunlop Aerospace Limited | Wheel hub assemblies |
| DE10238820A1 (de) * | 2002-08-23 | 2004-03-11 | Airbus Deutschland Gmbh | Anordung zur Erfindung von dünnwandigen Metallstrukturen |
| GB0329373D0 (en) * | 2003-12-18 | 2004-01-21 | Airbus Uk Ltd | Method of joining structural elements in an aircraft |
| US7554785B2 (en) * | 2004-03-23 | 2009-06-30 | The Boeing Company | Lightning damage protection for composite aircraft |
| US20060251496A1 (en) * | 2004-07-09 | 2006-11-09 | Bae Systems Plc | Fastener arrangement for fastening a detachable panel |
| US7296656B2 (en) * | 2005-04-22 | 2007-11-20 | United Technologies Corporation | Acoustic mechanical retainer |
| FR2905739B1 (fr) * | 2006-09-08 | 2008-11-07 | Airbus France Sas | Assemblage de panneaux et procede de montage d'un assemblage de panneaux |
| JP4657194B2 (ja) * | 2006-11-20 | 2011-03-23 | 本田技研工業株式会社 | 前縁スキンの段差調整構造および前縁スキンの組付方法 |
| US8016230B2 (en) * | 2007-05-11 | 2011-09-13 | The Boeing Company | Fastner-free primary structural joint for sandwich panels |
| US8398027B2 (en) * | 2007-09-17 | 2013-03-19 | The Boeing Company | Method and apparatus for reinforcing composite structures |
-
2005
- 2005-12-20 GB GBGB0525896.7A patent/GB0525896D0/en not_active Ceased
-
2006
- 2006-11-28 EP EP06808699A patent/EP1963178B1/en not_active Ceased
- 2006-11-28 WO PCT/GB2006/004439 patent/WO2007071905A1/en not_active Ceased
- 2006-11-28 CN CNA2006800478322A patent/CN101341070A/zh active Pending
- 2006-11-28 US US13/886,454 patent/USRE47738E1/en not_active Expired - Fee Related
- 2006-11-28 BR BRPI0620070-2A patent/BRPI0620070A2/pt not_active IP Right Cessation
- 2006-11-28 JP JP2008546567A patent/JP2009519861A/ja active Pending
- 2006-11-28 US US12/097,328 patent/US7909290B2/en not_active Ceased
- 2006-11-28 RU RU2008129606/11A patent/RU2427500C2/ru not_active IP Right Cessation
- 2006-11-28 AT AT06808699T patent/ATE476359T1/de not_active IP Right Cessation
- 2006-11-28 DE DE602006016006T patent/DE602006016006D1/de active Active
- 2006-11-28 CA CA2633106A patent/CA2633106C/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| ATE476359T1 (de) | 2010-08-15 |
| GB0525896D0 (en) | 2006-02-01 |
| JP2009519861A (ja) | 2009-05-21 |
| EP1963178A1 (en) | 2008-09-03 |
| RU2427500C2 (ru) | 2011-08-27 |
| US20080258008A1 (en) | 2008-10-23 |
| CN101341070A (zh) | 2009-01-07 |
| DE602006016006D1 (de) | 2010-09-16 |
| CA2633106C (en) | 2013-08-06 |
| USRE47738E1 (en) | 2019-11-26 |
| EP1963178B1 (en) | 2010-08-04 |
| RU2008129606A (ru) | 2010-01-27 |
| US7909290B2 (en) | 2011-03-22 |
| CA2633106A1 (en) | 2007-06-28 |
| WO2007071905A1 (en) | 2007-06-28 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B25D | Requested change of name of applicant approved |
Owner name: AIRBUS OPERATIONS LIMITED (GB) Free format text: NOME ALTERADO DE: AIRBUS UK LIMITED |
|
| B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 7A ANUIDADE. |
|
| 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: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2261 DE 06/05/2014. |