BRPI1014325B1 - método para formar uma junta e aparelho - Google Patents
método para formar uma junta e aparelho Download PDFInfo
- Publication number
- BRPI1014325B1 BRPI1014325B1 BRPI1014325A BRPI1014325A BRPI1014325B1 BR PI1014325 B1 BRPI1014325 B1 BR PI1014325B1 BR PI1014325 A BRPI1014325 A BR PI1014325A BR PI1014325 A BRPI1014325 A BR PI1014325A BR PI1014325 B1 BRPI1014325 B1 BR PI1014325B1
- Authority
- BR
- Brazil
- Prior art keywords
- strip
- panel
- flange
- channel
- adhesive
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims abstract description 97
- 239000012530 fluid Substances 0.000 claims abstract description 34
- 238000009434 installation Methods 0.000 claims description 133
- 239000000853 adhesive Substances 0.000 claims description 119
- 230000001070 adhesive effect Effects 0.000 claims description 118
- 239000011248 coating agent Substances 0.000 claims description 61
- 238000000576 coating method Methods 0.000 claims description 61
- 238000005304 joining Methods 0.000 claims description 10
- 239000002390 adhesive tape Substances 0.000 claims description 7
- 238000005253 cladding Methods 0.000 description 119
- 239000000463 material Substances 0.000 description 53
- 230000008569 process Effects 0.000 description 39
- 230000000670 limiting effect Effects 0.000 description 34
- 238000004519 manufacturing process Methods 0.000 description 20
- 230000000873 masking effect Effects 0.000 description 20
- 229910052782 aluminium Inorganic materials 0.000 description 19
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 19
- 238000012423 maintenance Methods 0.000 description 19
- 239000002131 composite material Substances 0.000 description 16
- 229910000831 Steel Inorganic materials 0.000 description 15
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 15
- 239000010959 steel Substances 0.000 description 15
- 239000010936 titanium Substances 0.000 description 15
- 229910052719 titanium Inorganic materials 0.000 description 15
- 239000003381 stabilizer Substances 0.000 description 8
- 239000000945 filler Substances 0.000 description 6
- 239000000565 sealant Substances 0.000 description 6
- 239000004593 Epoxy Substances 0.000 description 5
- 238000002513 implantation Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 238000013459 approach Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000010354 integration Effects 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 230000000149 penetrating effect Effects 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- 239000000725 suspension Substances 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 241001669679 Eleotris Species 0.000 description 1
- 229910001200 Ferrotitanium Inorganic materials 0.000 description 1
- 239000003570 air Substances 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 210000000078 claw Anatomy 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000003733 fiber-reinforced composite Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000007943 implant Substances 0.000 description 1
- 239000012035 limiting reagent Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000002829 reductive effect Effects 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000002023 wood Substances 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
- B64C7/00—Structures or fairings not otherwise provided for
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
-
- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
- Laminated Bodies (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/489,142 US8282042B2 (en) | 2009-06-22 | 2009-06-22 | Skin panel joint for improved airflow |
| PCT/US2010/032615 WO2011005350A2 (en) | 2009-06-22 | 2010-04-27 | Skin panel joint for improved airflow |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| BRPI1014325A2 BRPI1014325A2 (pt) | 2016-04-05 |
| BRPI1014325B1 true BRPI1014325B1 (pt) | 2020-05-19 |
Family
ID=43353435
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI1014325A BRPI1014325B1 (pt) | 2009-06-22 | 2010-04-27 | método para formar uma junta e aparelho |
Country Status (7)
| Country | Link |
|---|---|
| US (2) | US8282042B2 (enExample) |
| EP (1) | EP2445785B1 (enExample) |
| JP (1) | JP2012530653A (enExample) |
| CN (1) | CN102458981B (enExample) |
| BR (1) | BRPI1014325B1 (enExample) |
| CA (1) | CA2765568C (enExample) |
| WO (1) | WO2011005350A2 (enExample) |
Families Citing this family (36)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7325771B2 (en) * | 2004-09-23 | 2008-02-05 | The Boeing Company | Splice joints for composite aircraft fuselages and other structures |
| FR2932106B1 (fr) * | 2008-06-06 | 2010-05-21 | Airbus France | Procede de depose d'un revetement visant a ameliorer l'ecoulement laminaire |
| FR2932456B1 (fr) * | 2008-06-17 | 2010-05-28 | Airbus France | Systeme de drainage d'un courant de foudre genere par une decharge orageuse sur un aeronef |
| GB0901640D0 (en) * | 2009-02-03 | 2009-03-11 | Airbus Uk Ltd | Joint |
| US8282042B2 (en) | 2009-06-22 | 2012-10-09 | The Boeing Company | Skin panel joint for improved airflow |
| US9821538B1 (en) * | 2009-06-22 | 2017-11-21 | The Boeing Company | Ribbed caul plate for attaching a strip to a panel structure and method for use |
| FR2947523B1 (fr) * | 2009-07-03 | 2011-07-22 | Airbus Operations Sas | Element de fuselage comportant un troncon de fuselage et des moyens de jonction |
| EP2487106B1 (en) * | 2009-10-08 | 2018-07-25 | Mitsubishi Heavy Industries, Ltd. | Composite material structure, as well as aircraft wing and fuselage provided therewith |
| US8985515B2 (en) * | 2010-12-28 | 2015-03-24 | Textron Innovations Inc. | Multi-directional load joint system |
| GB201107071D0 (en) | 2011-04-27 | 2011-06-08 | Airbus Uk Ltd | Method of sealing a gap |
| DE102011111864A1 (de) * | 2011-08-31 | 2013-02-28 | Airbus Operations Gmbh | Abdecksystem für einen Innenraum eines Fahrzeugs, Verfahren zum Abdecken eines Bereichs eines Innenraums eines Fahrzeugs und Fahrzeug mit einem Innenraum, der zumindest bereichsweise durch das Abdecksystem abgedeckt ist |
| ES2627541T3 (es) | 2012-04-20 | 2017-07-28 | Ucb Pharma, S.A. | Métodos para tratar la enfermedad de Parkinson |
| US20130299073A1 (en) * | 2012-05-08 | 2013-11-14 | Lockheed Martin Corporation | Contour caul with expansion region |
| US9180958B2 (en) * | 2012-05-25 | 2015-11-10 | The Boeing Company | Aircraft, airframes and associated methods |
| US9279531B2 (en) | 2012-12-17 | 2016-03-08 | United Technologies Corporation | Composite ducts and methods |
| US9415853B2 (en) * | 2013-01-30 | 2016-08-16 | The Boeing Company | Surface sealing system |
| DE102013102812B4 (de) * | 2013-03-19 | 2017-01-26 | Airbus Operations Gmbh | Rumpfstruktur für ein Verkehrsmittel, Verkehrsmittel und Verfahren zum Herstellen einer Rumpfstruktur für ein Verkehrsmittel |
| US9096324B2 (en) | 2013-03-19 | 2015-08-04 | The Boeing Company | Joint assembly to form a sealed flow conduit |
| US20140331477A1 (en) * | 2013-05-07 | 2014-11-13 | The Boeing Company | Flush fastener design and installation |
| US9487288B2 (en) | 2013-06-04 | 2016-11-08 | The Boeing Company | Apparatus and methods for extending hybrid laminar flow control |
| US9272773B2 (en) | 2013-09-25 | 2016-03-01 | The Boeing Company | Apparatus and methods to operate laminar flow control doors |
| US10603888B2 (en) * | 2014-04-10 | 2020-03-31 | The Boeing Company | Filling and leveling methods and apparatus for building tight tolerance surfaces |
| US9676469B2 (en) * | 2014-04-10 | 2017-06-13 | Lockheed Martin Corporation | System and method for fastening structures |
| US9896190B1 (en) * | 2014-05-07 | 2018-02-20 | The Boeing Company | Wing leading edge architecture suitable for laminar flow |
| US11004661B2 (en) | 2015-09-04 | 2021-05-11 | Applied Materials, Inc. | Process chamber for cyclic and selective material removal and etching |
| EP3299297B1 (en) | 2016-09-27 | 2018-12-12 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | A rotary wing aircraft with a structural arrangement that comprises an electrically conductive connection |
| US10926858B2 (en) * | 2017-08-07 | 2021-02-23 | The Boeing Company | Pressure bulkhead system |
| US20190351624A1 (en) * | 2018-05-16 | 2019-11-21 | GM Global Technology Operations LLC | Systems and processes for repairing fiber-reinforced polymer structures |
| US11167836B2 (en) | 2018-06-21 | 2021-11-09 | Sierra Nevada Corporation | Devices and methods to attach composite core to a surrounding structure |
| GB2588340B (en) | 2018-06-21 | 2023-08-09 | Sierra Nevada Corp | Net edge composite core splices for aircraft wing |
| JP7625524B2 (ja) | 2019-01-11 | 2025-02-03 | オメロス コーポレーション | がんを処置するための方法および組成物 |
| GB2583352B (en) | 2019-04-24 | 2023-09-06 | Univ Southampton | Antiresonant hollow core fibre, preform therefor and method of fabrication |
| DE102019113566B4 (de) * | 2019-05-21 | 2021-03-18 | Airbus Defence and Space GmbH | Druckplattenanordnung, Herstellungsanordnung, Vorrichtung und Verfahren zum Herstellen eines Übergangsbereichs zwischen aerodynamischen Profilelementen |
| CN110576962B (zh) * | 2019-07-10 | 2021-02-09 | 青岛中科方舟航空科技有限公司 | 蒙皮铺装工艺以及无人机 |
| DE102021105806B4 (de) | 2021-03-10 | 2024-04-11 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Aerodynamischer Profilkörper für Luftfahrzeuge |
| DE102023102200B3 (de) | 2023-01-31 | 2024-02-01 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Aerodynamischer Profilkörper für Luftfahrzeuge |
Family Cites Families (38)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7018A (en) * | 1850-01-15 | File for keeping papers | ||
| US2841344A (en) * | 1955-11-28 | 1958-07-01 | Stroukoff Michael | Boundary layer control |
| US2997262A (en) | 1960-01-21 | 1961-08-22 | Gen Dynamics Corp | Aircraft wing structure |
| FR1523404A (fr) * | 1967-03-22 | 1968-05-03 | Sud Aviation | Perfectionnement aux raccordements entre fuselage et voilure d'un aérodyne |
| US4316701A (en) | 1976-08-30 | 1982-02-23 | The Boeing Company | Composite aerodynamic rotor blade assembly |
| US4575030A (en) | 1982-09-13 | 1986-03-11 | The Boeing Company | Laminar flow control airfoil |
| US4619423A (en) | 1983-11-10 | 1986-10-28 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Geometries for roughness shapes in laminar flow |
| US4727451A (en) | 1987-01-06 | 1988-02-23 | The Boeing Company | Metallic conduction method and system for joined sections of composite structures |
| US4888451A (en) * | 1988-11-29 | 1989-12-19 | United Technologies Corporation | Electrical continuity means for composite joints |
| US5014934A (en) | 1989-06-30 | 1991-05-14 | The Boeing Company | Removable seal for discontinuities in aircraft skin |
| US5065960A (en) | 1990-02-05 | 1991-11-19 | Northrop Corporation | Gap filler for advanced aircraft to reduce radar detectability |
| US5106037A (en) | 1990-02-05 | 1992-04-21 | Northrop Corporation | Umbrella seal for aircraft |
| US5368258A (en) * | 1993-08-05 | 1994-11-29 | Rohr, Inc. | Arrangement for maintaining laminar air flow over gaps in aircraft engine nacelle surfaces |
| US5487822A (en) * | 1993-11-24 | 1996-01-30 | Applied Materials, Inc. | Integrated sputtering target assembly |
| GB9411006D0 (en) | 1994-06-02 | 1994-07-20 | British Aerospace | Method of fastening composite aircraft skins |
| ATE226512T1 (de) | 1997-05-28 | 2002-11-15 | Structural Laminates Co | Verfahren zur herstellung eines mehrschichtwerkstoffes und ein mehrschichtwerkstoff der mit diesem verfahren herzustellen ist |
| JP2000159284A (ja) * | 1998-11-27 | 2000-06-13 | Fuji Photo Film Co Ltd | 磁気テープカセット用収納ケース |
| US6357374B1 (en) * | 2000-07-21 | 2002-03-19 | Cortana Corporation | Method and apparatus for increasing the effectiveness and efficiency of multiple boundary layer control techniques |
| US7202321B2 (en) | 2002-06-07 | 2007-04-10 | The Boeing Company | Method and composition for sealing components and components sealed thereby |
| US20040035979A1 (en) | 2002-08-23 | 2004-02-26 | Mccoskey William Robert | Integrally stiffened axial load carrying skin panels for primary aircraft structure and closed loop manufacturing methods for making the same |
| US7143983B2 (en) * | 2002-08-28 | 2006-12-05 | Lockheed Martin Corporation | Passive jet spoiler for yaw control of an aircraft |
| EP1628879B1 (en) | 2003-05-30 | 2006-09-20 | BAE Systems PLC | Composite structure lightning protection |
| 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 |
| DE102004056649A1 (de) | 2004-11-24 | 2006-06-01 | Airbus Deutschland Gmbh | Deckhaut für eine formvariable aerodynamische Fläche |
| ES2277716B1 (es) * | 2004-12-31 | 2008-05-16 | Airbus España, S.L. | Tapa reforzada para ranuras en un contorno aerodinamico. |
| FR2891239B1 (fr) * | 2005-09-28 | 2009-04-17 | Airbus France Sas | Panneau de plancher et installation pour la fixation d'elements d'amenagement comportant de tels panneaux |
| GB0525896D0 (en) * | 2005-12-20 | 2006-02-01 | Airbus Uk Ltd | A joint for use in aircraft construction |
| FR2915458B1 (fr) | 2007-04-25 | 2010-01-01 | Airbus France | Assemblage de panneaux de fuselage d'un avion |
| US8016230B2 (en) | 2007-05-11 | 2011-09-13 | The Boeing Company | Fastner-free primary structural joint for sandwich panels |
| US7874779B2 (en) * | 2007-07-23 | 2011-01-25 | The Monadnock Company | Fasteners, fastener components and fastener receptacles |
| US7735780B2 (en) * | 2007-12-20 | 2010-06-15 | L-3 Communications Integrated Systems, L.P. | Aircraft stringer clip and related methods |
| DE102008013759B4 (de) * | 2008-03-12 | 2012-12-13 | Airbus Operations Gmbh | Verfahren zur Herstellung eines integralen Faserverbundbauteils sowie Kernform zur Durchführung des Verfahrens |
| FI20080208L (fi) * | 2008-03-13 | 2008-03-27 | Patria Aerostructures Oy | Ilma-aluksen johtoreunaelementti, menetelmä sen valmistamiseksi sekä siipi ja vakain |
| US20090266870A1 (en) * | 2008-04-23 | 2009-10-29 | The Boeing Company | Joined composite structures with a graded coefficient of thermal expansion for extreme environment applications |
| US20100078155A1 (en) * | 2008-09-30 | 2010-04-01 | Third Millennium Engineering | Thin Cavity Fluidic Heat Exchanger |
| US8714488B2 (en) * | 2009-01-08 | 2014-05-06 | The Boeing Company | Elastic aircraft joint fairing |
| US8209865B2 (en) * | 2009-06-04 | 2012-07-03 | Lockheed Martin Corporation | Method of manufacturing aircraft using temporary fasteners |
| US8282042B2 (en) | 2009-06-22 | 2012-10-09 | The Boeing Company | Skin panel joint for improved airflow |
-
2009
- 2009-06-22 US US12/489,142 patent/US8282042B2/en active Active
-
2010
- 2010-04-27 WO PCT/US2010/032615 patent/WO2011005350A2/en not_active Ceased
- 2010-04-27 JP JP2012517520A patent/JP2012530653A/ja active Pending
- 2010-04-27 CA CA2765568A patent/CA2765568C/en active Active
- 2010-04-27 CN CN201080028137.8A patent/CN102458981B/zh active Active
- 2010-04-27 BR BRPI1014325A patent/BRPI1014325B1/pt active IP Right Grant
- 2010-04-27 EP EP10716701.7A patent/EP2445785B1/en active Active
-
2012
- 2012-09-10 US US13/608,425 patent/US8393578B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US20100320325A1 (en) | 2010-12-23 |
| EP2445785B1 (en) | 2017-02-22 |
| CA2765568C (en) | 2018-03-06 |
| CN102458981B (zh) | 2015-06-03 |
| EP2445785A2 (en) | 2012-05-02 |
| US8393578B2 (en) | 2013-03-12 |
| US20130000821A1 (en) | 2013-01-03 |
| AU2010271125A1 (en) | 2011-12-01 |
| CN102458981A (zh) | 2012-05-16 |
| WO2011005350A2 (en) | 2011-01-13 |
| US8282042B2 (en) | 2012-10-09 |
| CA2765568A1 (en) | 2011-01-13 |
| JP2012530653A (ja) | 2012-12-06 |
| WO2011005350A3 (en) | 2011-07-21 |
| BRPI1014325A2 (pt) | 2016-04-05 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
| B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
| B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
| B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 19/05/2020, OBSERVADAS AS CONDICOES LEGAIS. |