AT342785T

Method of welding, by using for example friction stir welding, surfaces with polymers sealant and welded structure

Abstract

Aircraft components, such as assembly 10, for example to form a lap joint between the inner surface of the outside sheathing reinforcement 14 and part 12, using a friction stir welding (FSW) is formed by a weld joint. Monomer sealant / adhesive agent, such as being applied to a surface for the sealing agent layer 24 are combined, the welds 16 and 18, the part 12 is the fluorine-containing coating, such as an elastomeric joint surface welding for sealing is formed in order to prevent corrosion of It is suitably cured by elevated temperatures of the process. Additional heat for curing can be made by a laser 30 or the induction heater 30.Welding, aircraft, reinforcing materials, components, friction stir welding, a sealant

Term

Term ended

Expired 5 August 2023, 3.1 years ago.

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24 members in 13 offices

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Priority claims
DocumentOfficeKindDate
40250502United States of AmericaP

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CA2494143A1CanadaA1
WO2004014593A1World Intellectual Property Organization (WIPO)A1
AU2003258106A1AustraliaA1
WO2004014593B1World Intellectual Property Organization (WIPO)B1
US2004173662A1United States of AmericaA1
EP1556186A1European Patent Office (EPO)A1
KR20050083615ARepublic of KoreaA
CN1675019AChinaA
RU2005106228ARussian FederationA
JP2005534499AJapanA
IL166643D0IsraelD0
EP1556186B1European Patent Office (EPO)B1
AT342785TThis recordAustriaT
ATE342785T1AustriaT1
DE60309194D1GermanyD1
ES2274303T3SpainT3
US7225966B2United States of AmericaB2
DE60309194T2GermanyT2
RU2325981C2Russian FederationC2
CN100398247CChinaC
AU2003258106B2AustraliaB2
KR101036076B1Republic of KoreaB1
JP4694200B2JapanB2
CA2494143CCanadaC