EP 3864184 A1 20210818 - METAL SHEET MADE OF HIGH-STRENGTH 2XXX ALLOY FOR AN AIRCRAFT FUSELAGE
Title (en)
METAL SHEET MADE OF HIGH-STRENGTH 2XXX ALLOY FOR AN AIRCRAFT FUSELAGE
Title (de)
BLECH AUS HOCHFESTER 2XXX-LEGIERUNG FÜR FLUGZEUGRUMPF
Title (fr)
TOLE EN ALLIAGE 2XXX A HAUTE PERFORMANCE POUR FUSELAGE D'AVION
Publication
Application
Priority
- FR 1871158 A 20181010
- FR 2019052373 W 20191007
Abstract (en)
[origin: WO2020074818A1] The invention relates to a thin metal sheet which is made of an alloy based on substantially recrystallized aluminum and which has a thickness of 0.25 to 12 mm, the alloy comprising, in percent by weight, Cu 3.4-4.0; Mg 0.5–0.8; Mn 0.1–0.7; Fe ≤ 0.15; Si ≤ 0.15; Zr ≤ 0.04; Ag ≤ 0.65; Zn ≤ 0.5; inevitable impurities ≤ 0.05 each and ≤ 0.15 in total, the remainder consisting of aluminum. The invention also relates to a process for manufacturing such a metal sheet and to the use thereof as a fuselage panel or sheet metal for the production of composite products such as fiber metal laminates (FML) for wing or fuselage applications in the aeronautical industry.
IPC 8 full level
C22C 21/16 (2006.01); C22C 21/18 (2006.01); C22F 1/057 (2006.01)
CPC (source: EP US)
B64C 1/00 (2013.01 - EP US); C22C 1/02 (2013.01 - US); C22C 21/16 (2013.01 - EP US); C22C 21/18 (2013.01 - EP US); C22F 1/057 (2013.01 - EP US); B64C 2001/0081 (2013.01 - US)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
Designated extension state (EPC)
BA ME
DOCDB simple family (publication)
WO 2020074818 A1 20200416; BR 112021006605 A2 20210706; CA 3115014 A1 20200416; CN 112805397 A 20210514; EP 3864184 A1 20210818; FR 3087206 A1 20200417; FR 3087206 B1 20220211; US 2021388470 A1 20211216
DOCDB simple family (application)
FR 2019052373 W 20191007; BR 112021006605 A 20191007; CA 3115014 A 20191007; CN 201980065873 A 20191007; EP 19816820 A 20191007; FR 1871158 A 20181010; US 201917284373 A 20191007