EP 4107061 A1 20221228 - METHOD FOR MANUFACTURING AN AERODYNAMIC AIRCRAFT STRUCTURE AND AERODYNAMIC AIRCRAFT STRUCTURE THUS OBTAINED
Title (en)
METHOD FOR MANUFACTURING AN AERODYNAMIC AIRCRAFT STRUCTURE AND AERODYNAMIC AIRCRAFT STRUCTURE THUS OBTAINED
Title (de)
VERFAHREN ZUR HERSTELLUNG EINER AERODYNAMISCHEN STRUKTUR EINES LUFTFAHRZEUGS UND SO HERGESTELLTE AERODYNAMISCHE STRUKTUR EINES LUFTFAHRZEUGS
Title (fr)
PROCEDE DE FABRICATION D'UNE STRUCTURE AERODYNAMIQUE D'AERONEF ET STRUCTURE AERODYNAMIQUE D'AERONEF AINSI OBTENUE
Publication
Application
Priority
- FR 2001597 A 20200218
- EP 2021053786 W 20210216
Abstract (en)
[origin: WO2021165268A1] The invention relates to a method for manufacturing an aerodynamic structure (34) comprising a first panel (42) having an aerodynamic face (F34) as well as a second reinforced panel (44), characterised in that the manufacturing method comprises a step of stamping the second panel (44) to obtain at least one raised shape (46) which is recessed on the second face (44.2), as well as a step of joining the first and second panels (42, 44) by pressing them against each other outside the raised shape(s) (46). The invention also relates to an aerodynamic structure obtained using said method.
IPC 8 full level
B64C 9/32 (2006.01); B64C 9/00 (2006.01); B64F 5/10 (2017.01)
CPC (source: EP US)
B64C 9/00 (2013.01 - EP); B64C 9/32 (2013.01 - EP US); B64F 5/10 (2016.12 - EP US)
Citation (search report)
See references of WO 2021165268A1
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
Designated validation state (EPC)
KH MA MD TN
DOCDB simple family (publication)
FR 3107254 A1 20210820; CN 115103799 A 20220923; EP 4107061 A1 20221228; US 2023062638 A1 20230302; WO 2021165268 A1 20210826
DOCDB simple family (application)
FR 2001597 A 20200218; CN 202180014880 A 20210216; EP 2021053786 W 20210216; EP 21706530 A 20210216; US 202117799954 A 20210216