The present application relates to an aircraft assembly and, in particular, a wing leading edge wing assembly. The assembly includes a structural component, such as a leading edge panel, and a cover panel located over the structural component. The cover panel has a thermoplastic layer with an inner surface. A thermoplastic fastening member extends through the structural component and is welded to the inner surface so that the structural component is fastened between the inner surface and the fastening member.
AIRCRAFT ASSEMBLY, METHOD OF ASSEMBLING AN AIRCRAFT ASSEMBLY, AND KIT OF PARTS
FLUGZEUGBAUGRUPPE, VERFAHREN ZUR ZUSAMMENBAU EINER FLUGZEUGBAUGRUPPE UND KIT VON TEILEN
ASSEMBLAGE DANS UN AÉRONEF, PROCÉDÉ D'ASSEMBLAGE D'UN ASSEMBLAGE DANS UN AÉRONEF ET KIT DE PIÈCES
2021-10-13
Patent
Electronic Resource
English
IPC: | B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B29L INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES , Index-Schema für besondere Gegenstände in Verbindung mit Unterklasse B29C / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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