A connector for connecting a frame to a transversely extending stringer of a fuselage structure of an aircraft includes a base carrier extending in a longitudinal connector direction, a first connecting portion connected to the base carrier and extending in a first transverse connector direction, the first connecting portion having a coupling structure in an end region remote from the base carrier for engaging around an end region of a cross-section of the stringer, and a second connecting portion connected to the base carrier and adapted to be connected to the frame.
VERBINDER UND VERFAHREN ZUM VERBINDEN EINES SPANTS UND EINES STRINGERS EINER RUMPFSTRUKTUR EINES LUFTFAHRZEUGS, RUMPFSTRUKTUR UND LUFTFAHRZEUG
CONNECTOR AND METHOD FOR CONNECTING A FRAME AND A STRINGER OF A FUSELAGE STRUCTURE OF AN AIRCRAFT, FUSELAGE STRUCTURE AND AIRCRAFT
CONNECTEUR ET PROCÉDÉ DE CONNEXION D'UN CADRE ET D'UN LONGERON D'UNE STRUCTURE DE FUSELAGE D'UN AÉRONEF, STRUCTURE DE FUSELAGE ET AÉRONEF
02.07.2025
Patent
Elektronische Ressource
Deutsch
IPC: | B64C AEROPLANES , Flugzeuge |
INNENVERKLEIDUNGSTEIL ZUR VERKLEIDUNG EINER RUMPFSTRUKTUR EINES LUFTFAHRZEUGS
Europäisches Patentamt | 2021
|Europäisches Patentamt | 2021
|Europäisches Patentamt | 2017
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