A bulkhead (300) joint assembly (312) that includes a strap section (314) configured to secure to an aft section of a fuselage and forward section (308) of the fuselage and extend past a bulkhead (300) of the fuselage. The bulkhead joint assembly (312) also includes a chord (318) engaging and secured to the strap section (314), wherein the chord (318) is configured to extend along the bulkhead (300) to transfer a force from the bulkhead (300) in shear between the chord (318) and the strap section (314).
BULKHEAD JOINT ASSEMBLY
DRUCKSCHOTTVERBINDUNGSANORDNUNG
ENSEMBLE DE JOINT DE CLOISON
20.07.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |