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
2022-07-20
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |