A bulkhead joint assembly that includes a strap section configured to secure to an aft section of a fuselage and forward section of the fuselage and extend past a bulkhead of the fuselage. The bulkhead joint assembly also includes a chord engaging and secured to the strap section, wherein the chord is configured to extend along the bulkhead to transfer a force from the bulkhead in shear between the chord and the strap section.
BULKHEAD JOINT ASSEMBLY
2020-04-23
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |