A seal-cover assembly for a structure including a first side and a second side opposing the first side. The seal-cover assembly includes a cap defining a recess, and an insert fixed to the cap within the recess to form a cover unit. The cover unit is configured to be secured to the first side of the structure. The seal-cover assembly includes a fastener configured to be disposed through the structure from the second side of the structure. The fastener is attached to the cover unit relative to the second side without accessing the first side of the structure. Additionally, an aircraft includes the structure and the seal-cover assembly as discussed above. Furthermore, a method of assembling the seal-cover assembly to the structure includes the cover unit secured to the first side of the structure such that an interior of the cover unit is inaccessible from the first side.
SEAL-COVER ASSEMBLY FOR AN AIRCRAFT OR OTHER STRUCTURE AND A METHOD OF ASSEMBLING THE SAME
DICHTUNGSABDECKUNGSANORDNUNG FÜR EIN FLUGZEUG ODER EINE ANDERE STRUKTUR UND MONTAGEVERFAHREN DAFÜR
ENSEMBLE COUVERCLE ÉTANCHE POUR UN AÉRONEF OU UNE AUTRE STRUCTURE ET SON PROCÉDÉ D'ASSEMBLAGE
2024-02-07
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
SEAL-COVER ASSEMBLY FOR AN AIRCRAFT OR OTHER STRUCTURE AND A METHOD OF ASSEMBLING THE SAME
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