An assembly comprising a fuel stringer duct (5), a bulkhead (200), and a bulkhead retainer (150) is disclosed. The bulkhead (200) is positioned in the fuel stringer duct (5) to block the flow of fluid along the fuel stringer duct (5). The bulkhead retainer (200) comprises a retainer portion (152) that extends through an opening (52) in a wall of the fuel stringer duct (5) and which is configured to abut with the bulkhead (200) to prevent movement of the bulkhead (200) along the fuel stringer duct (5). A method of installing a bulkhead (200) in a fuel stringer duct (5) is also disclosed.
IMPROVEMENTS RELATING TO FUEL STRINGER DUCT BULKHEADS
VERBESSERUNGEN IM ZUSAMMENHANG MIT KRAFTSTOFFSTRINGERKANALSCHOTTEN
PERFECTIONNEMENTS RELATIFS AUX CLOISONS DE CONDUIT DE LISSE DE CARBURANT
2025-04-23
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |