A fastening system to couple a first aircraft structure and a second aircraft structure is disclosed. The fastening system (110) includes a fastener (420), a nutplate (400) having a body (402) defining an opening (510) to receive the fastener (420), a flange (404) extending from the body (402) to engage an outer surface of the first structure, and a first sleeve (406) protruding from the flange (404) in a direction away from the body (402), the first sleeve (406) to couple to a first bore formed in the first structure and prevents rotation of the nutplate (400) relative to the first structure.
FASTENING SYSTEM FOR AIRCRAFT STRUCTURES
BEFESTIGUNGSSYSTEM FÜR FLUGZEUGSTRUKTUREN
SYSTÈME DE FIXATION POUR STRUCTURES D'AÉRONEF
02.10.2024
Patent
Elektronische Ressource
Englisch
IPC: | F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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