A connecting assembly for connecting two structures of an aircraft, the connecting assembly including a central element featuring a through-hole, preferably a bore, configured to make a connection with one of the two structures by virtue of a fastener element including a shank inserted into the through-hole. The connecting assembly further includes a plurality of shock-absorbing elements made from a deformable material. Each of the shock-absorbing elements are, on the one hand, secured to the central element and, on the other hand, configured to bear against a surface of the other of the two structures. An aircraft part includes such a connecting assembly.
ENSEMBLE DE LIAISON ENTRE DEUX STRUCTURES D'UN AERONEF, PARTIE D'AERONEF COMPRENANT UN TEL ENSEMBLE, ET AERONEF
ASSEMBLY FOR CONNECTION BETWEEN TWO STRUCTURES OF AN AIRCRAFT, PART OF AN AIRCRAFT COMPRISING SUCH AN ASSEMBLY, AND AIRCRAFT
ANORDNUNG ZUR VERBINDUNG VON ZWEI STRUKTUREN EINES LUFTFAHRZEUGS, LUFTFAHRZEUGTEIL MIT EINER SOLCHEN ANORDNUNG UND LUFTFAHRZEUG
2024-07-17
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge / 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 / F16C SHAFTS , Wellen |
European Patent Office | 2022
|ENSEMBLE D'AERONEF COMPRENANT UN ELEMENT D'ACCROCHAGE D'UN MOTEUR ET AERONEF ASSOCIE
European Patent Office | 2016
|European Patent Office | 2021
|European Patent Office | 2024
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