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.
Connecting assembly for connecting two aircraft structures, aircraft part comprising such assembly, and aircraft
2022-10-20
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2022
|Europäisches Patentamt | 2022
|WING FOR AN AIRCRAFT, AIRCRAFT, AND CONNECTING ASSEMBLY
Europäisches Patentamt | 2022
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