公开(公告)号：EP4420975A1

公开(公告)日：2024-08-28

申请号：EP23382173.5

申请日：2023-02-24

申请人： Airbus Operations, S.L.U.

发明人： JARA RODELGO, Álvaro ,  GONZÁLEZ ANTOHI, Miguel ,  GUTIÉRREZ ARCONADA, Roberto

IPC分类号： B64C3/44 ,  B64C3/54 ,  B64C9/04 ,  B64C5/00

CPC分类号： B64C3/44 ,  B64C2003/44520130101 ,  B64C9/04 ,  B64C5/00 ,  B64C3/54 ,  B64C2003/54320130101

摘要： The invention provides a drive mechanism, a drive system and an aerodynamic structure for an aircraft, each comprising at least one articulated module (1A) comprising four links (10A, 20A, 30A, 40A), wherein each link comprises three coupling points (Ai, Bi, Ci, i=1..4) distributed forming a triangular geometry, wherein the links are coupled to each other such that an articulation with only one degree of freedom is provided.