CROSS CONNECTING DEVICE FOR RETAINING AND DIRECTING AT LEAST ONE AERODYNAMIC BODY WITH RESPECT TO THE MAIN WING OF THE SPMOILET, WING AND AIRCRAFT WITH SUCH A CROSS CONNECTION DEVICE

摘要

1. The wing of the aircraft with the main wing (1) and at least one made with the possibility of adjustment relative to it across its span direction by means of a drive device by an aerodynamic body (2a, 2b, 2c, 2e, 2f; 3a, 3b, B), having: ! - at least two spacers (11, 12) spaced apart from each other in the span of the main wing for guiding the aerodynamic body while adjusting relative to the main wing, which establish the aerodynamic body by means of a swivel (13, 14) so that it allows at least one rotational degree of freedom of the aerodynamic body (2a, 2b, 2c, 2e, 2f; 3a, 3b, B) relative to the main wing with the axis of rotation (13a, 14a), which has a directional component across the direction (S) of size ha aerodynamic body; ! - a transverse connecting device (L) for holding and guiding at least one aerodynamic body when it is adjusted relative to the main wing in the direction (S) of its wingspan, having: an articulating joint (L3), a first connecting element (L1) for connecting the first end of the articulating connection with the main wing or an aircraft part or other aerodynamic body connected to it, and a second connecting element (L2) for connecting the second end of the articulation connection to the aerodynamic body (B), when ohm cross connecting device (L) only has five degrees of freedom and allows adjustment movement of the aerodynamic body relative to the main wing (1) across its direction (S) span. ! 2. The wing according to claim 1, characterized in that at least two attachments