| 摘要 |
The present disclosure is related to a retractable and slidable system, which form the flaps or empennage of an aircraft. This invention thus allows lowering/raising the empennage of an aircraft. The empennage design enables it to conduct the fluid flow through the flaps. The present design has the ability to increase the displacement efficiency of the fluids through the aircraft in which it is displaced; the system consists of a mechanism which has a structure system which when actuated as a whole, allows raising or lowering an aerodynamic profile. The flap system can slide into the keel, or camber line, in such a way that, following the aerodynamic profile, can be actuated to be only contracted in that direction. |
