LAUNCHING AND LANDING SYSTEM OF A VEHICLE? AIR CREW NOT TRIPULATED.

摘要

A system (10) for landing UAVs (15), comprising a catapult structure (25) that includes a central arm (26); and a shaft means (45) installed along said central arm of said structure and in which it makes it possible for said central arm (26) to move around it; and base means (50) connecting said shaft means (45) to a platform (20) in which said system can be installed; and an assembly (35), essentially formed as a substantially Y-shaped part that can be installed on said upper end of said central arm (26) of said structure (25); and an elastic extensible means (30) installed in an extended manner in a separation between the two arms (39, 41) of said assembly (35) and adjusted for connection with a landing UAV (15); characterized in that it further comprises a controlled traction and braking means (55) that connects between the lower end of said central arm (26) of said structure (25) and said platform (20) on which said system can be installed (10); and in which, in said landing phase, said controlled traction and braking means (55) essentially slows down the movement of said central arm (26) of said structure (25) which is propelled to rotate about the axis means of said system (45), from the moment when said UAV (15) makes contact with said elastic means (30) and with which propels said structure (25) to move around said axis means (45).