An unmanned aerial vehicle launching and landing system

Details An unmanned aerial vehicle launching and landing system An unmanned aerial vehicle launching and landing system

B - Operations, Transporting

64

F

B64F 1/02 (2006.01) B64F 1/04 (2006.01) B64F 1/08 (2006.01)

Patent

CA 2659678

A system for landing UAV's comprising a slingshot structure (25) that includes a central arm (26) and an axis means (45) installed along the central arm of the structure and wherein it enables the central arm to move around it in addition, the system comprises base means (50) connecting the axis means to a platform (20) at which the system is installable. The system also include a controlled pulling and braking means (55) that connects between lower end of the central arm of the structure and the platform upon which the system is installable and an assembly (35), essentially formed as a substantially "Y" shape part that is installable unto the top end of the central arm of the structure and a stretchable elastic means (30) installed in a stretched manner at a gap formed between the two arms of the assembly and set to connect with a landing UAV(15). At the landing phase, the controlled pulling and braking means of the system, essentially brakes the motion of the central arm of the structure that is propelled to revolve around the system's axis means, from a time that the UAV forms contact with the elastic means and with it propels the structure to move around the axis means.

La présente invention concerne un système pour faire atterrir des UAV comprenant une structure en lance-pierre (25) qui comprend un bras central (26) et un moyen d'axe (45) installé le long du bras central de la structure. Il permet au bras central de se déplacer autour de lui. De plus, le système comprend un moyen de base (50) reliant le moyen d'axe à une plate-forme (20) sur laquelle le système peut être installé. Le système comprend également un moyen de tirage et de freinage commandé (55) qui fait la connexion entre l'extrémité inférieure du bras central de la structure et la plate-forme sur laquelle le système peut être installé et un ensemble (35), essentiellement formé d'une partie sensiblement en forme de Y, pouvant être installée sur l'extrémité supérieure du bras central de la structure et un moyen élastique étirable (30) installé de manière étirée sur un intervalle formé entre les deux bras de l'ensemble et configuré pour se connecter avec un UAV d'atterrissage (15). À la phase d'atterrissage, le moyen de tirage et de freinage commandé du système freine principalement le mouvement du bras central de la structure qui est propulsée pour évoluer autour du moyen d'axe du système, à partir du moment où le UAV prend contact avec le moyen élastique et propulse avec lui la structure pour se déplacer autour du moyen d'axe.

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