Authenticated messages between unmanned vehicles
US-2016285864-A1 · Sep 29, 2016 · US
US9950791B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9950791-B2 |
| Application number | US-201615064557-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 8, 2016 |
| Priority date | Mar 8, 2016 |
| Publication date | Apr 24, 2018 |
| Grant date | Apr 24, 2018 |
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Embodiments of the present invention provide an apparatus comprising a body including a cavity for storing one or more packages, and a conveyor belt disposed above a top surface of the body. The belt is shaped to receive one or more packages, and the belt is controllable to rotate a package placed on the belt either from the top surface to the cavity for storage or from the cavity to the top surface for dispatch. A package comprises at least one of a drone and a payload transported by the drone. The apparatus further comprises a landing mechanism for stabilizing a drone landing on the apparatus.
Opening claim text (preview).
What is claimed is: 1. An apparatus, comprising: a body including a cavity for storing one or more packages; a conveyor belt disposed above a top surface of the body, wherein the belt is shaped to receive one or more packages, and the belt is controllable to rotate a package placed on the belt either from the top surface to the cavity for storage or from the cavity to the top surface for dispatch; and a landing mechanism for stabilizing a drone landing on the apparatus; wherein a package comprises at least one of a drone and a payload transported by the drone. 2. The apparatus of claim 1 , wherein the body further includes a recharge unit for re-charging one or more batteries of one or more drones stored in the cavity. 3. The apparatus of claim 1 , wherein the landing mechanism facilitates landing of a drone from above the apparatus. 4. The apparatus of claim 3 , wherein: the landing mechanism comprises one or more retractable shock absorbers for slowing and stabilizing the fall of a drone landing from above the apparatus; and the apparatus provides power to extend and retract the shock absorbers. 5. The apparatus of claim 3 , wherein: the landing mechanism comprises an array of electromagnets for slowing and stabilizing the fall of a drone landing from above the apparatus; and the apparatus provides alternating current to power the array of electromagnets. 6. The apparatus of claim 3 , wherein: the landing mechanism is configured to release blasts of air to slow and stabilize the fall of a drone landing from above the apparatus. 7. The apparatus of claim 1 , wherein the landing mechanism facilitates landing of a drone from below the apparatus. 8. The apparatus of claim 7 , wherein: the landing mechanism comprises a net suspended below the body to envelop and catch a drone in the air. 9. The apparatus of claim 8 , wherein a drone caught by the net is one of the following: a malfunctioning drone that has lost power in air, a drone programmed to power down when positioned within proximity of the apparatus, or a powered drone. 10. The apparatus of claim 1 , wherein the apparatus serves as at least one of the following: a beacon, a landing area, a sheltered storage area, a takeoff area, and a drone recharge facility. 11. The apparatus of claim 1 , wherein the apparatus is mounted to a stationary installation. 12. The apparatus of claim 1 , wherein the apparatus is mobile. 13. The apparatus of claim 12 , wherein the apparatus is mounted to a non-stationary flat-bed ground or water vehicle. 14. The apparatus of claim 12 , wherein the apparatus is mounted to a drone of a first size, the drone is capable of storing and carrying one or more other drones of a second size, and the first size is greater than the second size. 15. The apparatus of claim 1 , wherein the belt comprises one or more mechanical movable arms, the arms controllable to grasp or release a package positioned on the belt. 16. The apparatus of claim 1 , wherein the cavity comprises one or more mechanical movable arms, the arms controllable to grasp or release a package in the cavity. 17. The apparatus of claim 1 , wherein at least one of the belt and the landing mechanism is controllable by a drone landing on the apparatus via an executable flight plan for the drone.
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