Post-type apparatus for containing and charging unmanned vertical take-off and landing aircraft and method of containing and charging unmanned vertical take-off and landing aircraft using the same
US-2016347192-A1 · Dec 1, 2016 · US
US10434885B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10434885-B2 |
| Application number | US-201415500291-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 5, 2014 |
| Priority date | Aug 5, 2014 |
| Publication date | Oct 8, 2019 |
| Grant date | Oct 8, 2019 |
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A landing platform for an unmanned aerial vehicle, including a plurality of substantially funnel-shaped centering housings configured to cooperate with a corresponding plurality of projections of the aerial vehicle for reaching a predetermined landing position. The platform can include a mechanism for recharging the battery of the aerial vehicle and/or with an arrangement for serial data transfer.
Opening claim text (preview).
The invention claimed is: 1. A landing platform for an unmanned aerial vehicle, comprising: a plurality of substantially funnel-shaped centering housings configured to cooperate with a corresponding plurality of projections of the unmanned aerial vehicle for reaching a predetermined landing position; a positive electrical contact and a negative electrical contact configured to cooperate with a corresponding positive electrical contact and with a corresponding negative electrical contact in at least one of the projections of the unmanned aerial vehicle for recharging a battery of the aerial vehicle; wherein the electrical contacts of the platform comprise arms configured to embrace a projection of the unmanned aerial vehicle. 2. The landing platform of claim 1 , wherein an axis of the funnel-shaped housings is coaxial with an axis of the projections. 3. The landing platform of claim 1 , wherein the substantially funnel-shaped centering housings comprise a substantially frusto-conical mouth and a tubular portion that extends downwardly from a bottom of the frusto-conical mouth. 4. The landing platform of claim 1 , wherein the arms are staggered so that each arm cooperates with the projection at a different height of the projection. 5. The landing platform of claim 1 , further comprising an arrangement for serial data transfer. 6. The landing platform of claim 1 , wherein a surface of the substantially funnel-shaped centering housings is at least partially of a material that offers reduced friction with the projections. 7. The landing platform of claim 1 , wherein at least a portion of a surface of the substantially funnel-shaped centering housings substantially follows a logarithm curve. 8. The landing platform of claim 1 , further comprising a substantially flat surface, wherein the substantially funnel-shaped centering housings are recessed with respect to the substantially flat surface. 9. The landing platform of claim 8 , wherein at least two of the substantially funnel-shaped centering housings are substantially tangent in proximity of the substantially flat surface. 10. The landing platform of claim 1 , wherein closure of the arms towards the projection is controlled by a pressure sensor. 11. The landing platform of claim 4 , wherein closure of the arms towards the projection is controlled by a pressure sensor. 12. An assembly comprising an unmanned aerial vehicle and a landing platform according to claim 1 . 13. The assembly of claim 12 , wherein the unmanned aerial vehicle is a vertical takeoff unmanned aerial vehicle comprising a plurality of rotors and a plurality of projections, each being in a form of a cylindrical foot, which extend downwardly from a fixed structure of the unmanned aerial vehicle. 14. The assembly of claim 12 , wherein the unmanned aerial vehicle further comprises a plug/socket arrangement to transfer data between the unmanned aerial vehicle and the landing platform. 15. The assembly of claim 13 , wherein the unmanned aerial vehicle further comprises a plug/socket arrangement to transfer data between the unmanned aerial vehicle and the landing platform.
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