Stabilized airborne drop delivery
First Claim
1. A method, comprising:
- navigating, by at least one computing device of an Unmanned Aerial Vehicle (UAV), a flight path of the UAV to deliver an item;
positioning, by the at least one computing device, the UAV over a delivery zone to deliver the item;
actuating, by the at least one computing device, a winch mechanism of the UAV to extend at least one tether to deliver the item, the winch mechanism comprising a first winch mechanism secured to the UAV at a first orientation and a second winch mechanism secured to the UAV at a second orientation; and
monitoring, by the at least one computing device, at least one of a height of the UAV or the item above a landing surface within the delivery zone, wherein;
the at least one tether comprises a first tether of the first winch mechanism and a second tether of the second winch mechanism;
the first tether flexes in a first direction and resists flexing in a second direction; and
the second tether flexes in the second direction and resists flexing in the first direction.
1 Assignment
0 Petitions
Accused Products
Abstract
Stabilized delivery using an Unmanned Aerial Vehicle (UAV) is described. In one embodiment, the UAV includes a flight controller configured to control a flight path of the UAV, a winch mechanism secured to an underside of the UAV, a platform tethered to and extendable from the winch mechanism, and a ballast system configured to stabilize the platform. The winch mechanism may be relied upon to drop an item for delivery without landing the UAV. The winch mechanism can include a first winch mechanism secured to the UAV at a first orientation and a second winch mechanism secured to the UAV at a second orientation. Because the winch mechanism may give rise to certain design and operating considerations, various active and passive flight and/or ballast control systems are described. These systems maintain an orientation of the UAV, the platform, and/or the item during one or more stages of airborne drop delivery.
20 Citations
17 Claims
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1. A method, comprising:
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navigating, by at least one computing device of an Unmanned Aerial Vehicle (UAV), a flight path of the UAV to deliver an item; positioning, by the at least one computing device, the UAV over a delivery zone to deliver the item; actuating, by the at least one computing device, a winch mechanism of the UAV to extend at least one tether to deliver the item, the winch mechanism comprising a first winch mechanism secured to the UAV at a first orientation and a second winch mechanism secured to the UAV at a second orientation; and monitoring, by the at least one computing device, at least one of a height of the UAV or the item above a landing surface within the delivery zone, wherein; the at least one tether comprises a first tether of the first winch mechanism and a second tether of the second winch mechanism; the first tether flexes in a first direction and resists flexing in a second direction; and the second tether flexes in the second direction and resists flexing in the first direction. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8)
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9. A method, comprising:
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navigating, by at least one computing device of an Unmanned Aerial Vehicle (UAV), the UAV over a delivery zone to deliver an item; and actuating, by the at least one computing device, a winch mechanism of the UAV to extend at least one tether to deliver the item, the winch mechanism comprising at least two winch mechanisms secured to the UAV at different locations and orientations, wherein; the at least one tether comprises a first tether and a second tether; the first tether flexes in a first direction and resists flexing in a second direction; and the second tether flexes in the second direction and resists flexing in the first direction. - View Dependent Claims (10, 11, 12, 13, 14)
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15. A method, comprising:
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navigating, by at least one computing device of an Unmanned Aerial Vehicle (UAV), the UAV over a delivery zone; and actuating, by the at least one computing device, a winch mechanism of the UAV to extend at least one tether, wherein; the winch mechanism comprises a first winch mechanism and a second winch mechanism; and the first winch mechanism is secured to the UAV at a first orientation and the second winch mechanism is secured to the UAV at a second orientation different than the first orientation, wherein; the at least one tether comprises a first tether and a second tether; the first tether flexes in a first direction and resists flexing in a second direction; and the second tether flexes in the second direction and resists flexing in the first direction. - View Dependent Claims (16, 17)
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Specification