Drones and drone systems
Drones with propulsions systems supported in a housing are provided where the orientation of the housing is independent from the orientation of the propulsion system. Drones are provided where a propulsion system is rotatable about a first axis and a second axis that is perpendicular to the first axis, permitting the propulsion system to assume substantially any position with a sphere. Drones are provided where a bladeless inner tube is rotatable about a first axis and a second axis that is perpendicular to the first axis, permitting the inner tube to assume substantially any position within a sphere. Drone systems are provided with connectable unit drones. An unmanned land vehicle is provided having a wheel assembly that is rotatable about a first axis and a second axis that is perpendicular to the first axis, permitting the wheel assembly to assume substantially any position with a sphere.
1. A drone system, comprising:
a plurality of unit drones, each unit drone being connectable to another unit drone such that when the plurality of unit drones are directly or indirectly connected, the plurality of connected unit drones form a remotely controllable unitary body, wherein at least one of the unit drones comprises
a housing;
a ring assembly supported by the housing, the ring assembly comprising a top bearing with a top movable inner portion and a bottom bearing with a bottom movable inner portion and a wall connected with and extending between the top movable inner portion and the bottom movable inner portion;
an external rotator supported by the housing, the external rotator being outside of the ring assembly and having an outer surface mechanically engaged with an outer surface of the wall in the ring assembly, the external rotator configured to drive circumferential rotation of the movable portions of the ring assembly about a first axis; and
the wall of the ring assembly having a pair of openings opposite one another, each opening having an internal rotator therein, the pair of internal rotators directly or indirectly supporting a propulsion system inside the ring assembly, where at least one of the internal rotators is configured to drive rotation of the propulsion system about a second axis perpendicular to the first axis;
wherein, in operation, the housing has an orientation that is independent of an orientation of the propulsion system, and rotation of the ring assembly about the first axis is independent of rotation of the propulsion system about the second axis, permitting the propulsion system to assume substantially any position within a sphere inside the ring assembly.
2. The drone system of claim 1 , wherein the plurality of unit drones comprise a deployment system for connection structure such that, when deployed, the connection structure is connectable with reciprocal connection structure any of a plurality of angles, thereby permitting the unitary body to form non-flat shapes.
3. The drone system of claim 1 , wherein connection structure comprises an electromagnet.
4. The drone system of claim 1 , wherein the deployment system includes an inflatable bladder and inflation mechanism.
5. The drone system of claim 4 , wherein at least a portion of the inflatable bladder system comprises solar skin.
6. The drone system of claim 4 comprising at least one deployed inflated bladder, such that the unitary body requires less energy for operation than would be required in the absence of the deployed inflated bladder.