Base stations for unmanned aerial vehicles (UAVs)
A base station for an unmanned aerial vehicle (UAV) is disclosed that includes: an enclosure defining an internal cavity that is configured to receive the UAV; a door that is movably connected to the enclosure; actuators that extend between the door and the enclosure to facilitate opening and closure of the door; a cradle that is configured to receive the UAV and which is movable in relation to the enclosure such that the cradle is repositionable between a retracted position and an extended position to facilitate movement of the UAV into and out of the enclosure; and engagement members that are secured to the actuators and which are configured for contact with propeller assemblies on the UAV to facilitate folding of the propeller assemblies during movement of the UAV into the enclosure.
1. A base station for an unmanned aerial vehicle (UAV), the base station comprising:
an enclosure defining an internal cavity configured to receive the UAV;
a door movably connected to the enclosure;
actuators extending between the door and the enclosure to facilitate opening and closure of the door;
a cradle configured to receive the UAV, the cradle being movable in relation to the enclosure such that the cradle is repositionable between a retracted position and an extended position to facilitate movement of the UAV into and out of the enclosure; and
engagement members secured to the actuators and configured for contact with propeller assemblies on the UAV to facilitate folding of the propeller assemblies during movement of the UAV into the enclosure.
2. The base station of claim 1 , wherein the engagement members include a compliant material to inhibit unseating of the UAV from the cradle upon contact between the engagement members and the propeller assemblies.
3. The base station of claim 1 , wherein the engagement members include mounting brackets configured for connection to the actuators.
4. The base station of claim 1 , wherein the actuators include:
a first actuator; and
a second actuator spaced laterally from the first actuator along a width of the enclosure.
5. The base station of claim 4 , wherein the engagement members include:
a first engagement member connected to the first actuator; and
a second engagement member connected to the second actuator such that the second engagement member is spaced laterally from the first engagement member along the width of the enclosure.
6. A method of docking an unmanned aerial vehicle (UAV) within a base station, the method comprising:
opening a door of the base station;
performing a first stage retraction of the UAV into the base station;
partially folding rear propeller assemblies on the UAV via rotation of the rear propeller assemblies into contact with engagement members on the base station;
performing a second stage retraction of the UAV into the base station;
completely folding the rear propeller assemblies via rotation of the rear propeller assemblies into contact with the engagement members;
performing a third stage retraction of the UAV into the base station;
partially folding front propeller assemblies on the UAV via rotation of the front propeller assemblies into contact with the engagement members; and
completely folding the front propeller assemblies.
7. The method of claim 6 , wherein performing the second stage retraction of the UAV includes folding an antenna on the UAV via contact with the door.
8. The method of claim 6 , wherein partially folding the rear propeller assemblies includes:
rotating a first rear propeller assembly in a first direction; and
rotating a second rear propeller assembly in a second direction opposite to the first direction.
9. The method of claim 8 , wherein completely folding the rear propeller assemblies includes:
rotating the first rear propeller assembly in the second direction; and
rotating the second rear propeller assembly in the first direction.
10. The method of claim 9 , wherein completely folding the rear propeller assemblies includes positioning the rear propeller assemblies such that they are oriented towards the front propeller assemblies.
11. The method of claim 10 , further including partially closing the door to facilitate contact between the engagement members and the front propeller assemblies.
12. The method of claim 11 , wherein partially folding the front propeller assemblies includes:
actively rotating a first front propeller assembly in the second direction; and
actively rotating a second front propeller assembly in the first direction.
13. The method of claim 12 , wherein partially folding the front propeller assemblies further includes:
passively rotating the first front propeller assembly in the first direction; and
passively rotating the second front propeller assembly in the second direction, wherein passively rotating the first front propeller assembly and passively rotating the second front propeller assembly includes performing a fourth stage retraction of the UAV into the base station.
14. The method of claim 13 , wherein partially folding the front propeller assemblies includes positioning the front propeller assemblies such that they are oriented away from the rear propeller assemblies.
15. The method of claim 14 , wherein completely folding the front propeller assemblies includes:
rotating the first front propeller assembly in the first direction; and
rotating the second front propeller assembly in the second direction.
16. The method of claim 15 , wherein completely folding the front propeller assemblies includes actively rotating the front propeller assemblies such that they are oriented towards the rear propeller assemblies.
17. A method of docking an unmanned aerial vehicle (UAV) within a base station including a landing surface and a door assembly movable in relation to the landing surface, the method comprising:
folding rear propeller assemblies on the UAV via rotation of the rear propeller assemblies into contact with engagement members supported by the door assembly of the base station;
retracting the UAV into the base station; and
folding front propeller assemblies on the UAV via rotation of the front propeller assemblies into contact with the engagement members.
18. The method of claim 17 , further including adjusting a position of the door assembly to facilitate contact between the engagement members and the rear propeller assemblies and contact between the engagement members and the front propeller assemblies.
19. The method of claim 17 , wherein folding the rear propeller assemblies and folding the front propeller assemblies includes rotating the rear propeller assemblies and rotating the front propeller assemblies into bumpers supported by actuators for the door assembly.
20. The method of claim 17 , wherein folding the rear propeller assemblies and folding the front propeller assemblies includes rotating the rear propeller assemblies and rotating the front propeller assemblies into bumpers supported by a door of the door assembly.