Payload delivery and drop device for unmanned aerial vehicle for automatic release upon surface contact
Embodiments of a payload delivery and drop device for an unmanned aerial vehicle, and method of its use are described. An apparatus includes a moveable collar defining a lumen having a centerline, and a rigid bar that has a first portion and a second portion. The first portion of the rigid bar has a centerline and the second portion of the rigid bar has a centerline. The second portion of the rigid bar is disposed within the lumen of the collar when the rigid bar is in a first position. The centerline of the first portion of the rigid bar is substantially non-parallel to the centerline of the lumen of the moveable collar when the rigid bar is in the first position. The centerline of the second portion of the rigid bar is substantially non-parallel to the centerline of the lumen when the rigid bar is in the second position.
1. An apparatus, comprising:
an aerial vehicle; and
a payload release device coupled to an underside of the aerial vehicle, the payload release device having a first configuration and a second configuration,
while the aerial vehicle is in flight and the payload release device is in the first configuration, the payload release device configured to at least partially retain a payload,
the payload release device configured to move from the first configuration to the second configuration in response to the payload release device being lowered into contact with an external surface,
while the payload release device is in the second configuration, the payload release device configured to not retain the payload,
the payload release device includes a plurality of elongate members that collectively define, at least in part, a volume within which a payload is retained when the payload release device is in the first configuration,
each elongate member from the plurality of elongate members including a collar and a rigid bar, the rigid bar of each elongate member from the plurality of elongate members configured to limit downward movement of the payload within the volume when the payload release device is in the first configuration,
the rigid bar of each elongate member from the plurality of elongate members configured to not limit downward movement of the payload within the volume when the payload release device is in the second configuration.
2. The apparatus of claim 1 , wherein:
the plurality of elongate members configured to limit a range of motion of the payload while retained within the volume.
3. The apparatus of claim 1 , wherein the payload release device is configured to retain the payload within the volume without a tether when the payload release device is in the first configuration.
4. An apparatus, comprising:
a payload release device configured to be coupled to an underside of an aerial vehicle, the payload release device having a plurality of members collectively defining at least in part a volume within which a payload is at least partially retained when the payload release device is in a first position,
the payload release device having a range of motion between the first position in which the payload is at least partially retained and a second position in which the payload is not retained,
the payload release device configured to move from the first position to the second position in response to at least a portion of the payload release device contacting an external surface during lowering of the payload release device,
each elongate member from the plurality of members including a collar and a rigid bar, the rigid bar of each elongate member from the plurality of members configured to limit downward movement of the payload within the volume when the payload release device is in the first position,
the rigid bar of each elongate member from the plurality of members configured to not limit downward movement of the payload within the volume when the payload release device is in the second position.
5. The apparatus of claim 4 , wherein:
the plurality of members is configured to moveably retain the payload within the volume when the payload release device is in the first position,
the plurality of members configured to limit a range of motion of the payload while retained within the volume.
6. The apparatus of claim 4 , wherein the payload release device is configured to retain the payload within the volume without a tether when the payload release device is in the first position.
7. A method, comprising:
retaining a payload at a payload release device while an aerial vehicle is in flight and the payload release device is in a first configuration, the payload release device coupled to an underside of the aerial vehicle, the payload release device including a plurality of elongate members that collectively define, at least in part, a volume within which a payload is retained when the payload release device is in the first configuration, each elongate member from the plurality of elongate members including a collar and a rigid bar, the rigid bar of each elongate member from the plurality of elongate members configured to limit downward movement of the payload within the volume when the payload release device is in the first configuration;
moving the payload release device from the first configuration to a second configuration in response to the payload release device being lowered into contact with an external surface; and
not retaining the payload to the payload release device while the payload release device is in the second configuration, the rigid bar of each elongate member from the plurality of elongate members configured to not limit downward movement of the payload within the volume when the payload release device is in the second configuration.
8. The method of claim 7 , wherein:
the plurality of elongate members configured to limit a range of motion of the payload while retained within the volume.
9. The method of claim 7 , wherein the payload release device is configured to retain the payload within the volume without a tether when the payload release device is in the first configuration.
10. The method of claim 7 , wherein the payload release device includes:
a hub configured to be coupled to the aerial vehicle;
a plurality of radially extending arms extended from the hub; and
a plurality of elongate, rigid tubes coupled to the plurality of radially extending arms such that the plurality of elongate, rigid tubes is non-parallel to the plurality of radially extending arms;
the plurality of radially extending arms, the plurality of elongate, rigid tubes, and the plurality of elongate members collectively define, in part, the volume within which the payload is received when the payload release device is in the first configuration.
11. The method of claim 10 , wherein at least one of a radially extending arm from the plurality of radially extending arms or an elongate, rigid tube from the plurality of elongate, rigid tubes has an adjustable length.