Base stations including integrated systems for servicing UAVs
An unmanned aerial vehicle (UAV) is disclosed that includes a power source. The power source includes: one or more power cells; one or more thermal transfer members that are thermally connected to the one or more power cells; and a heat exchanger that is thermally connected to the one or more thermal transfer members such that the one or more thermal transfer members and the heat exchanger facilitate a transfer of thermal energy between the power source and ambient air to decrease or increase temperature of the power source.
1. An unmanned aerial vehicle (UAV) comprising:
a power source including:
one or more power cells;
one or more thermal transfer members thermally connected to the one or more power cells, wherein the one or more power cells and the one or more thermal transfer members correspond in number; and
a heat exchanger thermally connected to the one or more thermal transfer members such that the one or more thermal transfer members extend between the one or more power cells and the heat exchanger, whereby the one or more thermal transfer members and the heat exchanger facilitate a transfer of thermal energy between the power source and ambient air to decrease or increase temperature of the power source.
2. The UAV claim 1 , wherein the one or more thermal transfer members include graphite.
3. The UAV claim 1 , wherein the one or more thermal transfer members are unitary in construction.
4. The UAV of claim 1 , wherein the one or more power cells include a plurality of individual power cells and the one or more thermal transfer members include a plurality of individual thermal transfer members.
5. The UAV of claim 1 , wherein the heat exchanger includes one or more diffusers to increase surface area of the heat exchanger and thermal energy distribution towards or away from the power source.
6. The UAV of claim 5 , wherein the one or more diffusers extend axially and/or laterally along an outer surface of the heat exchanger.
7. The UAV of claim 5 , wherein the one or more diffusers include a plurality of diffusers.
8. The UAV of claim 7 , wherein the plurality of diffusers are configured as fins defining one or more channels therebetween, the one or more channels being configured to direct air flow along the heat exchanger to increase thermal energy distribution towards or away from the power source.
9. An unmanned aerial vehicle (UAV) comprising:
a power source including a heat exchanger configured to transfer thermal energy between the power source and ambient air to decrease or increase temperature of the power source, the heat exchanger including one or more diffusers to increase surface area of the heat exchanger and thermal energy distribution towards or away from the power source, wherein the one or more diffusers extend continuously between opposite ends of the power source.
10. The UAV of claim 9 , wherein the one or more diffusers extend axially and/or laterally along an outer surface of the heat exchanger.
11. The UAV of claim 9 , wherein the one or more diffusers includes a plurality of diffusers.
12. The UAV of claim 11 , wherein the plurality of diffusers are configured as fins defining one or more channels therebetween, the one or more channels being configured to direct air flow along the heat exchanger to increase thermal energy distribution towards or away from the power source.
13. An unmanned aerial vehicle (UAV) comprising:
a body;
one or more antennas extending from the body, the one or more antennas being reconfigurable between an active configuration, in which the one or more antennas extend outwardly from the body, and a passive configuration, in which the one or more antennas are positioned adjacent to the body, wherein the one or more antennas include first ends connected to an exterior surface of the body and second free ends; and
a power source connected to the body, the power source including one or more diffusers extend axially and/or laterally along an outer surface of the power source to transfer thermal energy between the power source and ambient air to decrease or increase temperature of the power source.
14. The UAV of claim 13 , wherein the one or more antennas are biased towards the active configuration.
15. The UAV of claim 13 , wherein the one or more diffusers includes a plurality of diffusers configured as fins defining one or more channels therebetween, the one or more channels being configured to direct air flow along the power source to increase thermal energy distribution towards or away from the power source.
16. The UAV of claim 13 , wherein the power source further includes:
one or more power cells; and
one or more thermal transfer members thermally connected to the one or more power cells and the one or more diffusers.
17. The UAV of claim 16 , wherein the one or more thermal transfer members include graphite.
18. The UAV of claim 16 , wherein the one or more thermal transfer members are unitary in construction.
19. The UAV of claim 6 , wherein the one or more diffusers extend continuously between opposite ends of the power source.
20. The UAV of claim 9 , wherein the power source further includes:
one or more power cells; and
one or more thermal transfer members thermally connected to the one or more power cells, wherein the heat exchanger is thermally connected to the one or more thermal transfer members such that the one or more thermal transfer members extend between the one or more power cells and the heat exchanger.