Battery with liquid temperature controlling system

1. A system comprising:

a plurality of batteries including a first battery and a second battery;

a support structure coupled to the plurality of batteries, the support structure including:

a first seal provided on a first surface of the support structure around the first battery; and

a second seal provided on a second surface opposite to the first surface of the support structure around the second battery,

an opening for receiving a portion of the first battery and a portion of the second battery, wherein the opening extends between the first seal and the second seal;

a channel formed within the opening between the portion of the first battery and the portion of the second battery;

an inlet provided on a top surface of the support structure adapted to receive a fluid;

an outlet provided on a bottom surface of the support structure adapted to receive the fluid after the fluid travels through the channel in direction of gravity, wherein the channel extends between the inlet and the outlet.

2. The system of claim 1 , wherein the first seal or the second seal includes an o-ring.

3. The system of claim 1 , wherein the support structure includes a plurality of channels, such that a respective channel is formed between each pair of adjacent batteries among the plurality of batteries.

4. The system of claim 1 , wherein the plurality of batteries include a first set of batteries and a second set of batteries that extend parallel to the first set of batteries along a horizontal plane, the first set of batteries including the first battery, the second set of batteries including the second battery.

5. The system of claim 1 , wherein the system is coupled to a battery-powered aircraft, the system further comprising:

a liquid temperature controlling system coupled to the battery-powered aircraft when the battery-powered aircraft is on ground, wherein the liquid temperature controlling system is configured to:

detachably couple the support structure and the plurality of batteries to the liquid temperature controlling system;

circulate a temperature controlled liquid as the fluid through the channel to produce a plurality of temperature controlled batteries, wherein the temperature controlled fluid comes into direct contact with the plurality of batteries;

remove the temperature controlled liquid from the plurality of temperature controlled batteries; and

decouple the plurality of temperature controlled batteries and the liquid temperature controlling system.

6. The system of claim 5 , wherein removing the temperature controlled liquid from the plurality of temperature controlled batteries includes blowing air from the liquid temperature controlling system to the plurality of batteries.

7. The system of claim 5 , wherein removing the temperature controlled liquid from the plurality of temperature controlled batteries includes using gravity to drain the temperature controlled liquid from the plurality of temperature controlled batteries.

8. The system of claim 1 , the system is coupled to a battery-powered aircraft, and wherein the fluid traveling through the channel in the direction of the gravity is air while the battery-powered aircraft is on the air.

9. A method comprising:

providing a system including a plurality of batteries coupled to a support structure in a battery-powered aircraft, wherein the support structure includes:

a first seal provided on a first surface of the support structure around a first battery; and

a second seal provided on a second surface opposite to the first surface of the support structure around a second battery,

an opening for receiving a portion of the first battery and a portion of the second battery, wherein the opening extends between the first seal and the second seal;

a channel formed within the opening between the portion of the first battery and the portion of the second battery;

an inlet provided on a top surface of the support structure adapted to receive a fluid;

an outlet provided on a bottom surface of the support structure adapted to receive the fluid after the fluid travels through the channel in direction of gravity, wherein the channel extends between the inlet and the outlet;

detachably coupling the support structure and the plurality of batteries to a liquid temperature controlling system;

circulating a temperature controlled liquid through the channel of the support structure to produce a plurality of temperature controlled batteries, wherein the temperature controlled fluid comes into direct contact with the plurality of batteries;

removing the temperature controlled liquid from the plurality of temperature controlled batteries; and

decoupling the plurality of temperature controlled batteries and the liquid temperature controlling system.

10. The method of claim 9 , wherein removing the temperature controlled liquid from the plurality of temperature controlled batteries includes:

blowing air from the liquid temperature controlling system to the plurality of batteries.

11. The method of claim 9 , wherein removing the temperature controlled liquid from the plurality of temperature controlled batteries includes:

using gravity to drain the temperature controlled liquid from the plurality of temperature controlled batteries.

12. The method of claim 9 , wherein the first seal or the second seal includes an o-ring.

13. The method of claim 9 , wherein the support structure includes a plurality of channels, such that a respective channel is formed between each pair of adjacent batteries among the plurality of batteries.

14. The method of claim 9 , wherein the plurality of batteries include a first set of batteries and a second set of batteries that extend parallel to the first set of batteries along a horizontal plane, the first set of batteries including the first battery, the second set of batteries including the second battery.