Battery module for electrically-driven aircraft

1. A battery module comprising:

a plurality of cell tubes configured to accommodate a plurality of battery cells within the plurality of cell tubes so that individual of the plurality of battery cells are positioned within individual of the plurality of cell tubes;

a first conductive plate comprising a plurality of first holes and configured to electrically connect first terminals of the plurality of battery cells; and

a plurality of first spacers mounted in the plurality of first holes and configured to support the plurality of cell tubes and the plurality of battery cells with respect to the first conductive plate, the plurality of first spacers comprising ceramic or glass fiber and being configured to provide thermal and electrical isolation between the plurality of battery cells and the first conductive plate,

wherein one of the plurality of first spacers is ring-shaped and comprises a first side and a second side opposite the first side, and the first side has an inner edge and the second side has an outer edge, the inner edge circumferentially surrounding and supporting part of one of the plurality of cell tubes, the outer edge being positioned in one of the plurality of first holes to support the first conductive plate.

2. The battery module of claim 1 , further comprising:

a second conductive plate comprising a plurality of second holes and configured to electrically connect second terminals of the plurality of battery cells opposite the first terminals; and

a plurality of second spacers mounted in the plurality of second holes and configured to support the plurality of cell tubes and the plurality of battery cells with respect to the second conductive plate, the plurality of second spacers comprising ceramic or glass fiber and being configured to provide thermal and electrical isolation between the plurality of battery cells and the second conductive plate.

3. The battery module of claim 1 , wherein the plurality of first spacers comprise ceramic.

4. The battery module of claim 1 , wherein the plurality of first spacers are configured to support the plurality of battery cells and the plurality of cell tubes so that the plurality of battery cells, the plurality of cell tubes, and the first conductive plate do not directly contact each other, the plurality of battery cells being removable from the plurality of cell tubes.

5. The battery module of claim 1 , wherein the plurality of first spacers are configured to support the plurality of battery cells and the plurality of cell tubes so that the plurality of battery cells, the plurality of cell tubes, and the first conductive plate do not directly contact each other, the plurality of battery cells being removable from the plurality of cell tubes.

6. The battery module of claim 5 , wherein the plurality of first spacers comprise ceramic, plastic, or glass fiber.

7. The battery module of claim 1 , wherein the plurality of first holes are configured to permit combustion components from the plurality of battery cells to pass through the first conductive plate.

8. The battery module of claim 7 , further comprising a housing configured to support the first conductive plate, the housing comprising a plurality of second holes facing the plurality of first holes, the plurality of second holes being configured to permit the combustion components to pass through the housing.

9. The battery module of claim 8 , further comprising tape or a cover that is attached to the housing and covering the plurality of second holes, the tape or the cover being configured to release from the housing responsive to a pressure within one of the plurality of cell tubes increasing from an explosion of one of the plurality of battery cells.

10. The battery module of claim 8 , wherein the plurality of second holes is configured to direct an air flow through the housing between plurality of cell tubes but not within the plurality of cell tubes.

11. The battery module of claim 1 , wherein the plurality of cell tubes comprises a surface treatment that is electrically isolating.

12. The battery module of claim 1 , wherein the first conductive plate comprises a printed circuit board, the printed circuit board comprising a sensor configured to monitor a voltage, a current, a temperature, or an internal pressure of at least one of the plurality of battery cells.

13. The battery module of claim 12 , further comprising:

a circuit board assembly electrically connected to the printed circuit board; and

a controller mounted on the circuit board assembly and configured to control the plurality of battery cells.

14. The battery module of claim 1 , wherein the plurality of cell tubes are configured to accommodate a total of between 4 battery cells and 32 battery cells, inclusive.

15. The battery module of claim 1 , in combination with an exhaust channel, the plurality of first spacers being configured to support the plurality of cell tubes to divert a fire from one of the plurality of battery cells toward the exhaust channel to prevent the fire from spreading to another of the plurality of battery cells.

16. The battery module of claim 15 , in combination with an inlet channel configured to direct an air flow to and around the plurality of cell tubes and into the exhaust channel.

17. The battery module of claim 1 , wherein the plurality of cell tubes comprises aluminum, steel, or carbon.

18. The battery module of claim 1 , wherein the plurality of cell tubes are arranged in at least two rows of cell tubes and at least two columns of cell tubes.

19. A vehicle housing supporting the battery module of claim 1 so that an air flow passes by the plurality of cell tubes when the vehicle housing is in motion, the vehicle housing being configured to fly.

20. The battery module of claim 1 , wherein the plurality of first spacers comprise glass fiber.