METHOD FOR COOLING A BATTERY AND COOLING SYSTEM
A method for cooling a battery for an electrically powered aircraft, wherein the battery has battery cell(s) and a battery cooling device with a latent heat store. The method includes: A) transferring a first amount of heat from the battery cell to the latent heat store, causing a phase transition in the phase change material, B) removing the battery from the aircraft, C) establishing an operative connection of the battery cooling device to a cooling circuit of a separate second cooling device, D) passing a flow of a coolant through the cooling circuit, E) transferring a second amount of heat from the latent heat store to the coolant, thus causing a phase transition to occur in the phase change material, and F) disconnecting the battery cooling device from the cooling circuit. Step E and/or F are carried out at least partially simultaneously with a charging process of the battery.
1 . A method for cooling a battery ( 3 ) for an electrically powered aircraft ( 1 ), the battery ( 3 ) comprising a battery cell ( 5 ) and a battery cooling device with at least one latent heat store ( 19 ), the method comprising the following steps:
A) transferring a first amount of heat from the battery cell ( 5 ) to the latent heat store ( 19 ), causing a phase transition to occur in the phase change material of the latent heat store ( 19 ),
B) removing the battery ( 3 ) from the aircraft ( 1 ),
C) establishing an operative connection of the battery cooling device to a cooling circuit ( 27 ) of a separate second cooling device ( 26 ),
D) passing a flow of a coolant ( 13 ) through the cooling circuit ( 27 ),
E) transferring a second amount of heat from the latent heat store ( 19 ) to the coolant ( 13 ), causing a phase transition to occur in the phase change material of the latent heat store ( 19 ), and
F) disconnecting the battery cooling device from the cooling circuit ( 27 ),
wherein at least one of step D or step E take place at least partially simultaneously with a charging process of the battery ( 3 ).
2 . The method as claimed in claim 1 , wherein step E takes place after step D, and the operative connection of the battery cooling device to the cooling circuit ( 27 ) is improved by an inflow of the coolant in method step E.
3 . The method as claimed in claim 1 , wherein the cooling circuit ( 27 ) operates according to a counterflow principle.
4 . The method as claimed in claim 1 , wherein after the step C, the method further comprises inserting the battery ( 3 ) into a holder of a ground charging station ( 25 ) which allows simultaneous charging of the battery ( 3 ) and cooling of the latent heat store ( 19 ).
5 . A cooling system ( 6 ) for cooling a battery cell ( 5 ) of an electrically powered aircraft ( 1 ), the cooling system ( 6 ) comprising:
a battery cooling device configured to absorb a first amount of heat at least from the battery cell ( 5 ) during an electrical discharge process, the battery cooling device comprising at least one latent heat store ( 19 ) having a variable aggregate state;
a separate second cooling device ( 26 ) which is thermally coupleable to the battery cooling device and is configured to receive a second amount of heat from the battery cooling device; and
an electrical charging device for the battery cell ( 5 ) for electrically contacting and charging the battery cells ( 5 ) for the charging process of the battery cells ( 5 ).
6 . The cooling system ( 6 ) as claimed in claim 5 , wherein the phase change material of the latent heat store ( 19 ) of the battery cooling device is macroencapsulated in a carrier matrix.
7 . The cooling system ( 6 ) as claimed in claim 5 , wherein the phase change material of the latent heat store ( 19 ) of the battery cooling device comprises at least one of a sleeve around the battery cells, a plate of an at least partial housing around a plurality of battery cells, or at least one perforated plate.
8 . The cooling system ( 6 ) as claimed in claim 5 , wherein the phase change material of the latent heat store ( 19 ) is configure for a temperature range for heat generation of the battery cell ( 5 ) in an operating state in a range of 20° C. to 60° C.
9 . The cooling system ( 6 ) as claimed in claim 5 , further comprising a fire protection material located around the battery cells.
10 . The cooling system ( 6 ) as claimed in claim 5 , wherein the second cooling device ( 26 ) has at least one of a flexible hose ( 9 ) or a cooling plate which is finable with and passed through by a coolant ( 13 ).
11 . The cooling system ( 6 ) as claimed in claim 5 , wherein the second cooling device ( 26 ) is part of a stationary ground charging station ( 25 ) and the ground charging station ( 25 ) comprises an electrical charging device for the battery cell ( 5 ) and is configured to electrically contact the battery cells ( 5 ) for a charging process of the battery cell ( 5 ).
12 . The cooling system ( 6 ) as claimed in claim 5 , wherein the second cooling device ( 26 ) is part of a stationary ground charging station ( 25 ) and the ground charging station ( 25 ) comprises a holder for the battery ( 3 ) and is configured to connect the second cooling device ( 26 ) and the battery cooling device in a thermally conductive manner.
13 . The cooling system ( 6 ) as claimed in claim 5 , wherein the battery ( 3 ) comprises a busbar and the battery cell ( 5 ) is electrically conductively connected to the busbar.
14 . The cooling system ( 6 ) as claimed in claim 13 , wherein the battery cell ( 5 ) is electrically conductively connected to the busbar via at least one wire bond, the battery ( 3 ) comprises at least two battery cells ( 5 ) which are configured as cylindrical round cells ( 5 ) with a negatively polarized end face (N) and with a positively polarized end face (P), and the round cells ( 5 ) are geometrically oriented in a same way and are connected via the wire bond, on a same side of the battery cells.