Battery housing for accommodating battery device with multiple battery cells for an electric aircraft
AssigneeLilium eAircraft GmbH
InventorsDaniel WIEGAND, Benjamin REICHMANN
Life of this patent
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Abstract
The invention is related to a battery housing (10) for accommodating a battery device (20) with multiple battery cells (22) for an electric aircraft (100), comprising at least one inner wall (30) and at least one outer wall (40) forming together a battery volume (50) for holding the multiple battery cells (22), characterised in that the at least one outer wall (40) comprises an outside surface (42) wherein the outside surface (42) has an aerodynamical shape for completing a part of a fuselage (110) of the electric aircraft (100).
Claims18
1-17. (canceled)
A battery housing for accommodating a battery device with multiple battery cells for an electric aircraft, the battery housing comprising:
- at least one inner wall and at least one outer wall forming together a battery volume for holding the multiple battery cells,
- wherein the at least one outer wall comprises an outside surface and wherein the outside surface has an aerodynamical shape for completing a part of a fuselage of the electric aircraft.
A method for mounting a battery housing to an electric aircraft, the battery housing comprising at least one inner wall and at least one outer wall forming together a battery volume for holding multiple battery cells therein, wherein the at least one outer wall comprises an outside surface and wherein the outside surface has an aerodynamical shape for completing a part of a fuselage of the electric aircraft, the method comprising:
- placing multiple battery cells in a battery volume to create a battery device;
- mounting the battery housing to the electric aircraft completing at least a part of a fuselage.
A battery assembly comprising:
- at least one battery housing comprising:
- at least one inner wall and at least one outer wall forming together a battery volume for holding multiple battery cells therein,
- wherein the at least one outer wall comprises an outside surface and wherein the outside surface has an aerodynamical shape for completing a part of a fuselage of an electric aircraft.
Dependencies are inferred from the claim text.