Abstract: The present invention relates to a high-performance battery cell (10) for driving an electric aircraft, comprising a plurality of layers (12) stacked one to another to form a cell stack (100; 200; 300; 400), the cell stack (100; 200; 300; 400) comprising at least two electrode layers (102, 104; 202, 204; 302, 304; 402, 404) comprising a cathode layer and an anode layer, and coating layers (120, 122, 124; 220, 222, 224; 320, 322, 324; 420, 422, 424) applied to the electrode layers (102, 104; 202, 204; 302, 304; 402, 404), wherein at least one of the electrode layers (102, 104; 202, 204; 302, 304; 402, 404) and/or at least one of the coating layers (120, 122, 124; 220, 222, 224; 320, 322, 324; 420, 422, 424) comprises at least one degassing channel (16) connecting an inner portion of the cell stack (100; 300; 400) with an edge portion of the cell stack (100; 300; 400), and/or at least one weakened portion (202a,b, 204a,b; 302a,b, 304a,b) pre-defining at least one path of weakness connecting an inner portion of

Abstract: A method of fabricating a pre-lithiated electrode comprises: disposing a Li-PET sheet comprising a layer of lithium metal adjacent to a prefabricated electrode comprising a layer of anode material; contacting a surface of the layer of anode material with a surface of the layer of lithium metal; and calendering the layer of lithium metal and the prefabricated electrode together. The present disclosure further provides a lithium-ion battery cell comprising such pre-lithiated electrode.

Abstract: The present invention relates to an electrode comprising at least one metal foil and at least two layers each comprising at least one lithium ion acceptor.