A battery arrangement (10) for the structural integration of batteries (1) in a vehicle, in particular an aircraft or spacecraft (100), comprises at least one battery (1); and two supporting, multi-layered structural laminates (2), between which the at least one battery (1) is held on both sides via battery holders (3), wherein each multi-layered structural laminate has a cooling plate layer (4) and a current collector layer (5), wherein the at least one battery (1) is coupled electrically to the current collector layer (5).
AIRCRAFT OR SPACECRAFT HAVING A STRUCTURAL COMPONENT WITH A BATTERY ARRANGEMENT INTEGRATED THEREIN
FLUGZEUG ODER RAUMFAHRZEUG AUFWEISEND EIN TRAGENDES BAUTEIL MIT EINER DARIN INTEGRIERTEN BATTERIEANORDNUNG
AÉRONEF OU ASTRONEF COMPORTANT UN ÉLÉMENT PORTEUR AVEC UN AGENCEMENT DE BATTERIE INTÉGRÉ DANS CELUI-CI
2020-12-23
Patent
Electronic Resource
English
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