운송 수단, 특히 항공기 또는 우주선(100) 내에 배터리(1)를 구조적으로 통합하기위한 배터리 배치구조(10)는 적어도 하나의 배터리(1); 적어도 하나의 배터리(1)의 양측을 배터리 홀더(3)를 통해 지지하는 두 개의 지지 냉각 플레이트(2); 및 상기 두 개의 냉각 플레이트(2)를 서로 연결하는 복수 개의 커넥팅 로드(4); 를 포함한다.
A battery arrangement (10) for structurally integrating batteries (1) in a vehicle, in particular an aircraft or spacecraft (100), comprises at least one battery (1); two supporting cooling plates (2) between which the at least one battery (1) is held on both sides via battery holders (3); and a plurality of connecting rods (4) which connect the two cooling plates (2) to one another.
Battery arrangement for structurally integrating batteries in a vehicle
운송 수단 내에 배터리를 구조적으로 통합하기 위한 배터리 배치구조
2025-02-12
Patent
Electronic Resource
Korean
IPC: | H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64G Raumfahrt , COSMONAUTICS |
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