A battery holding device for an electrically driven aircraft, including a battery holder for accommodating at least one battery, a connection for establishing electrical contact between the at least one battery and an electrical drive of the aircraft, and a primary securing device for locking the at least one battery in the battery holder. The important factor is that the battery holding device includes at least one secondary securing device for locking the at least one battery in the battery holder, wherein the secondary securing device can be closed and released independently of the primary securing device. The invention also relates to a battery system, to an aircraft and to a corresponding method.
BATTERY HOLDING DEVICE, BATTERY SYSTEM, AIRCRAFT AND METHOD FOR CHANGING A BATTERY FOR AN AIRCRAFT
2021-08-26
Patent
Electronic Resource
English
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 / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
BATTERY HOLDING DEVICE, AND AIRCRAFT HAVING A BATTERY HOLDING DEVICE OF THIS TYPE
European Patent Office | 2019
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