The invention relates to a hydrogen storage system and an aircraft including the same. The hydrogen storage system (10) comprises a hydrogen tank (12) and a system for controlling evaporation of hydrogen in the hydrogen tank. The control system comprises: a hydrogen discharge pipe (18) connected on the one hand to the hydrogen tank and on the other hand to a controllable valve (22); and a processing unit (16) configured to control the valve as a function of the pressure in the tank. The hydrogen storage system (10) further comprises a fuel cell (14) permanently connected to the hydrogen tank, and the processing unit is powered by the fuel cell.
本公开涉及储氢系统和包括储氢系统的飞行器。储氢系统(10)包括氢罐(12)和用于控制所述氢罐内氢蒸发的系统。该控制系统包括:氢排放管(18),所述氢排放管一方面连接到所述氢罐并且另一方面连接到可控阀(22);以及处理单元(16),所述处理单元被配置成根据所述罐中的压力来控制所述阀。所述储氢系统(10)进一步包括燃料电池(14),所述燃料电池永久连接到所述氢罐,并且所述处理单元由所述燃料电池供电。
Hydrogen storage system and aircraft comprising hydrogen storage system
储氢系统和包括储氢系统的飞行器
2022-10-11
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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