An aircraft propulsion module comprising: a hydrogen storage system (9); at least one electrochemical converter (7) connected to the hydrogen storage system wherein the at least one electrochemical converter is adapted to convert hydrogen supplied from the hydrogen storage system into electrical energy; and at least one electric motor (5) electrically connected to the at least one electrochemical transducer, where the electric motor is adapted to generate thrust; wherein the propulsion module comprises a first part (1) and a second part (2), each of the first and second parts comprising a respective fairing (4, 10); the first part and the second part can be separated from each other; the first part comprises at least one electrochemical converter and at least one electric motor; and the second part comprises a hydrogen storage housing of the hydrogen storage system for storing a reusable hydrogen storage unit. An aircraft comprising at least one such aircraft propulsion module.
一种飞行器推进模块,该飞行器推进模块包括:氢储存系统(9);至少一个电化学转换器(7),至少一个电化学转换器连接至氢储存系统,其中,至少一个电化学转换器适于将从氢储存系统供应的氢转换成电能;以及至少一个电动马达(5),至少一个电动马达电连接至所述至少一个电化学转换器,其中,电动马达适于产生推力;其中,推进模块包括第一部分(1)和第二部分(2),第一部分和第二部分中的每一者包括相应的整流罩(4、10);第一部分和第二部分能够彼此分离;第一部分包括至少一个电化学转换器和至少一个电动马达;并且第二部分包括氢储存系统的氢储存壳体,以用于储存可重复使用的氢储存单元。一种飞行器,该飞行器包括至少一个这样的飞行器推进模块。
Aircraft propulsion module and aircraft
飞行器推进模块以及飞行器
2023-10-10
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |