The invention relates to an electric or hybrid propulsion aircraft comprising an electrical device comprising at least a first electrical network (32) and at least a second electrical network (34) operating at a higher voltage than the first electrical network (32). The second electrical network (34) comprises at least one electrical energy distribution system (44); at least one reversible electric motor (36) for propelling the aircraft, directly or indirectly connected to the electrical energy distribution system (44); at least one reversible power system (38) directly or indirectly connected to the electrical energy distribution system (44); a safety box (52.1) positioned as close as possible to each motor (36) and each reversible power system (38).
本发明涉及一种包括电力装置的电力或混合动力推进飞行器,该电力装置至少包括第一电网(32)以及至少第二电网(34),该第二电网在高于第一电网(32)的电压下运行。该第二电网(34)包括至少一个电能分配系统(44);至少一个可逆电动机(36),其用于推进飞行器,其直接或间接地连接到电能分配系统(44);至少一个可逆电力系统(38),其直接或间接地连接到电能分配系统(44);安全盒(52.1),其定位为尽可能靠近每个电动机(36)和每个可逆电力系统(38)。
Electric or hybrid propulsion aircraft comprising suitable electrical device
包括适当电力装置的电力或混合动力推进飞行器
2022-06-21
Patent
Electronic Resource
Chinese
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