The invention relates to an auxiliary generator system for an aircraft. More specifically, the present invention relates to an auxiliary power system with a new architecture comprising a basic auxiliary power unit (APU) having a fully dual redundant starter and a power generation system that can be independently connected to a normal electrical network or an emergency electrical network of an aircraft. In addition, the invention also relates to an aircraft comprising the auxiliary power system and a method for supplying electric power to the aircraft through the system.
本发明涉及用于飞行器的辅助发电机系统。更具体地,本发明涉及一种具有新架构的辅助动力系统,该辅助动力系统包括基本辅助动力单元(APU),该基本辅助动力单元具有完全双冗余起动器和可以独立地连接至飞行器的正常电网络或应急电网络的发电系统。另外,本发明还涉及一种包括所述辅助动力系统的飞行器以及一种通过所述系统向飞行器供应电力的方法。
Auxiliary power system
辅助动力系统
14.06.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |