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发明授权
CN105691610B 用于直升机的混合动力系统及具有其的直升机 有权

用于直升机的混合动力系统及具有其的直升机
摘要：
本发明公开了一种用于直升机的混合动力系统及具有其的直升机，所述用于直升机的混合动力系统包括发动机、动力电池、ISG电机和尾桨电机，所述ISG电机与所述动力电池电气连接，且与所述发动机机械连接，且所述发动机和所述ISG电机中的至少一个输出的动力适于输出给所述直升机的主旋翼；所述尾桨电机分别与所述动力电池和所述ISG电机电气连接，且所述尾桨电机输出的动力适于输出给所述直升机的尾桨。根据本发明实施例的用于直升机的混合动力系统，控制灵活、安全性能高且节油。
摘要（英）：

The invention discloses a hybrid power system for a helicopter and the helicopter with the same. The hybrid power system for the helicopter comprises a power generator, a power battery, an ISG battery and a tail rotor motor, wherein the ISG battery is electrically connected with the power battery and mechanically connected with the power generator; power output by at least one of the power generator and the ISG motor is suitable for being output to a main rotor of the helicopter; and the tail rotor motor is electrically connected with the power battery and the ISG motor, and power output by the tail rotor motor is suitable for being output to a tail rotor of the helicopter. The hybrid power system for the helicopter is flexible in control and high in security performance, and saves fuel.

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