The invention relates to a propulsion system (7) for a helicopter (1), comprising a linked turbine engine (10) that is able to drive a main rotor (4) intended to be coupled to a rotary wing, characterized in that the propulsion system (7) comprises an electric machine (14) that is able to form an electric motor, said electric machine (14) being coupled directly or indirectly to the main rotor (4).
本发明涉及用于直升机(1)的推进系统(7),其包括具有联动涡轮的涡轮轴发动机(10),所述涡轮轴发动机能够驱动预期联接到旋转机翼的主旋翼(4),其特征在于,所述推进系统(7)包括能够形成电动机的电机(14),所述电机(14)直接或间接联接到所述主旋翼(4)。
PROPULSION SYSTEM FOR HELICOPTER
用于直升机的推进系统
2020-12-08
Patent
Electronic Resource
Chinese
NTIS | 1968
NTIS | 1981