| 摘要 |
The invention relates to an emergency power supply device (3) for an aircraft (1), characterised in that it comprises at least one air intake duct (5) designed to receive a relative airflow V (during the flight of the aircraft), a turbine (25) arranged in said duct (5), to be driven by the relative airflow V, and at least one device (31) for generating power for the aircraft, said turbine (25) being connected to said power-generating device (31) in order to produce power for the aircraft at least under flight conditions thereof. |
