Emergency power supply device for an aircraft and aircraft provided with such a device

摘要

An emergency power supply device for aircraft, including at least one air intake duct configured to receive a relative airflow during a flight of the aircraft, a turbine arranged in the duct, to be driven by the relative airflow, and at least one device for generating power for the aircraft, the turbine being connected to the power-generating device to produce power for the aircraft at least under flight conditions thereof.