FIELD: engines.
SUBSTANCE: invention relates to a system for the electrical energy generating for the aircraft. System (20) comprises a fairing (21) comprising at least one turbine (22) located in the fairing (21) front part (21a), and the electric power generator (23) connected to said turbine. Fairing (21) front portion (21a) is provided with the air inlet means (26) which are movable between the open position, in which the turbine (22) is subject to a flow of air outside the fairing (21), and a closed position in which the turbine (22) is concealed inside the fairing (21).
EFFECT: invention serves to reduce aerodynamic drag and increases the possibility of the kinetic and potential energies recovery.
12 cl, 7 dwg
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