FIELD: aircraft engineering.
SUBSTANCE: proposed system comprises aircraft airfoil outer wing composed of flow-through nacelle. Aircraft airfoil outer wing top and bottom pars support power stage static pressure transducers with electric power generators and air jet with outlet nozzle. Flow-through nacelle inlet opening is provided with airflow controller. Said airflow controller is connected in series with computer and control unit.
EFFECT: higher safety and structural strength of aircraft power system.
1 dwg
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