AIRCRAFT POWER SUPPLY SYSTEM

摘要

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