FIELD: engines and pumps.
SUBSTANCE: invention relates to turbojet nacelle with power supply for drive system and control over thrust reverser and control and drive system of controlled nozzle. It differs from known designs in that power supply allows switching between first position whereat is supplies thrust drive and control system and second position whereat it supplies nozzle drive and control system. Note here that said switching occurs in response to control signal from computer intended for receiving thrust reverser opening command.
EFFECT: power supply for thrust and nozzle drive and control systems.
11 cl, 4 dwg
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