FIELD: engines and pumps.
SUBSTANCE: proposed device comprises airflow baffle, cowl displacing parallel with nacelle lengthwise axis, at least one flap with one end articulated with said cowl and flap drive system. Cowl can displace from closed position to open position. Flap drive system comprises composite lever turning at said cowl. Driving links are articulated with every end of said lever and arranged at the flap and device fixed structure, respectively. Another invention of this set relates to bypass turbojet nacelle equipped with aforesaid device.
EFFECT: invariable cross-section of discharge channel at thrust-reverse device at position of insignificant opening of baffles.
13 cl, 10 dwg
