| 摘要 |
FIELD: transport.SUBSTANCE: invention relates to aircraft engineering, particularly, to turbojet nacelle moving cowl drive and control system. Proposed system comprises cowl electrically driven lock 4 and cowl actuator 2. Besides, this system comprises centralised electronic control unit 15 to control operation of locking means and actuator in preset operating order. Also, invention relates to nacelle including detachable air intake structure with abode described drive system.EFFECT: higher reliability.9 cl, 1 dwg |
