| 摘要 |
FIELD: engines and pumps.SUBSTANCE: proposed control system comprises turbojet thrust reverser, control computer, reverser control device controlled by said computer in response to data fed by transducers into computer via control device, turbojet adjustment device controlled by said computer in response to data fed by transducers into computer via control device. Invention covers also the method of control used in said control system, and aircraft.EFFECT: perfected system.10 cl, 2 dwg |
