| 摘要 |
FIELD: aviation. ^ SUBSTANCE: airplane includes two systems of general-airplane equipment control. The first system of general-airplane equipment control has two circuits of automatic control, which are structurally shaped into main and reserve units for transformations and calculations and connected to actuating devices via control and monitoring unit. Circuit of manual control is arranged with control panels, light indicator panels and central light indicator. Control system is coupled along multiplex channel to BCVM complex, electronic systems of engines control, system for registration and control, homing and landing equipment, complex control system. The second control system consists of independent and pilot-uncontrolled emergency automatic circuit. This is the third automatic circuit, which includes independent duplicating system of general-airplane equipment that consists of independent duplicating emergency system of registration and control over operation of all systems and units of airplane. ^ EFFECT: invention is aimed at increased safety of passengers in any emergency situations, also including those where human factor (pilot error) is the reason of plane crash. ^ 2 cl, 3 dwg |
