| 摘要 |
FIELD: aviation technique. ^ SUBSTANCE: control system has hydraulic drives of the steering surfaces of a flying vehicle, a hydraulic system with drain and pressure pipes and also the pressure part of a fuel system, as it the subsystem of an active fuel of the flying vehicle's fuel system is used. At that the pressure part of the fuel system is connected with the suction main of hydraulic system through a cutoff valve. The slide of the cutoff valve is spring loaded from one side and is connected with the pressure pipe of the hydraulic system from the other side and further through the slide valve executed on one axis with a piston of the hydraulic system's tank with the suction main of the hydraulic system. ^ EFFECT: proposed control system is characterized with increased vitality and reliability because at rising leaky sites in the hydraulic system it remains capable of working due to feeding fuel as working liquid to the aggregates-consumers of the hydraulic system. ^ 2 cl, 1dwg |
