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Application filed by Юрій Леонідович Сидорюк, Юрий Леонидович СидорюкfiledCriticalЮрій Леонідович Сидорюк
Priority to UA94063148ApriorityCriticalpatent/UA19475A/en
Publication of UA19475ApublicationCriticalpatent/UA19475A/en
The invention relates to the field of aeronautics. A disk flying vehicle contains a shell from gas-impermeable cloth, a nacelle and a steering rudder. It consists of an internal pneumatic body, on which the inner shell is stretched which contains a compensator of aerostatic pressure and is stretched over by the external pneumatic body, which contains control devices of aerostatic lift and stretched over by the outer shell, which has the form of a horizontally located wing in the form of a disk.
The required damping and control process quality in a fuel pressure regulator(Trebuemoe dempfirovanie i kachestvo protsessa regulirovaniia v reguliatore davleniia topliva)