Hovercraft tilting dynamic stabilizer system

摘要

the stabilizer consists of two separate air channels (2, 3), connecting the collector fan (1) with two flexible chambers located on the right and the left side of the hull, the separation valve (4), placed at the inlet of the air ducts (2, 3) and procedures zmu control valve.who provides the mechanism inertia (5) provided with a damping spru0119u017cynuju0105co - (6) and active element susceptible to tip side, connected to the valve element implementing the separation (4).