FIELD: airfield landing devices.
SUBSTANCE: proposed device includes platform mounted on trolley with wheel pairs and internal combustion engine of electric motor. Platform is provided with facilities for securing the aircraft relative to trolley after its lowering. Platform is adjustable in height by means of hydraulic unit; aircraft fasteners are made in form of spring-loaded rubber grips. Wheel pairs are provided with low-inertia electromagnetic brakes.
EFFECT: enhanced reliability of landing; reduced friction forces and impact of fuselage against landing strip.
1 dwg, 1 tbl
Authors
Dates
2006-03-27—Published
2004-06-15—Filed