SAPHARY all-weather light plane of vertical take-off (Light Vihrelyot) (Fig. 8) has the least overall dimensions among planes of the given class. It can land into any unprepared site and to fly in any weather conditions, excepting, objectively insuperable. The qualities which exotic for light plane it give a powerHyperflywheel serves a power source, simultaneously providing its hyperstability on ground and in flight. It’s have a lift-propellent device traditionally called as aSystem of an Airscrew-Wing with an Adaptive Wing and considered above the Vortical Lift-Propellent system.
Adaptive Wing names the device, the profile of which takes the form, close to optimum on each specific mode of flight. The elements of an Adaptive Wing automatically deviate depending on speed and angle of attack, saving smoothness of contours external and sometimes and internal surfaces. The control elements of an Adaptive Wing implements a built-in automated system under some law, selected because of calculation and experimental researches.
Thus there is the capability to minimize inductive resistance in cruise flight and to lower to a minimum peaks of rarefaction on a leading edge of a wing that prevents a separation of a flow and loss of sucking force on large angles of attack.
SAPHARY represents a high-wing plane with a small size fuselage 1, without a tail, but with slices-kiels 9, installed immediately on an Adaptive wing 3. Located on it on all span and chord the power mechanization rejects downwards jets of an air from the Vortical Lift-Propellent Systems 2 at take-off and landing. It is not closed completely in cruise flight, forming a Flat Vortex Shroud for a wing, that increases its common area. It allows to fly on a minimum angle of attack that reaching minimum inductive and profile resistance of a wing in turn provides.
Overstability of the plane in flight and motion and parking on an one wheel is provided by a Hyperflywheel 4 located behind a passenger cabin 5. It is established with a capability of a limited hunt effect of the rather cross-sectional axis. It allows to change an angle of attack of the airplane concerning a plane of rotation of aHyperflywheel 4. The indicated singularities provide Quasi-vertical Take-off and Landing (QVTL) (Fig. 9) This term is understood as vertical take-off on altitude of an air cushion created by it (1) with consequent moving above a reference surface at this altitude (2) or further set of altitude with a boost on a horizontal (3).
Similarly implement a steep drop (5) and contactless landing (6). The similar method was applied on earlier autogiro with use of inertia of a main rotor. However last had not a reserve of energy, sufficient for a long-duration hovering and furthermore movings in a horizontal plane for a selection of a landing site from an air. These shortages are away at a considered as example of the VTOL Light Vihrelyot.
