invention of an "AERODIS - ATMOSPHERIC

AERONAUTICAL VEHICLE"

This patent application aims to protect a new process of

5. flight and a new form of aeronautical construction, which has been

developed to take advantage of its superior aerodynamic design

qualities, offering great practical and operational advantage for its crew

and for its utilization by persons. The resulting AERODISK -

ATMOSPHERIC AERONAUTICAL VEHICLE is capable of flight, and

10. can be utilized for the transport of freight and passengers. It consists of a

cabin and a rotational aerodynamic circumfoil, an air-intake for the

circumfoil, support bearings, a fuel tank, a bay for landing gear, landing

gear, cowlings for the propulsion motor, ailerons, connection column,

flaps, directional rudder, a propulsion-motor unit, stabilization propeller,

1 5. air intake, exhaust and aerofoils.

Upon activating the ignition of the propulsion-motor and

raising the power level, the relative wind at the intake of the circumfoil

become engaged internally causing it to rotate, thus creating the lift for

the AERODISK - ATMOSPHERIC AERONAUTICAL VEHICLE and making

it capable of flight. Within the cabin the instruments necessary for the

control and maneuvering of the vehicle are arrayed.

Aeroplanes and helicopters are commonplace, but

problems are experienced in conciliating the difficulties of vertical take

5. off with the high-speed maneuvers, whereas this presents no difficulty in

case of the AERODISK - ATMOSPHERIC AERONAUTICAL VEHICLE. This

present invention constitutes a new high-technology aero-space vehicle,

of great utility, bringing together usefulness, practicality and

functionality. It can be manufactured in metallic materials or others of

10. comparable strength, in accordance with the desired size and/or

specified function, providing advantage and convenience to users.

In order to better illustrate the object of this present

descriptive report, drawings are attached merely for purposes of

demonstration, and these should in no way place any limitation upon the

15. scope of the patent.

Figure 1 (model 1 ) shows the AERODISK -

ATMOSPHERIC AERONAUTICAL VEHICLE in profile.

Figure 2 (model 2) shows the AERODISK -

ATMOSPHERIC AERONAUTICAL VEHICLE in profile.

20. Figure 3 shows a frontal view of the AERODISK -

ATMOSPHERIC AERONAUTICAL VEHICLE.

This present application for a patent of invention for the

AERODISK - ATMOSPHERIC AERONAUTICAL VEHICLE covers a cabin (1 )

(T), αir-intαke for the circumfoil (2) support bearings (3), an

aerodynamic circumfoil (4), fuel tank (5), bays for landing gear (6),

landing gear (7), cowlings for the propulsion-motor unit (8), ailerons (9),

connection column (10), flaps (1 1 ), directional rudder(12) a propulsion-

5. motor unit (13), stabilization propeller (14), air intake (15), exhaust (16)

aerofoils (17).

The AERODISK - ATMOSPHERIC AERONAUTICAL VEHICLE , besides

offering many advantages, presents characteristics fulfilling the requisite

of novelty, and thus merits a patent of invention as it fully satisfies the

10. criteria, since its invention combines and modifies previously known

elements, in a different form, resulting in a new form, a new process,

and with the advantages of greater efficiency and better utilization.