WO1997012805A1 - Aerodisk - atmospheric aeronautical vehicle - Google Patents

Aerodisk - atmospheric aeronautical vehicle Download PDF

Info

Publication number
WO1997012805A1
WO1997012805A1 PCT/BR1996/000044 BR9600044W WO9712805A1 WO 1997012805 A1 WO1997012805 A1 WO 1997012805A1 BR 9600044 W BR9600044 W BR 9600044W WO 9712805 A1 WO9712805 A1 WO 9712805A1
Authority
WO
WIPO (PCT)
Prior art keywords
atmospheric
circumfoil
aerodisk
propulsion
aeronautical vehicle
Prior art date
Application number
PCT/BR1996/000044
Other languages
French (fr)
Inventor
Jonathas De Amorim Gagliardi Madeira
Original Assignee
Amorim Gagliardi Madeira Jonat
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Amorim Gagliardi Madeira Jonat filed Critical Amorim Gagliardi Madeira Jonat
Publication of WO1997012805A1 publication Critical patent/WO1997012805A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/06Aircraft not otherwise provided for having disc- or ring-shaped wings
    • B64C39/062Aircraft not otherwise provided for having disc- or ring-shaped wings having annular wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/001Flying saucers

Definitions

  • This patent application aims to protect a new process of
  • ATMOSPHERIC AERONAUTICAL VEHICLE is capable of flight
  • circumfoil support bearings, a fuel tank, a bay for landing gear, landing
  • flaps flaps, directional rudder, a propulsion-motor unit, stabilization propeller,
  • control and maneuvering of the vehicle are arrayed.
  • present invention constitutes a new high-technology aero-space vehicle
  • Figure 1 shows the AERODISK -
  • Figure 2 shows the AERODISK -
  • Figure 3 shows a frontal view of the AERODISK -
  • AERODISK - ATMOSPHERIC AERONAUTICAL VEHICLE covers a cabin (1 ) (T), ⁇ ir-int ⁇ ke for the circumfoil (2) support bearings (3), an
  • aerodynamic circumfoil (4) fuel tank (5), bays for landing gear (6),

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

Patent of invention for the Aerodisk - Atmospheric Aeronautical Vehicle, consisting of a cabin (1, 1'), air intake for the circumfoil (2) support bearings (3), 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 (11), directional rudder (12), a propulsion-motor unit (13), stabilization propeller (14), air intake (15), exhaust (16), aerofoils (17), together making up an aeronautical vehicle, which is propelled by the propulsion-motor unit and controlled from the cabin and achieves flight through the spinning of the aerodynamic circumfoil.

Description

Descriptive Report for α Patent Application for the
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.

Claims

REQUEST
1 - The AERODISK - ATMOSPHERIC AERONAUTICAL
VEHICLE, is characterized by cabin (1) (! '), air-intake for the circumfoil
(2) support bearings (3), aerodynamic circumfoil (4), fuel tank (5), gates
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-motor unit (13), stabilization propeller (14), air
intake (15), exhaust (16) aerofoils (17).
PCT/BR1996/000044 1995-10-04 1996-09-25 Aerodisk - atmospheric aeronautical vehicle WO1997012805A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
BR9504322A BR9504322A (en) 1995-10-04 1995-10-04 Aerodisk - atmospheric aircraft
BRPI9504322-5 1995-10-04

Publications (1)

Publication Number Publication Date
WO1997012805A1 true WO1997012805A1 (en) 1997-04-10

Family

ID=4062394

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/BR1996/000044 WO1997012805A1 (en) 1995-10-04 1996-09-25 Aerodisk - atmospheric aeronautical vehicle

Country Status (2)

Country Link
BR (1) BR9504322A (en)
WO (1) WO1997012805A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106986029A (en) * 2017-03-31 2017-07-28 郭应辉 Disc-shaped flying craft

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1506566A1 (en) * 1967-04-25 1969-09-04 Klaus Bender Rotor disc
US3572613A (en) * 1969-02-17 1971-03-30 Arthur Porter Circular wing aircraft
US3690597A (en) * 1970-01-20 1972-09-12 Renato Di Martino Vertical take-off landing aircraft having a pair of coaxial counter-rotating rotors, each formed by a set of revolvable blades radially jutting from the body of the craft
DE1817932A1 (en) * 1968-10-19 1974-04-04 Alexander Hembluck ROTARY WING AIRPLANE
DE2401125A1 (en) * 1974-01-10 1975-07-17 Heinrich Kunel Vertical take-off and landing aircraft - has an approx. circular shape with rotatable lift surfaces moving around its circumference
US3946970A (en) * 1974-12-16 1976-03-30 Blankenship Ben F Gyroscopically stabilized, vertical takeoff and landing aircraft
US4193568A (en) * 1976-07-06 1980-03-18 Heuvel Norman L Disc-type airborne vehicle and radial flow gas turbine engine used therein
US4773618A (en) * 1987-01-21 1988-09-27 Ow Gordon J W High speed vertical take-off and landing aircraft
US5054713A (en) * 1989-04-03 1991-10-08 Langley Lawrence W Circular airplane
WO1991015400A1 (en) * 1990-04-05 1991-10-17 Valverde Rene L Turbocraft
US5072892A (en) * 1989-12-01 1991-12-17 Carrington Alfred C Aerodynamic device
US5170963A (en) * 1991-09-24 1992-12-15 August H. Beck Foundation Company VTOL aircraft
US5303879A (en) * 1992-01-29 1994-04-19 Sky Disc Holding Sa Aircraft with a ducted fan in a circular wing

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1506566A1 (en) * 1967-04-25 1969-09-04 Klaus Bender Rotor disc
DE1817932A1 (en) * 1968-10-19 1974-04-04 Alexander Hembluck ROTARY WING AIRPLANE
US3572613A (en) * 1969-02-17 1971-03-30 Arthur Porter Circular wing aircraft
US3690597A (en) * 1970-01-20 1972-09-12 Renato Di Martino Vertical take-off landing aircraft having a pair of coaxial counter-rotating rotors, each formed by a set of revolvable blades radially jutting from the body of the craft
DE2401125A1 (en) * 1974-01-10 1975-07-17 Heinrich Kunel Vertical take-off and landing aircraft - has an approx. circular shape with rotatable lift surfaces moving around its circumference
US3946970A (en) * 1974-12-16 1976-03-30 Blankenship Ben F Gyroscopically stabilized, vertical takeoff and landing aircraft
US4193568A (en) * 1976-07-06 1980-03-18 Heuvel Norman L Disc-type airborne vehicle and radial flow gas turbine engine used therein
US4773618A (en) * 1987-01-21 1988-09-27 Ow Gordon J W High speed vertical take-off and landing aircraft
US5054713A (en) * 1989-04-03 1991-10-08 Langley Lawrence W Circular airplane
US5072892A (en) * 1989-12-01 1991-12-17 Carrington Alfred C Aerodynamic device
WO1991015400A1 (en) * 1990-04-05 1991-10-17 Valverde Rene L Turbocraft
US5170963A (en) * 1991-09-24 1992-12-15 August H. Beck Foundation Company VTOL aircraft
US5303879A (en) * 1992-01-29 1994-04-19 Sky Disc Holding Sa Aircraft with a ducted fan in a circular wing

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106986029A (en) * 2017-03-31 2017-07-28 郭应辉 Disc-shaped flying craft
CN106986029B (en) * 2017-03-31 2024-01-12 郭应辉 Dish-shaped aircraft

Also Published As

Publication number Publication date
BR9504322A (en) 1998-05-05

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