Vertical Take-Off and Landing Roadable Aircraft

• US 20160207368A1
• Filed: 01/21/2015
• Published: 07/21/2016
• Est. Priority Date: 01/21/2015
• Status: Abandoned Application

• Current Assignee: Gaonjur, Rajesh
• Original Assignee: Gaonjur, Rajesh
• Inventors: Gaonjur, Rajesh
• Application Number:
  US14/544,553
• Publication Number:
  US 20160207368A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B60F 5/02 convertible into aircraft
• CPC Class Codes: B64C 11/001 Shrouded propellers
• CPC Class Codes: B64C 27/08 with two or more rotors
• CPC Class Codes: B64C 37/00 Convertible aircraft

Abstract

A vertical take-off and landing (VTOL) roadable aircraft which has the features and dimensions of a typical road vehicle is disclosed. When operated on the road the wheels are powered by the engine. When the vehicle is configured for flight, a plurality of propellers is deployed from the storage compartment located on the roof and is powered by the same engine. The conversion process transforms the vehicle into a highly manoeuvrable quadcopter or a multi-rotor aircraft. The design concept enables propellers of relative large diameter to be conveniently secure to the vehicle, while allowing reliable deployment, retrieval and storage of the propellers as required. The total combined area of the propellers enables a low disk loading in the range of some helicopters with equivalent flight efficiency. The propellers are shrouded for safe operation. The conversion is automated, fast, and can be carried out while the vehicle is still moving.

Claims

1. A vehicle having a road configuration and a flight configuration comprising :

a fuselage or body of the vehicle;

a plurality of wheels which support the said fuselage on the ground, wherein at least one of the said wheels is rotated by at least one engine to enable the said vehicle to move during said road configuration;

a plurality of propellers, which is rotated generally in a horizontal plane by at least one engine so as to produce aerodynamic lift and enable the said vehicle to fly during said flight configuration;

a means which secure the said propeller to the said vehicle;

a means which enable the said propellers to be retrieved and stowed above one another on the roof of the said vehicle during said road configuration;

and a means to deploy the said propellers from the stowed position to the side of the said vehicle for use during said flight configuration.

2. A vehicle as recited in claim 1, wherein said propellers are shrouded, or enclosed so that the said vehicle can be operated safely.

3. A vehicle as recited in claim 1, wherein the said propeller comprises of a rotor hub with a plurality of blades extending radially from the said rotor hub.

5. A vehicle as recited in claim 1, wherein the said propeller comprise:

of a first rotor hub having a plurality of blades rotating in one direction; and

a second rotor hub having a plurality of blades rotating in counter-rotation to the said first rotor hub.

6. A vehicle as recited in claim 5, wherein the pitch of the said blades may be varied so as to modulate the amount of aerodynamic lift.

7. A vehicle as recited in claim 1, comprising of a storage compartment above the roof of the said vehicle so as to enclose the said propellers during the said road configuration, the said storage compartment comprising of side openings through which the said propellers are able to pass, when the said propellers are deployed during said flight configuration.

8. A vehicle as recited in claim 1. Wherein the said wheels and the said propellers may be rotated selective by the same engine or same group of to engines when the said vehicle is in said flight configuration or said road configuration.

9. A vehicle as recited as in claim 1, wherein each of the said propellers or group of said propellers are rotated by independent engine.

10. A vehicle as recited in claim 9, wherein the plurality of said propellers or said engines are mechanically interconnect in order to protect against single engine and multiple engines failures.

15. A vehicle as recited in claim 1, comprising of additional wings secured to the said vehicle so that to generate aerodynamic lift and control.

4. A vehicle as recited in clam 3, wherein the pitch of the said blades may be varied so as to modulate the amount of aerodynamic lift

11. A means which secure the said propeller to the said vehicle and enable the said propeller to be deployed for flight configuration or retrieved for road configuration,

the means comprising:

a shaft generally positioned vertically rotatably mounted and secured to the side of the said vehicle;

a supporting component rotatably mounted to the said shaft, which secure the said propeller to the said shaft ;

a first gear device mounted on the longitudinal axis of the said shaft and firmly secured to the said supporting component;

a second gear device which meshes with the first said gears device and is rotatably mounted and secured to the structure of the said vehicle, so that the rotation of the said second gear device enables the said propeller to pivot about the axis of the said shaft.

12. A means as recited in claim 11, wherein the said second gear device is rotated by a motor, in order to pivot the said propeller about the axis of the said shaft.

13. A means as recited in claim 11, wherein one end of the said shaft is connected to the engine, and the other end of the said shaft rotates the hub of said propellers by means of a transmission mechanism.

14. A mean as recited in claim 13, wherein a chain transmission comprising of a first sprocket gear mounted to one end of the said shaft and the second sprocket gear mounted to the hub of the said propeller, rotates the said propeller.