Personal transportation vehicle

• US 20100181414A1
• Filed: 01/21/2009
• Published: 07/22/2010
• Est. Priority Date: 01/21/2009
• Status: Abandoned Application

• Current Assignee: Ignacio Lopez Jr
• Original Assignee: Ignacio Lopez Jr
• Inventors: Lopez, Ignacio JR.
• Application Number:
  US12/320,136
• Publication Number:
  US 20100181414A1
• Time in Patent Office: Days
• US Class Current: 244/12.400
• CPC Class Codes: B64C 29/0033 the propellers being tiltable relative to the fuselage

Abstract

This is a Vertical/Short Takeoff and Landing (VSTOL) vehicle for personal transportation of at least one person, to a destination. The four main engine-driven rotors or propellers are pivot-mounted and can be varied in angular position. The main engines are operated by a vector-control system permitting the thrust of the vehicle engines to change from horizontal to vertical and vice versa for takeoff, forward or backwards flight, and landing procedures. This vehicle is also capable of hovering, ascending, and descending during flight. The other four rotors or propellers are mounted at fixed positions, two at the rear, and two at the front, of the vehicle. The vehicle also consists of landing gear of virtually any type.

Claims

1. The personal transportation vehicle substantially as described and illustrated herein.

2. All inventions described and illustrated herein.

3. A VSTOL vehicle comprising:

a a cockpit as part of the fuselage and a cargo area within the fuselage;

b a fuselage designed to maintain aerodynamic lift in horizontal or vertical flight and having both longitudinal and transverse axes;

c rotors or propellers which rotate about the longitudinal axis of the rotor or propeller to generate independent streams of airflow for propelling and stabilizing the vehicle;

d rotors or propellers which are pivot-mounted to the fuselage and can be varied in angular position;

e a means to transmit the energy generated by the engines to the rotors or propellers;

f a coordinated system to utilize the energy generated by the engines to stabilize and balance the vehicle and to allow the vehicle to move and rotate in any direction;

g a vector-control system permitting the thrust of the vehicle engines to change from horizontal to vertical and vice versa for takeoffs, flight, and landings;

h engines or power plants capable of generating and maintaining the necessary energy requirements during flight and emergency landings;

4. A VSTOL vehicle as in claim 3, wherein said rotors or propellers are ducted fans.

5. A VSTOL vehicle as in claim 3, wherein said rotors or propellers are not ducted fans.

6. A VSTOL vehicle as in claim 3, wherein the fuselage has at least two lift-producing rotors or propellers attached on each side of the transverse axis;

7. A VSTOL vehicle as in claim 3, wherein the fuselage has additional rotors or propellers which support the main rotors or propellers and further stabilize the vehicle;

8. A VSTOL vehicle as in claim 3, comprising of a means to generate and maintain high levels of angular momentum whereby the vehicle is stabilized by the gyroscopic effect;

9. A VSTOL vehicle as in claim 3, wherein the lift-producing rotors or propellers counter-rotate in relation to one another in order to compensate for and overcome the gyroscopic effect;

10. A VSTOL vehicle as in claim 3, wherein rotors or propellers and engines generate high levels of kinetic energy whereby the vehicle can utilize the generated energy to assist during takeoffs, flight, and landings.

11. A VSTOL vehicle as in claim 3, wherein the fuselage of this vehicle is shaped to utilize the ground effect during takeoffs, landings, and when hovering above land and water surfaces.

12. A VSTOL vehicle as in claim 3, wherein the vehicle has interchangeable landing gear, thereby allowing this vehicle to land on and takeoff from virtually any water or land surface.