FOLDABLE RISE AND STARE VEHICLE

• US 20140008485A1
• Filed: 07/06/2012
• Published: 01/09/2014
• Est. Priority Date: 07/06/2012
• Status: Active Grant

• Current Assignee: Gert Magnus Lundgren
• Original Assignee: Gert Magnus Lundgren
• Inventors: LUNDGREN, GERT MAGNUS
• Granted Patent: US 8,844,860 B2
• Time in Patent Office: Days
• US Class Current: 244/17.13
• CPC Class Codes: A63H 27/12 Helicopters A63H27/04 takes precedence; Flying tops
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 20/50 Foldable or collapsible UAVs with frangible components B64U20/30
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 50/11 using internal combustion piston engines
• CPC Class Codes: B64U 50/19 using electrically powered motors

Abstract

A Foldable Rise and Stare Vehicle with a single engine assembly that contains a pair of inline counter-rotating propellers.

• • Two inline counter-rotating engines are directly connected to the propellers.
  • Gimbal mounting the engine assembly permits thrust to be directed forward to back and left to right to control the vehicle position in the horizontal plane, when hovering.
  • Varying the relative engine speeds controls yaw.

The Foldable Rise and Stare Vehicle is adaptable as an unmanned vehicle.

The vehicle collapses into a flat asssembly similar to a foldable beach chair, allowing for convenient transportation.

Claims

1. A Foldable Rise and Stare Vehicle capable of vertical hover and stare, comprising:

A base frame;

A foldable frame;

The two frame components connected with a pair of joiners permitting the foldable frame to unfold about 90 degrees from the base frame;

An engine assembly attached to the two sides of the foldable frame affixed so as to be tilt-able about a primarily lateral axis comprising;

A pair of inline counter-rotating propellers;

A pair of inline counter rotating engines, each engine attached to one of the inline counter-rotating propellers;

The entire engine assembly tilt-able around a primarily longitudinal axis.

2. The Foldable Rise and Stare Vehicle of claim 1, wherein the engine assembly is mounted so as to be tilt-able about the lateral and longitudinal axis of the Foldable Rise and Stare Vehicle such that:

Rotation of the engine assembly about the lateral axis provides a change in direction of the thrust to contain a longitudinal component, thereby permitting control of forward/aft location of the Foldable Rise and Stare Vehicle

Rotation of the engine assembly about the longitudinal axis provides a change in direction of the thrust to contain a lateral component, thereby permitting control of lateral position of the Foldable Rise and Stare Vehicle.

3. The Foldable Rise and Stare Vehicle of claim 1, wherein the relative speed of the inline counter-rotating engines is controlled such that a difference in speed or torque between the engines creates an imbalance in the torque produced by each engine and propeller,

the imbalance in the torque produced by each engine and propeller being operative to control yaw of the Foldable Rise and Stare Vehicle.

4. The Foldable Rise and Stare Vehicle of claim 1, further comprising;

flight controls for controlling the Foldable Rise and Stare Vehicle attitude and position, and;

an automatic feedback control mechanism for stabilizing flight characteristics of the Foldable Rise and Stare Vehicle.

5. The Foldable Rise and Stare Vehicle of claim 1, wherein the inline counter-rotating engines are internal combustion engines.

6. The Foldable Rise and Stare Vehicle of claim 1, wherein the inline counter-rotating motors are electric motors.

7. The Foldable Rise and Stare Vehicle of claim 1, wherein the Foldable Rise and Stare Vehicle further comprises a radio control receiver for receiving control signals from a remote control unit.