Unmanned aerial vehicle with a tri-wing configuration

Patent metadata

Field	Value
Publication number	US-10640204-B2
Application number	US-201514637323-A
Country	US
Kind code	B2
Filing date	Mar 3, 2015
Priority date	Mar 3, 2015
Publication date	May 5, 2020
Grant date	May 5, 2020

Abstract

This disclosure describes a configuration of an unmanned aerial vehicle (UAV) that includes a substantially polygonal perimeter frame and a central frame. The perimeter frame includes a front wing, a lower rear wing, and an upper rear wing. The wings provide lift to the UAV when the UAV is moving in a direction that includes a horizontal component. The UAV may have any number of lifting motors. For example, the UAV may include four lifting motors (also known as a quad-copter), eight lifting motors (octo-copter), etc. Likewise, to improve the efficiency of horizontal flight, the UAV may also include one or more thrusting motors and corresponding thrusting propellers. When the UAV is moving horizontally, the thrusting motor(s) may be engaged and the thrusting propeller(s) will aid in the horizontal propulsion of the UAV.

First claim

What is claimed is:

1. An unmanned aerial vehicle (UAV), comprising:
a perimeter frame, including:
a front portion including a front wing configured to provide lift to the UAV when the UAV is moving in a direction that includes a horizontal component;
a rear portion including a first rear wing and a second rear wing positioned vertically above the first rear wing configured to provide lift to the UAV when the UAV is moving in the direction that includes the horizontal component;
a first side rail joining the front portion and the rear portion;
a second side rail joining the front portion and the rear portion; and
wherein the perimeter frame has a substantially polygonal shape; and
wherein no lifting motors are directly coupled to the perimeter frame; and

a central frame positioned within the substantially polygonal shape of the perimeter frame and coupled to an interior of the perimeter frame;
a thrusting motor coupled to one of the front wing or the first rear wing;
a thrusting propeller coupled to the thrusting motor and oriented to generate a substantially horizontal thrust;
wherein the thrusting motor and thrusting propeller are oriented so that at least a portion of the thrusting propeller is within the substantially polygonal shape of the perimeter frame;
a plurality of lifting motors, each of the plurality of lifting motors coupled to the central frame; and
a plurality of lifting propellers, each propeller coupled to a motor of the plurality of lifting motors, wherein each of the plurality of lifting propellers are within the substantially polygonal shape of the perimeter frame;
wherein the perimeter frame surrounds the plurality of lifting motors and the plurality of lifting propellers associated with the UAV.

2. The UAV of claim 1 , wherein:
the front wing includes a plurality of flaps;
each of the plurality of flaps is configured to be rotated together with respect to the front wing; and
each of the plurality of flaps is configured to be extended in opposite directions to increase a height of the front wing.

3. The UAV of claim 1 , further comprising an antenna element embedded in a surface of at least one of the front wing or the first rear wing.

4. The UAV of claim 1 , further comprising:
a second thrusting motor coupled to the other of the first rear wing and the front wing.

5. The UAV of claim 1 , wherein the front portion of the perimeter frame further includes:
a first winglet extending in a downward direction and substantially perpendicular to the front wing; and
a second winglet extending in a downward direction and substantially perpendicular to the front wing, wherein the first winglet and the second winglet are configured to provide stability and control to the UAV when the UAV is moving in the direction that includes the horizontal component.

6. The UAV of claim 1 , wherein the substantially polygonal shape of the perimeter frame is substantially rectangular.

7. An aerial vehicle, comprising:
a perimeter frame, including:
a front portion including a front wing;
a rear portion including a first rear wing and a second rear wing positioned vertically above the first rear wing;
a first side rail joining the front portion and the rear portion;
a second side rail joining the front portion and the rear portion; and
wherein the perimeter frame has a substantially polygonal shape; and
wherein no lifting motors are directly coupled to the perimeter frame; and

a central frame positioned within the substantially polygonal shape of the perimeter frame and coupled to the perimeter frame;
a first thrusting motor coupled to at least one of the front wing or the first rear wing;
a first thrusting propeller coupled to the first thrusting motor and oriented to generate a substantially horizontal thrust;
wherein the first thrusting motor and the first thrusting propeller are oriented so that at least a portion of the first thrusting propeller is within the substantially polygonal shape of the perimeter frame;
a plurality of lifting motors, each of the plurality of lifting motors coupled to the central frame; and
a plurality of lifting propellers, each propeller coupled to a motor of the plurality of lifting motors;
wherein the perimeter frame surrounds the plurality of lifting motors and the plurality of lifting propellers associated with the aerial vehicle.

8. The aerial vehicle of claim 7 , further comprising:
a second thrusting motor coupled to the other of the at least one of the front wing or the first rear wing and oriented to generate a substantially horizontal thrust.

9. The aerial vehicle of claim 7 , further comprising:
a first winglet coupled to the front portion, extending in a downward direction and substantially perpendicular to the front wing; and
a second winglet coupled to the front portion, extending in a downward direction and substantially perpendicular to the front wing, wherein the first winglet and the second winglet provide stability and control to the aerial vehicle when the aerial vehicle is moving in a direction that includes a horizontal component.

10. An aerial vehicle, comprising:
a front wing;
a first rear wing;
a second rear wing positioned vertically above the first rear wing;
a first side rail joining the front wing, the first rear wing, and the second rear wing;
a second side rail joining the front wing, the first rear wing, and the second rear wing; and
a central frame positioned within a perimeter defined by the front wing, the first rear wing, the first side rail, and the second side rail, wherein no lifting motors are directly coupled to the perimeter defined by the front wing, the first rear wing, the first side rail, and the second side rail;
a plurality of lifting motors, each of the plurality of lifting motors coupled to the central frame;
at least one thrusting motor oriented substantially perpendicular to at least one of the plurality of lifting motors; and
a thrusting propeller coupled to the at least one thrusting motor and oriented to generate a substantially horizontal thrust;
wherein the perimeter defined by the front wing, the first rear wing, the first side rail, and the second side rail surrounds the plurality of lifting motors associated with the aerial vehicle;
wherein the at least one thrusting motor and the thrusting propeller are oriented so that at least a portion of the thrusting propeller is within the perimeter defined by the front wing, the first rear wing, the first side rail, and the second side rail.

11. The aerial vehicle of claim 10 , further comprising:
a plurality of lifting propellers, each propeller coupled to a motor of the plurality of lifting motors.

12. The aerial vehicle of claim 10 , further comprising:
a first winglet coupled to at least one of the front wing or the first side rail, extending in a downward direction and substantially perpendicular to the front wing; and
a second winglet coupled to at least one of the front wing or the second side rail, extending in a downward direction and substantially perpendicular to the front wing.

Assignees

• Amazon Tech Inc

Inventors

• Welsh Ricky Dean
• Legrand Iii Louis Leroi

Classifications

• B64C39/04 Primary

  having multiple fuselages or tail booms · CPC title

• B64C23/069

  using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips · CPC title

• B64C29/0025

  the propellers being fixed relative to the fuselage · CPC title

• B64C27/22 Primary

  Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft · CPC title

• B64C9/26

  by multiple flaps · CPC title