Vehicle configuration with motors that rotate between a lifting position and a thrusting position

Patent metadata

Field	Value
Publication number	US-11319063-B2
Application number	US-201916550795-A
Country	US
Kind code	B2
Filing date	Aug 26, 2019
Priority date	Feb 19, 2015
Publication date	May 3, 2022
Grant date	May 3, 2022

Abstract

This disclosure describes a configuration of an unmanned aerial vehicle (“UAV”) that will facilitate extended flight duration. 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 (also known as an octo-copter), etc. Likewise, to improve the efficiency of horizontal flight, the UAV also includes a pivot assembly that may rotate about an axis from a lifting position to a thrusting position. The pivot assembly may include two or more offset motors that generate a differential force that will cause the pivot assembly to rotate between the lifting position and the thrusting position without the need for any additional motors or gears.

First claim

What is claimed is:

1. An unmanned aerial vehicle (UAV), comprising:
a frame;
a plurality of lifting motors and corresponding lifting propellers oriented to provide a vertical lift to the UAV when the lifting propellers are rotated by the lifting motors; and
a pivot assembly coupled to the frame of the UAV and configured to rotate between a lifting position and a thrusting position, the pivot assembly including:
a pivot arm extending from the frame of the UAV and configured to rotate with respect to the frame of the UAV; and
a first thrusting motor and a second thrusting motor coupled to a first side of the pivot arm;

wherein:
the pivot assembly is configured to rotate to the lifting position responsive to the first thrusting motor and the second thrusting motor rotating in a first direction; and
the pivot assembly is configured to rotate to the thrusting position responsive to the first thrusting motor and the second thrusting motor rotating in a second direction opposite to the first direction.

2. The UAV of claim 1 , wherein the first thrusting motor and the second thrusting motor provide a lifting force for the UAV responsive to the pivot assembly being in the lifting position.

3. The UAV of claim 1 , wherein the first thrusting motor and the second thrusting motor provide a thrusting force for the UAV responsive to the pivot assembly being in the thrusting position.

4. The UAV of claim 1 , wherein the first and the second thrusting motors are approximately perpendicular to the frame of the UAV when the pivot assembly is in the thrusting position.

5. The UAV of claim 1 , wherein at least a portion of the pivot arm is formed in a shape of a wing.

6. A pivot assembly, comprising:
a pivot arm configured to rotate about an axis;
at least one motor coupled to a first side of the pivot arm;
a first mechanical stop that inhibits a rotation of the pivot arm in a first direction about the axis; and
a second mechanical stop that inhibits the rotation of the pivot arm in a second direction about the axis;
wherein:
the pivot arm is configured to rotate in the first direction to the first mechanical stop responsive to the at least one motor rotating in a first rotational direction; and
the pivot arm is configured to rotate in the second direction to the second mechanical stop responsive to the at least one motor rotating in a second rotational direction opposite to the first rotational direction.

7. The pivot assembly of claim 6 , wherein the at least one motor generates a lifting force when rotation of the pivot arm is inhibited by the first mechanical stop responsive to the at least one motor rotating in the first rotational direction.

8. The pivot assembly of claim 6 , wherein the at least one motor generates a thrusting force when rotation of the pivot arm is inhibited by the second mechanical stop responsive to the at least one motor rotating in the second rotational direction.

9. The pivot assembly of claim 6 , wherein the at least one motor is coupled to one of an underside or an upper side of the pivot arm when rotation of the pivot arm is inhibited by the second mechanical stop.

10. The pivot assembly of claim 6 , wherein at least a portion of the pivot arm is formed in a shape of a wing.

11. The pivot assembly of claim 6 , wherein the at least one motor further comprises:
a first motor coupled at a first position on the first side of the pivot arm; and
a second motor coupled at a second position on the first side of the pivot arm.

12. The pivot assembly of claim 11 , wherein the first motor and the second motor are configured to rotate in a same rotational direction.

13. The pivot assembly of claim 6 , further comprising:
an inertial component that inhibits rotation of the pivot arm if a force generated by the at least one motor is less than a threshold.

14. The pivot assembly of claim 13 , wherein the inertial component is at least one of a brake, a clutch, or a dampener.

15. The pivot assembly of claim 6 , wherein:
the pivot assembly is coupled to a vehicle;
the pivot assembly provides a lifting force for the vehicle when the pivot arm is inhibited by the first mechanical stop; and
the pivot assembly provides a thrusting force for the vehicle when the pivot arm is inhibited by the second mechanical stop.

16. The pivot assembly of claim 15 , wherein:
the vehicle is at least one of an aerial vehicle, an unmanned aerial vehicle, a ground based vehicle, an unmanned ground based vehicle, a water based vehicle, an unmanned water based vehicle, a spacecraft, or an unmanned spacecraft.

17. A method of operating a pivot assembly, the method comprising:
rotating a pivot assembly relative to a frame of a vehicle to a lifting position by rotating a first motor in a first rotational direction, wherein the pivot assembly is coupled to the frame of the vehicle and includes a pivot arm configured to rotate relative to the frame, and the first motor is coupled to the pivot arm;
providing lift to the vehicle by the first motor responsive to the pivot assembly rotating to the lifting position;
rotating the pivot assembly relative to the frame of the vehicle to a thrusting position by rotating the first motor in a second rotational direction opposite to the first rotational direction; and
providing thrust to the vehicle by the first motor responsive to the pivot assembly rotating to the thrusting position.

18. The method of claim 17 , wherein the first motor is coupled to one of an underside or an upper side of the pivot arm when the pivot assembly is in the thrusting position.

19. The method of claim 17 , wherein a second motor is coupled on a same side of the pivot arm as the first motor;
wherein the pivot assembly is further rotated to the lifting position by rotating the second motor in the first rotational direction; and
wherein lift is further provided to the vehicle by the second motor responsive to the pivot assembly rotating to the lifting position.

20. The method of claim 19 , wherein the pivot assembly is further rotated to the thrusting position by rotating the second motor in the second rotational direction; and
wherein thrust is further provided to the vehicle by the second motor responsive to the pivot assembly rotating to the thrusting position.

Assignees

• Amazon Tech Inc

Inventors

• Welsh Ricky Dean

Classifications

• B64U2101/60

  for transporting passengers; for transporting goods other than weapons · CPC title

• B64U10/25

  Fixed-wing aircraft (VTOL aircraft B64U10/20) · CPC title

• B64U2101/20

  for use as communications relays, e.g. high-altitude platforms · CPC title

• B64U20/60

  UAVs characterised by the material · CPC title

• B64U30/294

  Rotors arranged in the UAV body · CPC title