Deployable propeller blades for aerial vehicles

• US 10,494,088 B1
• Filed: 08/18/2017
• Issued: 12/03/2019
• Est. Priority Date: 08/18/2017
• Status: Active Grant

• Current Assignee: Amazon Technologies, Inc. (Amazon.com, Inc.)
• Original Assignee: Amazon Technologies, Inc. (Amazon.com, Inc.)
• Inventors: Coralic, Vedran, Notteboom, Cyriel, Ludena, David Moro
• Primary Examiner(s): Vilakazi, Sizo B
• Application Number:
  US15/680,887
• Time in Patent Office: 837 Days
• CPC Class Codes: B64C 11/28 Collapsible or foldable blades
• CPC Class Codes: B64C 11/48 Units of two or more coaxial propellers
• CPC Class Codes: B64C 2027/8236 including pusher propellers
• CPC Class Codes: B64C 27/10 arranged coaxially
• CPC Class Codes: B64C 27/14 Direct drive between power plant and rotor hub
• CPC Class Codes: B64C 27/82 characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/14 with four distinct rotor axes, e.g. quadcopters
• CPC Class Codes: B64U 10/16 with five or more distinct rotor axes, e.g. octocopters
• CPC Class Codes: B64U 30/24 Coaxial rotors
• CPC Class Codes: B64U 30/291 Detachable rotors or rotor supports
• CPC Class Codes: B64U 50/23 with each propulsion means having an individual motor

Abstract

Aerial vehicles may be equipped with propellers having pivotable blades that are configured to rotate when the propellers are not rotating under power. A pivotable blade may rotate about an axis of a propeller with respect to a hub until the pivotable blade is coaligned with a fixed blade. When the propeller is rotating a lifting force from the blade may cause the blade to rotate to a deployed position that is not coaligned with the fixed blade.

Claims

1. An unmanned aerial vehicle comprising:

a frame;

a motor mounted to the frame, wherein the motor comprises a shaft;

a first hub positioned on the shaft and including;

a first blade joined to the first hub;

a second blade joined to the first hub; and

a guide;

wherein the first hub is coupled to the shaft or the motor and rotates with a rotation of the shaft and the motor;

a second hub positioned along the shaft and including;

a third blade joined to the second hub;

a fourth blade joined to the second hub; and

a protrusion extending from the second hub and mating with the guide of the first hub such that a rotation of the second hub with respect to the first hub is limited by the guide and the rotation of the first hub causes a rotation of the second hub; and

a spring positioned to apply a first force to at least one of the first hub or the second hub, wherein;

when the motor is not rotating, the first force causes the second hub to align with the first hub such that the third blade and fourth blade of the second hub are coaxially aligned with the first blade and the second blade; and

when the motor is rotating, a lifting force produced by a rotation of the third blade and the fourth blade causes the second hub to rotate with respect to the first hub such that the third blade and the fourth blade are not coaxially aligned with the first blade and the second blade.

2. The unmanned aerial vehicle of claim 1, wherein:

the first hub includes a substantially hollow upper portion; and

the guide is aligned along an interior of the substantially hollow upper portion.

3. The unmanned aerial vehicle of claim 2, wherein:

the second hub includes a lower portion positionable inside the substantially hollow upper portion of the first hub.

4. The unmanned aerial vehicle of claim 1, wherein the guide allows the second hub to rotate approximately ninety degrees with respect to the first hub such that when the motor is rotating the first blade, the second blade, the third blade, and the fourth blade are approximately equally spaced about a perimeter of the shaft.

5. The unmanned aerial vehicle of claim 1, wherein the guide has a curved shape based at least in part on a change in the first force applied by the spring as the second hub rotates with respect to the first hub.

6. A propeller apparatus, comprising:

a first hub;

a first blade coupled to the first hub;

a second hub pivotally coupled to the first hub;

a second blade coupled to the second hub; and

a spring applying a first force to at least one of the first hub or the second hub;

wherein;

the second hub is pivotable with respect to the first hub between;

a coaligned position in which the first blade and the second blade are coaligned and vertically stacked and the first force is greater than a second force resulting from a rotation of the first hub; and

a deployed position in which the first blade and the second blade are not coaligned and the first force is less than the second force.

7. The propeller apparatus of claim 6, further comprising:

a third blade coupled to the first hub; and

a fourth blade coupled to the second hub;

wherein;

the third blade and the fourth blade are coaligned and stacked when the second hub is in the coaligned position; and

the third blade and the fourth blade are not coaligned when the second hub is in the deployed position.

8. The propeller apparatus of claim 6, further comprising:

a shaft;

a propeller nut positioned on an end of the shaft; and

wherein the spring is positioned between an upper portion of the second hub and the propeller nut.

9. The propeller apparatus of claim 8, wherein:

the spring is in an extended position and applying a downward force on the second hub when the second hub is in the coaligned position; and

the spring is in a contracted position when the second hub is in the deployed position.

10. The propeller apparatus of claim 9, wherein:

the spring moves between the extended position and the contracted position when a lifting force generated at least in part by the second blade exceeds the downward force and the second hub rotates between the coaligned position and the deployed position.

16. The propeller apparatus of claim 6, wherein:

the first hub includes a guide; and

the second hub includes a protrusion positioned within the guide.

17. The propeller apparatus of claim 16, wherein the guide is configured to define the coaligned position and the deployed position of the second hub.

18. The propeller apparatus of claim 16, wherein the protrusion is configured to move between a first end of the guide and a second end of the guide.

19. The propeller apparatus of claim 18, wherein the first end of the guide is associated with the deployed position of the second hub, and the second end of the guide is associated with the coaligned position of the second hub.

20. The propeller apparatus of claim 16, wherein:

the first hub includes a substantially hollow upper portion;

the guide is aligned along an interior of the substantially hollow upper portion of the first hub;

the second hub includes a lower portion positionable inside the substantially hollow upper portion of the first hub; and

the protrusion is located along an exterior of the lower portion of the second hub.

11. An apparatus comprising:

a first hub operable to engage and be coupled with at least one of a shaft of a motor or the motor;

a second hub pivotably coupled to the first hub and operable to pivot with respect to the first hub between a coaligned position and a deployed position in response to a rotation of the first hub;

a first blade coupled to the first hub; and

a second blade coupled to the second hub;

wherein;

the second hub rotates when the first hub is rotated;

the second blade generates a lifting force when the second hub rotates;

the lifting force causes the second hub to rotate into the deployed position; and

the first blade is separated from the second blade when the second hub is in the deployed position.

12. The apparatus of claim 11, wherein the first blade and the second blade are coaligned and vertically stacked when the second hub is in the coaligned position.

13. The apparatus of claim 11, further comprising:

a guide incorporated into the first hub; and

a protrusion extending from the second hub and positioned within the guide; and

wherein the guide limits an amount of pivot of the second hub with respect to the first hub.

14. The apparatus of claim 13, further comprising:

a deployment notch positioned at a first end of the guide, wherein the deployment notch receives the protrusion when the second hub is in the deployed position.

15. The apparatus of claim 11, further comprising:

a spring configured to cause the second hub to be positioned in the coaligned position when the shaft is not rotating the first hub.