Propeller blade trailing edge fringes for improved sound control

• US 10,259,562 B2
• Filed: 12/18/2015
• Issued: 04/16/2019
• Est. Priority Date: 12/18/2015
• Status: Active Grant

• Current Assignee: Amazon Technologies, Inc. (Amazon.com, Inc.)
• Original Assignee: Amazon Technologies, Inc. (Amazon.com, Inc.)
• Inventors: Beckman, Brian C., Kimchi, Gur, Ko, Allan
• Primary Examiner(s): O'Hara, Brian M
• Application Number:
  US14/975,274
• Publication Number:
  US 20170174320A1
• Time in Patent Office: 1,215 Days
• CPC Class Codes: B64C 11/00 Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
• CPC Class Codes: B64C 11/18 Aerodynamic features
• CPC Class Codes: B64C 11/20 Constructional features
• CPC Class Codes: B64C 2230/14 achieving noise reductions
• CPC Class Codes: B64C 2230/28 at propeller or rotor blades
• CPC Class Codes: B64C 23/06 by generating vortices
• CPC Class Codes: B64C 27/06 with single rotor
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/10 Rotorcrafts
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 20/20 for noise reduction
• CPC Class Codes: B64U 2101/60 for transporting passengers; for transporting goods other than weapons
• CPC Class Codes: B64U 2101/64 for parcel delivery or retrieval
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 50/31 generated by photovoltaics
• CPC Class Codes: Y02T 50/10 Drag reduction
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

Sounds are generated by an aerial vehicle during operation. For example, the motors and propellers of an aerial vehicle generate sounds during operation. Disclosed are systems, methods, and apparatus for actively adjusting the position of one or more propeller blade treatments of a propeller blade of an aerial vehicle during operation of the aerial vehicle. For example, the propeller blade may have one or more propeller blade treatments that may be adjusted between two or more positions. Based on the position of the propeller blade treatments, the airflow over the propeller is altered, thereby altering the sound generated by the propeller when rotating. By altering the propeller blade treatments on multiple propeller blades of the aerial vehicle, the different sounds generated by the different propeller blades may effectively cancel, reduce, and/or otherwise alter the total sound generated by the aerial vehicle.

Claims

1. An aerial vehicle comprising:

a motor configured to rotate a propeller such that the propeller generates a lifting force;

the propeller including;

a hub that is coupled to the motor so that the motor can rotate the propeller;

a propeller blade extending from the hub, the propeller blade including;

a leading edge;

a tip;

a trailing edge; and

a fringe extending from the trailing edge of the propeller blade;

a controller configured to alter a position of the fringe; and

a sensor configured to monitor a sound generated around the aerial vehicle;

wherein the controller alters the position of the fringe at a speed based at least in part on the sound.

2. The aerial vehicle of claim 1, wherein the controller includes:

an adjustment arm that extends along the propeller blade and is affixed to the fringe such that;

when the adjustment arm is in a first adjustment arm position, the fringe is in a first fringe position, and

when the adjustment arm is in a second adjustment arm position, the fringe is in a second fringe position that is different than the first fringe position.

3. The aerial vehicle of claim 2,

wherein the controller alters the position of the fringe by moving the adjustment arm between the first adjustment arm position and the second adjustment arm position at the speed based at least in part on the sound.

4. The aerial vehicle of claim 2, wherein:

the fringe is retracted into the propeller blade when the adjustment arm is in the first adjustment arm position; and

the fringe is extended beyond the trailing edge of the propeller blade when the adjustment arm is in the second adjustment arm position.

5. The aerial vehicle of claim 1, wherein:

a sound generated by the propeller blade is dampened by the fringe disrupting air passing the propeller blade.

6. A propeller blade, comprising:

a hub;

a tip;

a surface area that extends between the hub and the tip, the surface area having an upper side, a lower side, a leading edge that extends between the hub and the tip, and a trailing edge;

a fringe coupled along the trailing edge of the propeller blade; and

a controller configured to alter a position of the fringe at a speed based at least in part on a sound generated around the propeller blade.

7. The propeller blade of claim 6,

wherein the controller is configured to alter the position of the fringe between a retracted position and an extended position, wherein:

the fringe is retracted into the propeller blade when in the retracted position;

the fringe extends beyond the trailing edge of the propeller blade when in the extended position;

the propeller blade generates a first sound and has a first drag when rotating and the fringe is in the retracted position;

the propeller blade generates a second sound and has a second drag when rotating and the fringe is in the extended position;

the second sound is different than the first sound; and

the second drag is different than the first drag.

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

a second fringe coupled along a first portion of the trailing edge of the propeller blade that extends from the hub of the propeller blade; and

wherein the fringe is coupled to a second portion of the propeller blade that extends along the trailing edge of the propeller blade from the first portion toward the tip of the propeller blade.

9. The propeller blade of claim 8,

wherein the controller is configured to alter the position of at least one of the fringe or the second fringe.

10. The propeller blade of claim 8, wherein the fringe is formed of a first material and the second fringe is formed of a second material that is different than the first material.

11. The propeller blade of claim 6, wherein at least one of a shape or a length of the fringe varies.

12. The propeller blade of claim 6, wherein the fringe includes a plurality of fibers that extend from the trailing edge of the propeller blade.

13. The propeller blade of claim 12, wherein:

the fibers are configured to flex in a vertical direction with a rotation of the propeller blade; and

the fibers are configured to flex in a horizontal direction to a position in which they are aligned with a rotational direction of the propeller blade.

14. The propeller blade of claim 12, wherein:

a first fiber of the plurality of fibers includes a first shape, a first length, a first curvature, a first diameter, and is formed of a first material;

a second fiber of the plurality of fibers includes a second shape, a second length, a second curvature, a second diameter, and is formed of a second material; and

wherein at least one of;

the first shape and the second shape are different;

the first length and the second length are different;

the first curvature and the second curvature are different;

the first diameter and the second diameter are different;

or

the first material and the second material are different.

15. An aerial vehicle, comprising:

a frame;

a motor coupled to the frame;

a propeller coupled to and rotatable by the motor;

a first fringe positioned on the propeller, wherein a sound generated by the propeller when the propeller is rotating is altered based at least in part on a position of the first fringe;

a second fringe positioned on the propeller, wherein the sound generated by the propeller when the propeller is rotating is further altered based at least in part on a position of the second fringe; and

a controller configured to send instructions to alter a position of at least one of the first fringe or the second fringe; and

wherein the instructions are based at least in part on a determination by the controller that the aerial vehicle is below a defined altitude.

16. The aerial vehicle of claim 15, wherein:

the first fringe extends from a first portion of a trailing edge of the propeller and is positioned toward a tip of the propeller such that the first fringe alters a sound generated by a tip vortex resulting from the rotation of the propeller; and

the second fringe extends from a second portion of the trailing edge of the propeller and alters sound generated by air passing across the propeller when the propeller is rotating.

17. The aerial vehicle of claim 15, wherein the first fringe and the second fringe are each formed of a fibrous material that flexes during rotation of the propeller.

18. The aerial vehicle of claim 15,

wherein the controller is configured to cause the position of at least one of the first fringe or the second fringe to be altered while the propeller is rotating.

19. The aerial vehicle of claim 15, further comprising:

a navigation component configured to determine an altitude of the aerial vehicle; and

wherein the controller is in communication with the navigation component.

20. The aerial vehicle of claim 15, wherein:

the first fringe may be moved between a first retracted position in which the first fringe is retracted into the propeller and a first extended position in which the first fringe extends beyond a trailing edge of the propeller;

the second fringe may be moved between a second retracted position in which the second fringe is retracted into the propeller and a second extended position in which the second fringe extends beyond the trailing edge of the propeller;

the controller sends instructions that cause at least one of the first fringe or the second fringe to move to the first extended position or the second extended position, respectively, when it is determined that the aerial vehicle is below the defined altitude;

sound generated by a tip vortex resulting from the rotation of the propeller is altered when the first fringe is in the first extended position; and

sound generated by air passing the propeller when the propeller is rotating is altered when the second fringe is in the second extended position.