Systems and methods for tuning propeller noise

Patent metadata

Field	Value
Publication number	US-11217217-B2
Application number	US-202016892540-A
Country	US
Kind code	B2
Filing date	Jun 4, 2020
Priority date	May 3, 2016
Publication date	Jan 4, 2022
Grant date	Jan 4, 2022

Abstract

The present disclosure relates to devices, systems, and methods for controlling and/or augmenting acoustic sounds emitted from flight vehicles, such as unmanned aerial vehicles (UAVs). For example, while in flight, a UAV may emit a characteristic sound or tone (or a plurality of such tones), which may be a result of propeller and/or motor noise. To mitigate such noise from UAVs, disclosed embodiments may include acoustic resonators that may provide additional tones to complement the sounds or tones emitted from the UAV. Namely, the acoustic resonators may be shaped, adjusted, or otherwise controlled to emit additional tones that form pleasing intervals in combination with the characteristic tone(s) from the UAV.

First claim

What is claimed is:

1. A device, comprising:
at least one propeller, wherein, while rotating, the at least one propeller emits at least one tone; and
at least one acoustic resonator proximate to the at least one propeller, wherein the at least one acoustic resonator is configured to emit at least one additional tone, wherein the at least one additional tone forms an interval with respect to the at least one tone, wherein the interval comprises a major third or a fifth.

2. The device of claim 1 , wherein the at least one acoustic resonator forms at least a portion of a shroud, wherein the shroud comprises an enclosure that at least partially encloses the at least one propeller.

3. The device of claim 1 , wherein the at least one tone and the at least one additional tone form a chord, wherein the chord comprises a plurality of intervals with respect to the at least one tone, wherein the plurality of intervals comprise at least a major third and a perfect fifth.

4. The device of claim 1 , wherein the device is incorporated in an unmanned aerial vehicle (UAV) and wherein the at least one propeller is configured to provide propulsion for the UAV.

5. The device of claim 4 , wherein the at least one tone and the at least one additional tone form a chord, wherein the chord is selected based on at least one of a flight mode of the UAV, a position of the UAV, or an altitude of the UAV.

6. A device, comprising:
at least one propeller, wherein, while rotating, the at least one propeller emits at least one tone; and
at least one acoustic resonator proximate to the at least one propeller, wherein the at least one acoustic resonator is configured to emit at least one additional tone, wherein the at least one additional tone forms a melody, wherein the melody comprises a plurality of successive additional tones.

7. The device of claim 6 , wherein the at least one acoustic resonator forms at least a portion of a shroud, wherein the shroud comprises an enclosure that at least partially encloses the at least one propeller.

8. The device of claim 6 , wherein the device is incorporated in an unmanned aerial vehicle (UAV) and wherein the at least one propeller is configured to provide propulsion for the UAV.

9. The device of claim 8 , wherein the at least one tone and the at least one additional tone form a melody selected from a plurality of possible melodies, wherein the plurality of possible melodies is selected based on at least one of a flight mode of the UAV, a position of the UAV, or an altitude of the UAV.

10. A method, comprising:
causing at least one propeller of an unmanned aerial vehicle (UAV) to rotate, wherein the at least one propeller is configured to provide propulsion for the UAV, wherein at least one acoustic resonator is proximate to the at least one propeller, and wherein at least one tuning element is coupled to the at least one acoustic resonator;
based on a flight mode of the UAV, a position of the UAV, or an altitude of the UAV, adjusting the at least one tuning element such that the adjusted tuning element and the corresponding acoustic resonator emit at least one additional tone.

11. The method of claim 10 , wherein adjusting the at least one tuning element comprises adjusting a resonant condition of the acoustic resonator based on a desired interval with respect to the at least one tone.

12. The method of claim 10 , wherein the at least one acoustic resonator forms at least a portion of a shroud, wherein the shroud comprises an enclosure that at least partially encloses the at least one propeller.

13. The method of claim 12 , wherein adjusting the at least one tuning element comprises adjusting at least one surface of the shroud based on a desired interval with respect to the at least one tone.

14. The method of claim 10 , wherein the at least one additional tone forms an interval with respect to the at least one tone, wherein the interval comprises a major third or a fifth.

15. The method of claim 10 , wherein the at least one tone and the at least one additional tone form a chord, wherein the chord comprises a plurality of intervals with respect to the at least one tone, wherein the plurality of intervals comprise at least a major third and a perfect fifth.

16. The method of claim 10 , wherein the at least one additional tone forms a melody, wherein the melody comprises a plurality of successive additional tones.

Assignees

• Wing Aviation Llc

Inventors

• Ratner Daniel

Classifications

• B64U50/14

  ducted or shrouded · CPC title

• B64U30/29

  Constructional aspects of rotors or rotor supports; Arrangements thereof · CPC title

• B64C11/001

  Shrouded propellers · CPC title

• G10K15/02 Primary

  Synthesis of acoustic waves (synthesis of speech G10L13/00) · CPC title

• G10F1/00

  Automatic musical instruments · CPC title