Noise reducing profile for helicopter rotor blade tracking wedges

Patent metadata

Field	Value
Publication number	US-9849976-B2
Application number	US-201414462889-A
Country	US
Kind code	B2
Filing date	Aug 19, 2014
Priority date	Aug 19, 2014
Publication date	Dec 26, 2017
Grant date	Dec 26, 2017

Abstract

A tracking wedge, a rotor and a method for modifying a movement of air over a tracking wedge. According to aspects of the disclosure, a tracking wedge used to correct the tracking of a helicopter rotor blade may include one or more acoustic management mechanisms. The acoustic management mechanisms may change the manner in which air moves over the surface of the tracking wedge. In some examples, changing the manner in which air moves over the surface of the tracking wedge may reduce noise generated by the use of the tracking wedge.

First claim

What is claimed is:

1. A tracking wedge, comprising:
a wedge-shaped body configured for attachment to an aerodynamic surface;
a leading edge;
a trailing edge;
a plurality of first acoustic management mechanisms disposed proximate to the trailing edge of the tracking wedge, each first acoustic management mechanism of the plurality of first acoustic management mechanisms having a first surface abutting a second surface to create a leading junction, the second surface abutting the first surface of an adjacent first acoustic management mechanism of the plurality of first acoustic management mechanisms to create a trailing junction, and the plurality of first acoustic management mechanisms having a variable trailing edge configured to modify a flow of air moving over a surface of the tracking wedge; and
a second acoustic management mechanism configured to shape the flow of air moving across the surface of the tracking wedge prior to the air coming in contact with the plurality of first acoustic management mechanisms.

2. The tracking wedge of claim 1 , wherein the plurality of first acoustic management mechanisms is configured to reduce an amount of disturbance placed on the air moving over the surface of the tracking wedge.

3. The tracking wedge of claim 1 , wherein the plurality of first acoustic management mechanisms comprises one or more voids.

4. The tracking wedge of claim 1 , wherein the second acoustic management mechanism comprises a series of dimples.

5. The tracking wedge of claim 1 , wherein the second acoustic management mechanism comprises a series of peaks.

6. The tracking wedge of claim 1 , wherein the variable edge of the plurality of first acoustic management mechanisms comprises one or more serrations.

7. The tracking wedge of claim 6 , wherein at least one of the one or more serrations comprises an end point configured to extend beyond a trailing edge of the aerodynamic surface.

8. The tracking wedge of claim 1 , wherein the first surface and the second surface of each first acoustic management mechanism of the plurality of first acoustic management mechanisms extend upwards from a bottom surface of the tracking wedge at a substantially 90 degree angle such that the leading junction creates a vertical line that is normal to the bottom surface of the tracking wedge, and wherein the first surface and the second surface of each first acoustic management mechanism of the plurality of first acoustic management mechanisms create a plane normal to the bottom surface of the tracking wedge.

9. The tracking wedge of claim 8 , wherein the first surface and the second surface of each first acoustic management mechanism of the plurality of first acoustic management mechanisms extend from the bottom surface of the tracking wedge at a non-substantially 90 degree angle to create a slope from a top surface to a bottom surface of the plurality of first acoustic management mechanisms.

10. A rotor blade, comprising:
a tracking wedge affixed to the rotor blade, the tracking wedge comprising:
a wedge-shaped body;
a trailing edge;
a plurality of first acoustic management mechanisms disposed proximate to the trailing edge of the tracking wedge, each first acoustic management mechanism of the plurality of first acoustic management mechanisms having a first surface abutting a second surface to create a leading junction, the second surface abutting the first surface of an adjacent first acoustic management mechanism of the plurality of acoustic management mechanisms to create a trailing junction, and the plurality of first acoustic management mechanisms having a variable trailing edge configured to modify a flow of air moving over a surface of the tracking wedge;
a second acoustic management mechanism configured to shape the flow of air moving across the surface of the tracking wedge prior to the air coming in contact with the plurality of first acoustic management mechanisms.

11. The rotor blade of claim 10 , wherein the plurality of first acoustic management mechanisms is configured to reduce an amount of disturbance placed on the air moving over the surface of the tracking wedge.

12. The rotor blade of claim 10 , wherein the second acoustic management mechanism comprises a series of dimples or a series of peaks.

13. The rotor blade of claim 10 , wherein the first surface and the second surface of each first acoustic management mechanism of the plurality of first acoustic management mechanisms extend upwards from a bottom surface of the tracking wedge at a substantially 90 degree angle such that the leading junction creates a vertical line that is normal to the bottom surface of the tracking wedge, and wherein the first surface and the second surface of each first acoustic management mechanism of the plurality of first acoustic management mechanisms create a plane normal to the bottom surface of the tracking wedge.

14. The rotor blade of claim 10 , wherein the variable edge of the plurality of first acoustic management mechanisms comprises one or more serrations and the one or more serrations include one or more voids.

15. The rotor blade of claim 14 , wherein at least one of the one or more serrations comprises an end point configured to extend beyond a trailing edge of the rotor blade.

16. A method of managing an acoustic profile associated with a tracking wedge, comprising:
rotating a rotor blade about a central axis;
routing an effluent airflow over a top surface of the tracking wedge having a wedge-shaped body;
modifying a movement of the effluent airflow in a suitable path to reduce noise using a plurality of first acoustic management mechanisms having a first surface abutting a second surface to create a leading junction, the second surface abutting the first surface of an adjacent first acoustic management mechanism of the plurality of first acoustic management mechanisms to create a trailing junction, and the plurality of acoustic management mechanisms having a variable trailing edge configured for modifying the movement of the effluent air over the tracking wedge; and
modifying a flow of air moving across a surface of the tracking wedge using a second acoustic management mechanism, the second acoustic management mechanism configured to shape the flow of air prior to the air coming in contact with the plurality of first acoustic management mechanisms.

17. The method of claim 16 , wherein the second acoustic management mechanism comprises a series of dimples or a series of peaks.

18. The method of claim 16 , wherein modifying the movement of the effluent airflow includes the first surface and the second surface of each first acoustic management mechanism of the plurality of first acoustic management mechanisms extending upwards from a bottom surface of the tracking wedge at a substantially 90 degree angle such that the leading junction creates a vertical line that is normal to the bottom surface of the tracking wedge, and wherein the first surface and the second surface of each first acoustic management mechanism of the plurality of first acoustic management mechanisms create a plane normal to the bottom surface of the tracking wedge.

19. The method of claim 16 , wherein the plurality of first acoustic management mechanisms comprises one or more serrations configured to reduce an amount of disturbance placed on the air moving over the surface of the tracking wedge.

20. The method of claim 19 , wherein at least one of the one or more serrations comprises an end point configured to extend beyond a trailing edge of the

Assignees

• Boeing Co

Inventors

• Piechowicz Richard

Classifications

• B64C2230/28

  at propeller or rotor blades · CPC title

• B64C2230/26

  by using rib lets or hydrophobic surfaces · CPC title

• B64C27/467 Primary

  Aerodynamic features · CPC title

• B64C27/008

  Rotors tracking or balancing devices · CPC title

• Y02T50/166

  Cross-Sectional Technologies · mapped topic