Vehicle external component having reduced vortex shedding

Patent metadata

Field	Value
Publication number	US-9827952-B2
Application number	US-201414501375-A
Country	US
Kind code	B2
Filing date	Sep 30, 2014
Priority date	Sep 30, 2014
Publication date	Nov 28, 2017
Grant date	Nov 28, 2017

Abstract

A windshield wiper arm is provided on an outside of an aircraft and positioned to directly engage an air flow while the aircraft is traveling. The wiper arm includes an arm portion coupled to the aircraft and having an arm exterior surface, the arm portion extending along an arm axis and defining an arm length. A bead extends outwardly from the arm exterior surface and defines a bead exterior surface, the bead being sized sufficiently to engage a boundary layer of the air flow. A wiper blade is coupled to the arm portion. The bead prevents separation of the boundary layer from the arm exterior surface, thereby to attenuate shedding of vortices and associated vibrations and noise.

First claim

What is claimed is:

1. A component disposed on an external side of a vehicle defining a vehicle surface and positioned to directly engage an air flow while the vehicle is traveling, the component comprising:
an arm coupled to the vehicle and having an arm exterior surface with an oval cross-sectional shape, the arm extending along an arm axis and defining an arm length, the arm being oriented relative to the vehicle surface so that the arm exterior surface includes an inward portion facing toward the vehicle surface, an arcuate outward portion facing away from the vehicle surface, an upstream end facing substantially normal to the vehicle surface, and a downstream end facing substantially normal to the vehicle surface, each of the inward and outward portions extending between the upstream and downstream ends; and
a bead extending from one of the inward and outward portions of the arm exterior surface and defining a bead exterior surface, the bead substantially perpendicular to the vehicle surface, the bead being sized to engage a boundary layer of the air flow and create turbulence in the airflow downstream of the bead.

2. The component of claim 1 , in which the bead extends substantially parallel to the arm axis and defines a bead length that is at least approximately 50% of the arm length.

3. The component of claim 2 , in which the bead has a height, the arm has a width, and a ratio of bead height to arm width is approximately 1 to 5%.

4. The component of claim 2 , in which the bead extends along a bead axis, and in which a distal half of the bead exterior surface is located a radius distance from the bead axis.

5. The component of claim 4 , in which the radius distance is approximately 0.025 inches.

6. The component of claim 1 , in which the bead extends from the inward portion of the arm exterior surface, and further comprising a second bead extending from the outward portion of the arm exterior surface and defining a second bead exterior surface configured to engage the boundary layer of the air flow and create turbulence in the air flow downstream of the second bead.

7. The component of claim 1 , in which the bead defines first and second ends, and in which the bead exterior surface extends continuously from the first end to the second end.

8. The component of claim 1 , in which the bead is formed integrally with the arm.

9. A method of reducing vortex shedding produced by an air flow passing over a component having an arm disposed on an outboard side of a vehicle and having an exterior surface with an oval cross-sectional shape, the method comprising:
orienting the arm relative to the vehicle surface so that the exterior surface of the arm includes an inward portion facing toward the vehicle surface, an arcuate outward portion facing away from the vehicle surface, an upstream end facing substantially normal to the vehicle surface, and a downstream end facing substantially normal to the vehicle surface, each of the inward and outward portions extending between the upstream and downstream ends;
positioning a bead along one of the inward and outward portions of the exterior surface of the arm, the bead defining a bead exterior surface extending from the arm exterior surface, the bead substantially perpendicular to the vehicle surface; and
creating turbulence in the airflow downstream of the bead by sizing the bead to engage a boundary layer of the air flow.

10. The method of claim 9 , in which positioning the bead comprises positioning the bead along the inward portion of the arm exterior surface.

11. The method of claim 10 , further comprising:
positioning a second bead along the exterior surface of the arm, the second bead defining a second bead exterior surface extending from the outward portion of the arm exterior surface; and
creating turbulence in the airflow downstream of the second bead by sizing the second bead to engage the boundary layer of the air flow.

12. The method of claim 9 , further comprising forming the bead integrally with the arm.

13. The method of claim 9 , further comprising:
forming the bead independently of the arm; and
bonding the bead to the arm.

14. A wiper arm disposed on an outside of an aircraft defining an aircraft surface and positioned to directly engage an air flow while the aircraft is traveling, the wiper arm comprising:
an arm portion coupled to the aircraft and having an arm exterior surface with an oval cross-sectional shape, the arm portion extending along an arm axis and defining an arm length, the arm portion being oriented relative to the aircraft surface so that the arm portion exterior surface includes an inward portion facing toward the aircraft surface, an arcuate outward portion facing away from the aircraft surface, an upstream end facing substantially normal to the aircraft surface, and a downstream end facing substantially normal to the aircraft surface, each of the inward and outward portions extending between the upstream and downstream ends;
a bead extending from one of the inward and outward portions of the arm exterior surface and defining a bead exterior surface having an arcuate profile, the bead having a size sufficient to engage a boundary layer of the air flow and create turbulence in the airflow downstream of the bead; and
a wiper blade coupled to the arm portion.

15. The wiper arm of claim 14 , in which the bead extends substantially parallel to the arm axis and defines a bead length that is at least approximately 50% of the arm length.

16. The wiper arm of claim 15 , in which the bead extends along a bead axis, in which a distal half of the bead exterior surface is located a radius distance from the bead axis, and in which the radius distance is approximately 0.025 inches.

17. The wiper arm of claim 14 , in which the bead extends from the inward portion of the arm exterior surface.

18. The wiper arm of claim 17 , further comprising a second bead extending from the outward portion of the arm exterior surface and defining a second bead exterior surface having an arcuate profile, the second bead having a size sufficient to engage the boundary layer of the air flow to create turbulence in the air flow downstream of the second bead.

19. The wiper arm of claim 14 , in which the bead is formed integrally with the arm portion.

Assignees

• Boeing Co

Inventors

• Spalart Philippe R
• Barker Gail M
• Bertolucci Brandon L

Classifications

• B60S1/3806

  Means, or measures taken, for influencing the aerodynamic quality of the wiper blades · CPC title

• B64C1/14

  Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens {accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers}(fairings movable in conjunction with undercarriage elements B64C25/16; bomb doors B64D1/06) · CPC title

• B60S1/3425 Primary

  Constructional aspects of the arm · CPC title

• B60S1/32

  characterised by constructional features of wiper blade arms {or blades} · CPC title

• B60S1/0408

  Means for influencing the aerodynamic quality of wipers, e.g. clip-on wind deflectors (B60S1/32 takes precedence) · CPC title