IP Library Patent Application 14681737
Patent Application
App. No. 14/681,737

Load Compensating Devices

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Quick Facts
Patent No.
US None
App. No.
14/681,737
Abstract

Various air deflector shapes, sizes and configurations for use in a load compensating device on an airfoil are provided. The air deflector arrangements are configured to alter the airflow around the air deflector in order to affect sound or acoustics associated with the air deflector when deployed during operation. Some example configurations that may alter the air flow around the air deflector include air deflectors having a plurality of apertures, air deflectors including a scalloped edge, and/or air deflectors including a plurality of protrusions extending from a portion of the air deflector.

Claims (30)

1 . An air deflector, comprising:

a first portion, the first portion being substantially rectangular and having a first end distal to a surface from which the air deflector extends and a second end proximal to the surface from which the air deflector extends; and

a second portion arranged vertically above the first portion, the second portion including a plurality of protrusions extending outward from the first end of the first portion,

wherein the air deflector is deployable from a first position recessed within an airfoil-shaped device to a second position extending outward from the airfoil-shaped device.

2 . The air deflector of claim 1 , wherein the plurality of protrusions include a plurality of scallops extending outward from the first end of the first portion.

3 . The air deflector of claim 1 , wherein the plurality of protrusions includes a plurality of triangular teeth extending outward from the first end of the first portion.

4 . The air deflector of claim 1 , wherein the plurality of protrusions of the second portion extend outward from the first end of the first portion in a direction away from the first portion.

5 . The air deflector of claim 4 , wherein the plurality of protrusions include a plurality of tapered teeth.

6 . The air deflector of claim 5 , wherein each tapered tooth includes a top surface, an opposite bottom surface, a first side surface and an opposite second side surface, and wherein the top surface and bottom surface are substantially parallel as the tapered tooth extends outward from the first end of the first portion and the first side surface and the second side surface taper toward each other as the tapered tooth extends outward from the first end of the first portion.

7 . The air deflector of claim 5 , wherein each tapered tooth includes a top surface, an opposite bottom surface, a first side surface and an opposite second side surface, and wherein the first side surface and the second side surface are substantially parallel as the tapered tooth extends outward from the first end of the first portion and the top surface and the bottom surface taper toward each other as the tapered tooth extends outward from the first end of the first portion.

8 . The air deflector of claim 1 , wherein the airfoil-shaped blade is a wind turbine blade.

9 . An air deflector, comprising:

a first portion, the first portion being substantially rectangular and having a first end distal to a surface from which the air deflector extends and a second end proximal to the surface from which the air deflector extends, the first portion having a substantially planar surface; and

a second portion arranged along the first end of the first portion, the second portion including a plurality of protrusions extending outward from the second portion and extending substantially perpendicular to the substantially planar surface of the first portion,

wherein the air deflector is deployable from a first position recessed within an airfoil-shaped device to a second position extending outward from the airfoil-shaped device.

10 . The air deflector of claim 9 , wherein the plurality of protrusions includes a plurality of triangular teeth extending outward from the first end of the first portion.

11 . The air deflector of claim 9 , wherein the plurality of protrusions includes a plurality of tapered teeth.

12 . The air deflector of claim 11 , wherein each tapered tooth includes a top surface, an opposite bottom surface, a first side surface and an opposite second side surface, and wherein the top surface and bottom surface are substantially parallel as the tapered tooth extends outward from the first end of the first portion and the first side surface and the second side surface taper toward each other as the tapered tooth extends outward from the first end of the first portion.

13 . The air deflector of claim 11 , wherein each tapered tooth includes a top surface, an opposite bottom surface, a first side surface and an opposite second side surface, and wherein the first side surface and the second side surface are substantially parallel as the tapered tooth extends outward from the first end of the first portion and the top surface and the bottom surface taper toward each other as the tapered tooth extends outward from the first end of the first portion.

14 . The air deflector of claim 9 , wherein the airfoil-shaped device is at least one of: a wind turbine blade, a helicopter blade, and an aircraft lifting surface.

15 . A wind turbine, comprising:

a rotor having an airfoil-shaped blade, the airfoil-shaped blade including an air deflector, the air deflector being movable between a first position in which the air deflector is recessed within the airfoil-shaped blade and a second position in which the air deflector extends outwardly from an exterior surface of the airfoil-shaped blade, the air deflector further including:

a first portion, the first portion being substantially rectangular and having a first end distal to a surface from which the air deflector extends and a second end proximal to the surface from which the air deflector extends; and

a second portion arranged vertically above the first portion along the first end of the first portion, the second portion including a first section having a substantially rectangular shape and a second section extending from the first section and including a plurality of protrusions extending outward therefrom; and

a controller configured to extend the air deflector from the first position to the second position.

16 . The wind turbine of claim 15 , wherein the second portion is aligned with the first portion.

17 . The wind turbine of claim 15 , wherein the second portion extends in a direction substantially perpendicular to the first portion.

18 . The wind turbine of claim 15 , wherein the first portion further includes a plurality of apertures extending through the first potion.

19 . The wind turbine of claim 15 , wherein the plurality of protrusions include a plurality of scallops.

20 . The wind turbine of claim 15 , wherein the plurality of protrusions include a plurality of tapered teeth.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 15, 2017
From: FRONTIER WIND, LLC
To: GE INFRASTRUCTURE TECHNOLOGY, LLC
Reel/Frame 041718/0336 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 8, 2015
From: TIAN, QING; KHAN, JEHAN Z.; BAKER, JONATHON P.
To: FRONTIER WIND, LLC
Reel/Frame 035362/0260 →