Pitch bearing assembly with stiffener

Patent metadata

Field	Value
Publication number	US-9951815-B2
Application number	US-201313928734-A
Country	US
Kind code	B2
Filing date	Jun 27, 2013
Priority date	Jun 27, 2013
Publication date	Apr 24, 2018
Grant date	Apr 24, 2018

Abstract

A pitch bearing assembly for a wind turbine may include an outer race and an inner race rotatable relative to the outer race. The inner race may define an inner circumference and may include a plurality of gear teeth around the inner circumference. The inner race may also include a circumferential flange extending at least partially around the inner circumference. In addition, the pitch bearing assembly may include a stiffener coupled to the circumferential flange.

First claim

What is claimed is:

1. A pitch bearing assembly a wind turbine, the pitch bearing assembly comprising:
an outer race;
an inner race rotatable relative to the outer race, the inner race defining an inner circumference and including a plurality of gear teeth around the inner circumference, the inner race further including a circumferential flange extending at least partially around the inner circumference, the circumferential flange extending radially inwardly relative to the inner race such that a top surface of the circumferential flange is coplanar with a top surface of the inner race, the top surface of the inner race configured to abut a root end of a rotor blade of the wind turbine when the rotor blade is coupled to the inner race; and
a stiffener coupled to the circumferential flange,
wherein the stiffener extends outwardly from the top surface of the circumferential flange such that the stiffener is configured to be received axially within an interior of the rotor blade relative to a plane defined by the root end of the rotor blade.

2. The pitch bearing assembly of claim 1 , wherein the circumferential flange is spaced apart axially from a top end of the gear teeth.

3. The pitch bearing assembly of claim 1 , wherein the circumferential flange is ring-shaped and extends around the entire inner circumference of the inner race.

4. The pitch bearing assembly of claim 1 , wherein the circumferential flange is formed from a plurality of flange segments spaced apart circumferentially around the inner circumference of the inner race.

5. The pitch bearing assembly of claim 1 , wherein the stiffener includes a ring-shaped mounting flange and a stiffening web extending within the mounting flange.

6. The pitch bearing assembly of claim 5 , wherein the stiffening web defines a planar profile or a non-planar profile.

7. The pitch bearing assembly of claim 6 , wherein the stiffening web is formed from at least one stiffening arm, the stiffening arm including a first radially extending portion and a second radially extending portion spaced apart axially from the first radially extending portion.

8. The pitch bearing assembly of claim 5 , wherein the stiffening web defines a solid cross-sectional profile or a non-solid cross-sectional profile.

9. The pitch bearing assembly of claim 1 , wherein the circumferential flange includes a first flange segment and a second flange segment, the stiffener being coupled between the first and second flange segments.

10. The pitch bearing assembly of claim 1 , wherein the circumferential flange is separate and spaced apart from the gear teeth along the inner circumference of the inner race.

11. A rotor blade assembly for a wind turbine, comprising:
a rotor blade including a body extending between a blade root and a blade tip, the blade root including a root end defining a plane;
a pitch bearing coupled to the blade root, the pitch bearing including an outer race and an inner race rotatable relative to the outer race, the inner race defining an inner circumference and including a plurality of gear teeth around the inner circumference, the inner race further including an integrally formed circumferential flange extending at least partially around the inner circumference, the circumferential flange extending radially inwardly relative to the inner race such that a top surface of the circumferential flange is coplanar with a top surface of the inner race, the top surface of the inner race configured to abut the root end of the blade root; and
a stiffener coupled to the circumferential flange,
wherein the stiffener extends outwardly from the top surface of the circumferential flange such that the stiffener is received axially within an interior of the rotor blade relative to the plane defined by the root end of the rotor blade.

12. The rotor blade assembly of claim 11 , wherein the circumferential flange is spaced apart axially from the gear teeth.

13. The rotor blade assembly of claim 11 , wherein the circumferential flange is separate and spaced apart from the gear teeth along the inner circumference of the inner race.

Assignees

• Gen Electric

Inventors

• Minadeo Adam Daniel
• Gevers William Francis
• Pine Robert Davis
• Schubert Andreas

Classifications

• F16C2300/14

  Large applications, e.g. bearings having an inner diameter exceeding 500 mm · CPC title

• F16C35/042

  Housings for rolling element bearings for rotary movement · CPC title

• Y02E10/721

  Cross-Sectional Technologies · mapped topic

• F16C19/18

  with two or more rows of balls · CPC title

• F16C35/045

  with a radial flange to mount the housing · CPC title