Wind turbine pitch bearing with line contact rolling elements

Patent metadata

Field	Value
Publication number	US-10677290-B2
Application number	US-201715783590-A
Country	US
Kind code	B2
Filing date	Oct 13, 2017
Priority date	Oct 13, 2017
Publication date	Jun 9, 2020
Grant date	Jun 9, 2020

Abstract

A pitch bearing for coupling a rotor blade to a hub of a wind turbine includes an outer race configured to be coupled to the hub, an inner race rotatable relative to the outer race and configured to be coupled to the rotor blade, and a first plurality of line contact rolling elements. The outer race defines a first outer raceway wall and the inner race defines a first inner raceway wall. The first plurality of line contact rolling elements is disposed between the first inner and outer raceway walls. Each of the plurality of line contact rolling elements defines a predetermined contact angle. The predetermined contact angle is defined as an angle between a reference line extending perpendicular to a longitudinal axis of one of the plurality of line contact rolling elements and a reference line extending parallel to a horizontal plane of the pitch bearing. Further, the predetermined contact angle includes angles between 0 degrees (°) and 90°.

First claim

What is claimed is:

1. A pitch bearing for coupling a rotor blade to a hub of a wind turbine, the pitch bearing comprising:
an outer race configured to be coupled to the hub, the outer race defining a first outer raceway wall comprising a plurality of first protrusions;
an inner race rotatable relative to the outer race and configured to be coupled to the rotor blade, the inner race defining a first inner raceway wall comprising a plurality of second protrusions; and,
a first plurality of line contact rolling elements disposed between the first inner and outer raceway walls such that one of each of the plurality of first and second protrusions fit at least partially within one of the first plurality of line contact rolling elements so as to secure the first line contact rolling element in place, the first plurality of line contact rolling elements comprising tapered rolling elements or cylindrical rolling elements,
wherein each of the first plurality of line contact rolling elements defines a predetermined contact angle, the predetermined contact angle defined as an angle between a reference line extending perpendicular to a longitudinal axis of one of the first plurality of line contact rolling elements and a reference line extending parallel to a horizontal plane of the pitch bearing, the predetermined contact angle comprising angles between 0 degrees (°) and 90°.

2. The pitch bearing of claim 1 , wherein the outer race defines a second outer raceway wall and the inner race defines a second inner raceway wall, the pitch bearing further comprising a second plurality of line contact rolling elements disposed between the second inner and outer raceway walls, the second plurality of line contact rolling elements comprising tapered rolling elements or cylindrical rolling elements.

3. The pitch bearing of claim 2 , wherein the first and second plurality of line contact rolling elements comprise tapered rolling elements, and wherein reference lines extending parallel to the longitudinal axes of the first and second plurality of tapered rolling elements converge at a common point of the pitch bearing and define a taper angle, the taper angle configured to minimize slip of the tapered rolling elements.

4. The pitch bearing of claim 3 , wherein the taper angle comprises angles ranging from about 0.25° to about 6°.

5. The pitch bearing of claim 2 , further comprising a raceway rib extending between the first and second plurality of rolling elements.

6. The pitch bearing of claim 1 , further comprising at least one additional plurality of rolling elements.

7. A pitch bearing for coupling a rotor blade to a hub of a wind turbine, the pitch bearing comprising:
an outer race configured to be coupled to the hub, the outer race defining a first outer raceway wall comprising a plurality of first protrusions;
an inner race rotatable relative to the outer race and configured to be coupled to the rotor blade, the inner race defining a first inner raceway wall comprising a plurality of second protrusions; and,
a first plurality of line contact rolling elements disposed between the first inner and outer raceway walls such that one of each of the plurality of first and second protrusions fit within one of the first plurality of line contact rolling elements so as to secure the first line contact rolling element in place, the first plurality of line contact rolling elements comprising tapered rolling elements or cylindrical rolling elements,
wherein each of the first plurality of line contact rolling elements defines a predetermined contact angle, the predetermined contact angle defined as an angle between a reference line extending perpendicular to a longitudinal axis of one of the first plurality of line contact rolling elements and a reference line extending parallel to a horizontal plane of the pitch bearing, the predetermined contact angle comprising non-0° angles and non-90° angles.

8. The pitch bearing of claim 7 , wherein the outer race defines a second outer raceway wall and the inner race defines a second inner raceway wall, the pitch bearing further comprising a second plurality of line contact rolling elements disposed between the second inner and outer raceway walls, the second plurality of line contact rolling elements comprising tapered rolling elements or cylindrical rolling elements.

9. The pitch bearing of claim 8 , wherein the first and second plurality of line contact rolling elements comprise tapered rolling elements, and wherein reference lines extending parallel to the longitudinal axes of the first and second plurality of tapered rolling elements converge at a common point of the pitch bearing and define a taper angle, the taper angle configured to minimize slip of the tapered rolling elements.

10. The pitch bearing of claim 9 , wherein the taper angle comprises angles ranging from about 0.25° to about 6°.

11. The pitch bearing of claim 7 , further comprising at least one additional plurality of rolling elements.

12. The pitch bearing of claim 8 , further comprising a raceway rib extending between the first and second plurality of rolling elements.

13. A slewing ring bearing for a wind turbine, the slewing ring bearing comprising:
an outer race;
an inner race rotatably coupled to the outer race, the inner race being positioned relative to the outer races such that at least one raceway is defined between the inner and outer races, the at least one raceway comprising a plurality of first protrusions and a plurality of second protrusions; and,
a plurality of line contact rolling elements spaced circumferentially around the at least one raceway such that one of each of the plurality of first and second protrusions fit within one of the plurality of line contact rolling elements so as to secure the line contact rolling element in place, the plurality of line contact rolling elements comprising tapered rolling elements or cylindrical rolling elements,
each of the plurality of line contact rolling elements defining a predetermined contact angle, the predetermined contact angle defined as an angle between a reference line extending perpendicular to a longitudinal axis of one of the plurality of line contact rolling elements and a reference line extending parallel to a horizontal plane of the pitch bearing, the predetermined contact angle comprising non-0° angles and non-90° angles.

14. The slewing ring bearing of claim 13 , wherein the slewing ring bearing comprises at least one of a pitch bearing or a yaw bearing of a wind turbine.

Assignees

• Gen Electric

Inventors

• Birkenstock Joseph Edward
• Gobeli William Max
• Minadeo Adam Daniel

Classifications

• F16C2300/14

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

• Y02E10/721

  Cross-Sectional Technologies · mapped topic

• F16C33/366

  Tapered rollers, i.e. rollers generally shaped as truncated cones · CPC title

• F16C2360/31

  Wind motors · CPC title

• Y02E10/74

  Wind turbines with rotation axis perpendicular to the wind direction · CPC title