Pitch bearing

Patent metadata

Field	Value
Publication number	US-10214284-B2
Application number	US-201314041674-A
Country	US
Kind code	B2
Filing date	Sep 30, 2013
Priority date	Sep 30, 2013
Publication date	Feb 26, 2019
Grant date	Feb 26, 2019

Abstract

A pitch bearing for connecting first and second articles is provided. The first article includes a first curved outer surface and the second article includes a second curved outer surface opposite the first curved outer surface. The pitch bearing includes an axisymmetric structure interposed between the first and second curved outer surfaces. The axisymmetric structure includes compliant layers and stabilizing layers interleaved between the compliant layers. The compliant layers and the stabilizing layers proximate to the first article haves a curvature matching that of the first curved outer surface. The compliant layers and the stabilizing layers proximate to the second article have a curvature matching that of the second curved outer surface. A shear stiffness of each of the stabilizing layers is greater than a shear stiffness of each of the compliant layers.

First claim

What is claimed is:

1. A pitch bearing assembly comprising:
a first article including a unitary body having a first end and a second end, at least one of the first end and the second end having a solid cross-section, the at least one of the first end and the second end including a convex curved outer surface extending along a longitudinal axis of the first article;
a second article including a body portion having a first leg including a first distal end and a second leg including a second distal end, the first and second legs being integrally formed with and extending radially outwardly of the body portion, the body portion including a central passage defining a concave curved inner surface, the central passage being receptive of at least one of the first end and the second end of the unitary body; and
a pitch bearing operatively connects the first article and the second article, the pitch bearing comprising:
an axisymmetric structure interposed between the convex curved outer surface of the first article and the concave curved inner surface of the second article, the axisymmetric structure having a cylindrical shape with a curvature extending along the longitudinal axis and including compliant layers and stabilizing layers interleaved between the compliant layers, wherein the curvature is convex relative to the longitudinal axis,
the compliant layers and the stabilizing layers proximate to the first article have a curvature matching that of the convex curved outer surface of the first article,
the compliant layers and the stabilizing layers proximate to the second article have a curvature matching that of the concave curved inner surface of the second article, and
a shear stiffness of each of the stabilizing layers is greater than a shear stiffness of each of the compliant layers.

2. The pitch bearing assembly according to claim 1 , wherein respective curvatures of the convex curved outer surface of the first article and the concave curved inner surface of the second article are complementary.

3. The pitch bearing assembly according to claim 2 , wherein each of the compliant layers and each of the stabilizing layers have similar curvatures.

4. The pitch bearing assembly according to claim 1 , wherein focal points respectively defined by the convex curved outer surface of the first article and the concave curved inner surface of the second article are within an axial span of the second article.

5. The pitch bearing assembly according to claim 1 , wherein the curvature of the axisymmetric structure extends smoothly and continuously along an entire axial length of the axisymmetric structure and an axial end of the axisymmetric structure is flared outwardly and an axial midpoint of the axisymmetric structure protrudes inwardly.

6. The pitch bearing assembly according to claim 1 , wherein respective curvatures of the convex curved outer surface of the first article and the concave curved inner surface of the second article are spherical.

7. The pitch bearing assembly according to claim 6 , wherein the respective curvatures of each of the compliant layers and each of the stabilizing layers are spherical.

8. The pitch bearing according to claim 1 , wherein each of the compliant layers comprises rubber.

9. The pitch bearing according to claim 1 , wherein the compliant layers and the stabilizing layers have a curvature matching that of the first and second curved outer surfaces.

10. A pitch bearing assembly, comprising:
a first unitary article including a first end and a second end, the first article being rotatable with the first end proximate and operatively coupled to a center of rotation and having a first longitudinal axis and an outer surface extending along the first longitudinal axis with a convex cylindrical shape at the second end extending along a longitudinal axis of the first article;
a second article configured to be attached to the second end of the first article, the second article having a first leg including a first distal end and a second leg including a second distal ends extending radially outwardly of a body having a central passage extending along a second longitudinal axis, the central passage including an inner surface extending along the second longitudinal axis with a concave cylindrical shape;
a torque tube operatively coupled to the center of rotation and to the second article at distal ends of the second article; and
a convex cylindrical axisymmetric structure interposed between the outer surface of the first unitary article and the inner surface of the second unitary article and including compliant layers and stabilizing layers interleaved between the compliant layers,
the compliant layers and the stabilizing layers have respective curvatures matching that of the outer surface of the first unitary article and the inner surface of the second unitary article, and
a shear stiffness of each of the stabilizing layers is greater than a shear stiffness of each of the compliant layers.

11. The pitch bearing assembly according to claim 10 , wherein the first article comprises high strength steel and the second article comprises titanium.

12. The pitch bearing assembly according to claim 10 , wherein the second article is configured for attachment to a component of a rotormachine rotor blade.

13. The pitch bearing assembly according to claim 10 , wherein each of the compliant layers and each of the stabilizing layers have similar curvatures.

14. The pitch bearing assembly according to claim 10 , wherein focal points respectively defined by the outer surface of the first unitary article and the inner surface of the second unitary article are within an axial span of the second article.

15. The pitch bearing assembly according to claim 10 , wherein a curvature of the axisymmetric structure extends smoothly and continuously along an entire axial length of the axisymmetric structure and an axial end of the axisymmetric structure is flared outwardly and an axial midpoint of the axisymmetric structure protrudes inwardly.

16. The pitch bearing assembly according to claim 10 , wherein respective curvatures of the outer surface of the first unitary article and the inner surface of the second unitary article are spherical.

17. The pitch bearing assembly according to claim 16 , wherein the respective curvatures of each of the compliant layers and each of the stabilizing layers are spherical.

18. A pitch bearing assembly, comprising:
a first unitary article including first and second ends, the first article being rotatable with the first end proximate and operatively coupled to a center of rotation and having a first curved outer surface at the second end extending along a longitudinal axis of the first article;
a second article including a first leg having a first distal end and a second leg including a second distal end extending radially outwardly of a body having a central passage, the second article being configured to be attached with coaxial overlap to the second end of the first article, the central passage having a curved inner surface;
a torque tube operatively coupled to the center of rotation and to the second article at distal ends of the second article; and
an axisymmetric structure interposed between the outer surface of the first article and the inner surface of the second article and including compliant layers and stabilizing layers interleaved between the compliant layers,
the compliant layers and the stabilizing layers have respective curvatures matching that of the outer surface of the first article and the inner surface of the se

Assignees

• Sikorsky Aircraft Corp

Inventors

• Hunter David H
• Parsons Eric S
• Nussenblatt Eric Lucien
• Casey Ryan Thomas

Classifications

• B64C27/48

  Root attachment to rotor head · CPC title

• F16F1/393

  with spherical or conical sleeves · CPC title

• B64C27/35 Primary

  having elastomeric joints · CPC title

• F16F1/40

  consisting of a stack of similar elements separated by non-elastic intermediate layers {(F16F9/306 takes precedence; laminated constructions to protect buildings against abnormal external influences, e.g. earthquakes, E04H9/022)} · CPC title