Increased capacity spherical lined bearings

1. A method to control feathering movement of a rotor blade, comprising:

attaching the rotor blade to a yoke arm via a first attachment means in a first bearing comprising a first pivoting element and a first housing and via a second attachment means in a second bearing comprising a second pivoting element and a second housing;

forming a first aperture extending longitudinally through the first pivoting element along a centerline of the first bearing, the first attachment means extending longitudinally through the first aperture;

forming a second aperture extending longitudinally through the second pivoting element along a centerline of the second bearing, the second attachment means extending longitudinally through the second aperture;

aligning the first bearing and the second bearing on the yoke arm in a linear fashion;

limiting feathering to a first direction and a second direction;

intersecting the centerline of the first bearing with a longitudinal axis of the yoke arm at only a first point;

intersecting the centerline of the second bearing with the longitudinal axis of the yoke arm at only a second point;

allowing pivoting movement of the rotor blade relative to the yoke arm along the first direction and second direction to compensate for feathering during flight;

notching the first housing with a first set of notches to increase the feathering;

notching the second housing with a second set of notches to increase the feathering; and

contouring the first set of notches and the second set of notches to correspond to an exterior surface of the first attachment means and an exterior surface of the second attachment means, respectively, to increase the feathering.

2. The method of claim 1 , further comprising:

restricting both longitudinal and transverse movement of the rotor blade relative to the yoke arm with the first bearing and the second bearing.

3. The method of claim 1 , wherein the step of aligning the first bearing and the second bearing on the yoke arm in a linear fashion locates the first bearing and the second bearing on a plane.

4. A rotary system, comprising:

a yoke arm;

a rotor blade;

a first bearing comprising a first pivoting element and a first housing, the first bearing being carried by the yoke arm and configured to pivotally secure the rotor blade to the yoke arm;

a second bearing comprising a second pivoting element and a second housing, the second bearing being carried by the yoke arm and configured to pivotally secure the rotor blade to the yoke arm;

a first aperture extending longitudinally through the first pivoting element along a centerline of the first bearing, a first attachment means extending longitudinally through the first aperture;

a second aperture extending longitudinally through the second pivoting element along a centerline of the second bearing, a second attachment means extending longitudinally through the second aperture;

four distinct cutouts located in the first housing; and

four distinct cutouts located in the second housing;

wherein the rotor blade is pivotally secured to the yoke arm by the first attachment means and the second attachment means;

wherein the first bearing and the second bearing together allow feathering movement of the rotor blade relative to the yoke arm during flight in only a first feathering direction and a second feathering direction;

wherein at least two of the four distinct cutouts located in the first housing are contoured to correspond to an exterior surface of the first attachment means to increase feathering;

wherein at least two of the four distinct cutouts located in the second housing are contoured to correspond to an exterior surface of the second attachment means to increase feathering;

wherein the centerline of the first bearing intersects with a longitudinal axis of the yoke arm at only a first point; and

wherein the centerline of the second bearing intersects with the longitudinal axis of the yoke arm at only a second point.

5. The rotary system of claim 4 , wherein the first bearing and the second bearing are both located on a plane.