Fastener openings for stress distribution

1. A mating structure, comprising:

a fastener opening defined by the mating structure and extending through the mating structure, wherein the fastener opening comprises:

a circular portion defined by the mating structure and comprising a first radius of curvature,

a first slot portion located in the mating structure, defined by radially spaced proximal and distal walls, and extending from the circular portion, the first slot portion continuous with the circular portion,

an end portion on the first slot portion, the end portion comprising a second radius of curvature less than the first radius of curvature, and

a second slot portion located in the mating structure, defined by radially spaced proximal and distal walls, and extending from the circular portion, the second slot portion comprising a third radius of curvature less than the first radius of curvature, wherein the circular portion is located between the first slot portion and the second slot portion, wherein the mating structure comprises a gas turbine rotor body, wherein the first slot portion and the second slot portion comprise a curvature defined by a radius extending from a center of one of the first slot portion or the second slot portion to an engine central longitudinal axis, and wherein the circular portion, the first slot portion, and the second slot portion are defined in a single plane perpendicular to the central longitudinal axis.

2. The mating structure of claim 1 , wherein the proximal and distal walls defining the first slot portion are tangential to a second wall of the mating structure defining the end portion.

3. The mating structure of claim 2 , wherein the circular portion is configured to retain a fastener.

4. The mating structure of claim 2 , wherein the first slot portion and the second slot portion comprise a uniform width.

5. A structure configured to rotate about an axis, comprising:

a fastener opening comprising:

a circular portion defined by the structure and comprising a first radius of curvature,

a first slot portion located in the structure, defined by radially spaced proximal and distal walls, and extending from the circular portion circumferentially relative to the axis, the first slot portion continuous with the circular portion,

an end portion on the first slot portion comprising a second radius of curvature less than the first radius of curvature, wherein the proximal and distal walls defining the first slot portion are tangential to a second wall of the structure defining the end portion, and

a second slot portion located in the structure, defined by radially spaced proximal and distal walls, and extending from the circular portion circumferentially relative to the axis, the second slot portion comprising a third radius of curvature less than the first radius of curvature, wherein the first slot portion joins the circular portion opposite the second slot portion, wherein the structure comprises a gas turbine rotor body, wherein the first slot portion and the second slot portion comprise a curvature defined by a radius extending from a center of one of the first slot portion or the second slot portion to the axis, and wherein the circular portion, the first slot portion, and the second slot portion are defined in a single plane perpendicular to the axis.

6. The structure of claim 5 , wherein the circular portion is configured to retain a fastener radially relative to the axis.

7. The structure of claim 6 , wherein the circular portion is configured to retain the fastener circumferentially relative to the axis.

8. The structure of claim 5 , wherein the first slot portion and the second slot portion comprise a uniform width in a radial direction relative to the axis.

9. The structure of claim 8 , wherein a radial surface of the structure comprises a tapered surface disposed around at least a portion of the fastener opening.

10. A rotating component of a gas turbine engine, comprising:

a rotor of a compressor section configured to rotate about an axis;

a rotating structure adjacent the rotor;

a fastener passing through a fastener opening defined by at least one of the rotor or the rotating structure, wherein the fastener opening comprises:

a circular portion comprising a first radius of curvature and configured to retain the fastener circumferentially relative to the axis,

a first slot portion defined by radially spaced proximal and distal walls and extending from the circular portion circumferentially relative to the axis, the first slot portion continuous with the circular portion,

an end portion on the first slot portion comprising a second radius of curvature less than the first radius of curvature, wherein the proximal and distal walls defining the first slot portion are tangential to a second wall of the end portion, and

a second slot portion defined by radially spaced proximal and distal walls and extending from the circular portion circumferentially relative to the axis, the second slot portion comprising a third radius of curvature less than the first radius of curvature, wherein the circular portion is located between the first slot portion and the second slot portion,

wherein the first slot portion and the second slot portion comprise a curvature defined by a radius extending from a center of one of the first slot portion or the second slot portion to the axis, and wherein the circular portion the first slot portion, and the second slot portion are defined in a single plane perpendicular to the axis.

11. The rotating component of claim 10 , wherein the first slot portion and the second slot portion comprise a uniform width in a radial direction relative to the axis.

12. The rotating component of claim 11 , wherein the uniform width of the first slot portion and the second slot portion is less than a diameter of the circular portion.