Rounded radial snap configuration for a gas turbine engine cover plate
A rotating machine includes a plurality of rotors. Each of the rotors includes a rotor bore protruding radially inward from a platform. A ring shaped cover plate is interfaced with each rotor bore via at least one snap. The at least one snap includes a first arm extending from the cover plate and having a convex facing contact surface, and multiple second arms extending axially from each rotor bore and having contact surfaces facing the convex surface.
1. A rotating machine comprising:
a plurality of rotors, each of the rotors including a rotor bore protruding radially inward from a platform,
a ring shaped cover plate interfaced with each rotor bore via at least one snap;
the at least one snap comprising a first arm extending from the cover plate and having a convex facing contact surface, and a plurality of second arms extending axially from each rotor bore and having contact surfaces facing the convex surface;
wherein the convex facing contact surface is a radially outward facing contact surface and the contact surfaces of the second arms are radially inward facing contact surfaces;
wherein at least one of the radially inward facing contact surfaces and the radially outward facing contact surface includes at least one of a feature intruding into the surface and a feature extruding from the surface; and
wherein each radially inward facing contact surface is concave at a position where the radially inward facing contact surface contacts the corresponding radially outward facing contact surface.
2. The rotating machine of claim 1 , wherein the convex radially outward facing contact surface is defined by an arc having a constant radius.
3. The rotating machine of claim 1 , wherein the convex radially outward facing contact surface is defined by an arc having a variable radius.
4. The rotating machine of claim 3 , wherein the convex radially outward facing contact surface is biased away from the cover plate and towards each rotor bore.
5. The rotating machine of claim 3 , wherein the convex radially outward facing contact surface is biased toward the cover plate and away from each rotor bore.
6. The rotating machine of claim 3 , wherein a forward most position of the convex radially outward facing contact surface has the smallest radius and a downstream most position of the surface has the largest radius.
7. The rotating machine of claim 3 , wherein a forward most position of the convex radially outward facing contact surface has the largest radius and a downstream most position of the surface has the smallest radius.
8. The rotating machine of claim 1 , wherein a curvature of each radially inward facing contact surface matches a curvature of the radially outward facing contact surface.
9. The rotating machine of claim 1 , wherein a curvature of the radially inward facing contact surface has a larger radius than a curvature of the radially outward facing contact surface.
10. The rotating machine of claim 1 , wherein each of the radially inward facing contact surfaces and the radially outward facing contact surface includes the at least one of the feature intruding into the surface and the feature extruding from the surface.
11. The rotating machine of claim 1 , wherein the rotating machine is a gas turbine engine, and wherein each of the rotors and the cover plate are components of a turbine stage of the gas turbine engine.
12. The rotating machine of claim 1 , wherein the radially outward facing contact surface includes the feature intruding into the surface, and the feature intruding into the surface intrudes into the convex radially outward facing contact surface.
13. The rotating machine of claim 1 , wherein the radially outward facing contact surface includes the feature extruding from the surface, and the feature extruding from the surface protrudes from the convex radially outward facing contact surface.
14. The rotating machine of claim 1 , wherein the radially outward facing contact surface extends a full circumferential length of the at least one snap.