Turbine blade damper seal
An example turbine includes a turbine disk and a turbine blade. The turbine disk includes a plurality of lugs and a plurality of slots. Each of the plurality of lugs is located between two of the plurality of slots. Each of the plurality of lugs includes a tab that extends radially outwardly from an end of the lug. The tab has a first section having an upper surface and a second section having an upper surface. The upper surface of the first section is inclined greater than the upper surface of the second section, and the upper surface of the first section of the tab defines a contour. The turbine blade includes a root received in one of the plurality of slots and a platform, and the platform has a lower surface defining a contour. When the turbine blade is received in one of the plurality of slots, the lower surface of the platform is located above a portion of the upper surface of the first section of the tab, and the contour of the upper surface of the first section of the tab matches the contour of the lower surface of the platform.
1. A turbine comprising:
a turbine disk including a plurality of lugs and a plurality of slots, wherein each of the plurality of lugs is located between two of the plurality of slots, and each of the plurality of lugs includes a tab that extends radially outwardly from an end of the lug, wherein the tab has first section having an upper surface and a second section having an upper surface, the upper surface of the first section is inclined greater than the upper surface of the second section, and the upper surface of the first section of the tab defines a contour; and
a turbine blade, wherein the turbine blade includes a root received in one of the plurality of slots and a platform, and the platform has a lower surface defining a contour,
wherein, when the turbine blade is received in one of the plurality of slots, the lower surface of the platform is located above a portion of the upper surface of the first section of the tab, and the contour of the upper surface of the first section of the tab matches the contour of the lower surface of the platform.
2. The turbine as recited in claim 1 , wherein an upper surface of each of the plurality of lugs includes an axial groove and a circumferential groove that intersects the axial groove, and the circumferential groove defines a rear surface of the tab.
3. The turbine as recited in claim 2 , wherein the axial groove is substantially perpendicular to the circumferential groove.
4. The turbine as recited in claim 2 , wherein the circumferential groove is deeper than the axial groove.
5. The turbine as recited in claim 2 , wherein the axial groove receives a damper seal located under the platform.
6. The turbine as recited in claim 5 , wherein a portion of the damper seal rests against the rear surface of the tab.
7. The turbine as recited in claim 2 , wherein each of the plurality of lugs extends axially between opposing first and second sides, the tab extending circumferentially along the second side.
8. The turbine as recited in claim 7 , wherein the axial groove extends from the first side to the circumferential groove.
9. The turbine as recited in claim 2 , wherein a depth of the circumferential groove is greater than a depth of the axial groove.
10. The turbine as recited in claim 1 , wherein the upper surface of the first section of the tab is substantially parallel to the lower surface of the platform.
11. The turbine as recited in claim 1 , wherein the respective upper surfaces of the first and second sections meet at a ridge.
12. The turbine as recited in claim 1 , wherein the respective upper surfaces of the first and second sections are inclined towards the ridge.
13. A turbine disk comprising:
a hub;
a plurality of lugs extending radially outward from the hub; and
a plurality of slots, each slot located between a respective pair of the lugs;
wherein a radially outer end of each of the plurality of lugs includes an axial groove, a circumferential groove, and a tab, the axial groove intersecting the circumferential groove, the tab extending radially outwardly and defining a portion of the circumferential groove; and
wherein the tab has a first section having a first upper surface and a second section having a second upper surface, the first and second upper surfaces inclined towards each other and meeting at a ridge.
14. The turbine disk of claim 13 , wherein an incline of the first upper surface is greater than an incline of the second upper surface.
15. The turbine disk of claim 13 , wherein:
each of the plurality of lugs extends axially between opposing first and second sides;
the tab extends circumferentially along the second side.
16. The turbine disk of claim 13 , wherein the axial groove extends from the first side to the circumferential groove.
17. The turbine disk of claim 13 , wherein the axial groove is substantially perpendicular to the circumferential groove.
18. The turbine disk of claim 13 , wherein the lugs comprise a plurality of arms configured to interfit with turbine blades disposed within the slots.
19. The turbine disk of claim 18 , wherein the arms are arranged in a dovetail or fir tree configuration.