Turbine airfoil having cooling hole arrangement
A turbine airfoil includes a body that has inner and outer platforms and an airfoil section that extends between the inner and outer platforms. Cooling holes define external breakout points from the body. The external breakout points are located in accordance with Cartesian coordinates of at least points 1 through 11, 193 through 201, and 268 through 275 set forth in Table 1 herein.
1. A turbine airfoil comprising:
a body having inner and outer platforms and an airfoil section extending between the inner and outer platforms; and
cooling holes that define external breakout points from the body, the external breakout points being located in accordance with Cartesian coordinates of at least points 1 through 11, 193 through 201, and 268 through 275 set forth in Table 1.
2. The turbine airfoil as recited in claim 1 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 12 through 55 set forth in Table 1.
3. The turbine airfoil as recited in claim 1 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 56 through 102 set forth in Table 1.
4. The turbine airfoil as recited in claim 1 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 103 through 192 set forth in Table 1.
5. The turbine airfoil as recited in claim 4 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 202 through 267 set forth in Table 1.
6. The turbine airfoil as recited in claim 5 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 276 through 293 set forth in Table 1.
7. A gas turbine engine comprising:
a compressor section;
a combustor; and
a turbine section, the turbine section including an array of turbine airfoils, each turbine airfoil comprising:
a body having inner and outer platforms and an airfoil section extending between the inner and outer platforms, and
cooling holes that define external breakout points from the body, the external breakout points being located in accordance with Cartesian coordinates of at least points 1 through 11, 193 through 201, and 268 through 275 set forth in Table 1.
8. The gas turbine engine as recited in claim 7 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 12 through 55 set forth in Table 1.
9. The gas turbine engine as recited in claim 7 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 56 through 102 set forth in Table 1.
10. The gas turbine engine as recited in claim 7 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 103 through 192 set forth in Table 1.
11. The gas turbine engine as recited in claim 10 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 202 through 267 set forth in Table 1.
12. The gas turbine engine as recited in claim 11 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 276 through 293 set forth in Table 1.
13. A turbine airfoil comprising:
a body having inner and outer platforms and an airfoil section extending between the inner and outer platforms; and
cooling holes that define external breakout points from the body, the external breakout points being located in accordance with Cartesian coordinates of at least points 1 through 11 and 193 through 201 set forth in Table 1.
14. The turbine airfoil as recited in claim 13 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 12 through 55 set forth in Table 1.
15. The turbine airfoil as recited in claim 14 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 56 through 102 set forth in Table 1.
16. The turbine airfoil as recited in claim 15 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 103 through 146 set forth in Table 1.
17. The turbine airfoil as recited in claim 16 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 147 through 192 set forth in Table 1.
18. The turbine airfoil as recited in claim 17 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 268 through 275 set forth in Table 1.
19. The turbine airfoil as recited in claim 18 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 202 through 267 set forth in Table 1.
20. The turbine airfoil as recited in claim 19 , wherein the cooling holes having external breakout points in accordance with Cartesian coordinates of points 276 through 293 set forth in Table 1.