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The present application provides an impingement cooling system for use with a contoured surface. The impingement cooling system may include an impingement plenum and an impingement plate with a linear shape facing the contoured surface. The impingement surface may include a number of projected area

The present application provides an impingement cooling system for use with a contoured surface. The impingement cooling system may include an impingement plenum and an impingement plate with a linear shape facing the contoured surface. The impingement surface may include a number of projected area thereon with a number of impingement holes having varying sizes and varying spacings.

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1. An impingement cooling system for use with a non-planar contoured surface of gas turbine with multiple irregular depressions and projections, comprising: a nozzle with an impingement plenum in communication with a cooling flow in a cooling conduit, the cooling flow flowing through the impingement

1. An impingement cooling system for use with a non-planar contoured surface of gas turbine with multiple irregular depressions and projections, comprising: a nozzle with an impingement plenum in communication with a cooling flow in a cooling conduit, the cooling flow flowing through the impingement plenum in a first direction;an impingement plate facing the contoured surface;the impingement plate comprising a substantially flat shape;a cover plate positioned substantially parallel to the impingement plate, wherein the impingement plenum comprises a cavity defined between the impingement plate and the cover plate, such that the cooling flow impacts the cover plate and flows through the impingement plate in a second direction;the impingement plate comprising a plurality of projected areas thereon, the projected areas corresponding to the multiple irregular depression and projections of the contoured surface;wherein each of the plurality of projected areas comprises a plurality of impingement holes with varying sizes and varying spacings between the impingement holes for each of the plurality of projected areas. 2. The impingement cooling system of claim 1, wherein the plurality of projected areas comprises a first area with impingement holes of a first size and a second area with impingement holes of a second size. 3. The impingement cooling system of claim 1, wherein the plurality of projected areas comprises a first area with impingement holes of a first spacing and a second area with impingement holes of a second spacing. 4. The impingement cooling system of claim 1, wherein the plurality of projected areas comprises a first area with impingement holes of a first size and a first spacing and a second area with impingement holes of a second size and a second spacing. 5. The impingement cooling system of claim 1, wherein the multiple projections of the contoured surface comprises a plurality of projections with tips positioned at a plurality of distances from the impingement plate. 6. The impingement cooling system of claim 5, wherein the size and the spacing of the plurality of impingement holes in each of the plurality of projected areas varies with the distance to an opposed contoured area. 7. The impingement cooling system of claim 1, wherein the impingement plate maintains the contoured surface with substantially constant heat transfer coefficients thereacross. 8. A turbine, comprising: a turbine nozzle;an impingement cooling system;the impingement cooling system comprising a plurality of impingement holes with a plurality of sizes and spacings between the plurality of impingement holes, and an impingement plenum with an impingement plate with the plurality of impingement holes therein; anda turbine component positioned about the impingement cooling system;the turbine component comprising a contoured surface with multiple irregular depression and projections, wherein the plurality of impingement holes of the impingement cooling system correspond to the multiple irregular depressions and projections of the contoured surface. 9. The turbine of claim 8, wherein the impingement plate comprises a substantially flat shape. 10. The turbine of claim 8, wherein the impingement plate comprises a grid with a plurality of projected areas. 11. The turbine of claim 10, wherein the plurality of projected areas comprises the plurality of impingement holes therein. 12. The turbine of claim 10, wherein the plurality of projected areas comprises a first area with impingement holes of a first size and a second area with impingement holes of a second size. 13. The turbine of claim 10, wherein the plurality of projected area comprises a first area with impingement holes of a first spacing and a second area with impingement holes of a second spacing. 14. The turbine of claim 10, wherein the plurality of projected areas comprises a first area with impingement holes of a first size and a first spacing and a second area with impingement holes of a second size and a second spacing. 15. The turbine of claim 10, wherein the multiple projections of the contoured surface comprises a plurality of projections with tips positioned at a plurality of distances from the impingement plate. 16. The turbine of claim 8, wherein the impingement cooling system maintains the contoured surface with substantially constant heat transfer coefficients thereacross. 17. A turbine, comprising: a turbine nozzle;an impingement cooling system;the impingement cooling system comprising a linear impingement plate with a plurality of impingement holes with a plurality of sizes and spacings between the plurality of impingement holes, and an impingement plenum with an impingement plate with the plurality of impingement holes therein; anda turbine component positioned about the impingement cooling system;the turbine component comprising a contoured surface such that the impingement cooling system maintains the contoured surface with substantially constant heat transfer coefficients thereacross, wherein the contoured surface comprises multiple irregular depressions and projections, and the plurality of impingement holes of the impingement cooling system correspond to the multiple irregular depressions and projections of the contoured surface. 18. The impingement cooling system of claim 1, wherein the multiple depressions of the contoured surface comprises a plurality of depressions with troughs positioned at a plurality of distances from the impingement plate; and the plurality of impingement holes are positioned such that cooling flow flowing through the impingement holes impacts the contoured surface about the troughs. 19. The turbine of claim 8, wherein the multiple depressions of the contoured surface comprises a plurality of depressions with troughs positioned at a plurality of distances from the impingement plate; and the plurality of impingement holes are positioned such that cooling flow flowing through the impingement holes impacts the contoured surface about the troughs. 20. The turbine of claim 17, wherein the multiple depressions of the contoured surface comprises a plurality of depressions with troughs positioned at a plurality of distances from the impingement plate; and the plurality of impingement holes are positioned such that cooling flow flowing through the impingement holes impacts the contoured surface about the troughs.