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An improved sealing device for use between a transition duct aft frame and turbine inlet is disclosed. The improved sealing device includes a plurality of corrugated metal seals that are secured to the transition duct aft frame along the arc-like sections of the aft frame. The corrugated seals conta

An improved sealing device for use between a transition duct aft frame and turbine inlet is disclosed. The improved sealing device includes a plurality of corrugated metal seals that are secured to the transition duct aft frame along the arc-like sections of the aft frame. The corrugated seals contact both the transition duct aft frame and turbine inlet to provide a more effective seal and to control the amount of compressor discharge air introduced to cool the turbine vane platforms. In the preferred embodiment, the corrugated seals are coated to reduce wear, fretting, and galling and are used in conjunction with a transition duct thermally free aft frame and pivot bearing mounting system. An alternate embodiment of the seal is also disclosed that utilizes an alternate cooling hole pattern for providing additional cooling air to the turbine vane platform. A further alternate embodiment of the seal incorporates a group of wear reduction coatings from which to select.

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1. A sealing device having a general arc-shape for use between a gas turbine combustor transition duct aft frame and a turbine inlet, said sealing device comprising:a first end;a second end;a centerpoint positioned along said arc-shaped sealing device equidistant between said first and second ends;a

1. A sealing device having a general arc-shape for use between a gas turbine combustor transition duct aft frame and a turbine inlet, said sealing device comprising:a first end;a second end;a centerpoint positioned along said arc-shaped sealing device equidistant between said first and second ends;a plurality of mounting tabs, each of said mounting tabs having a first surface, a second surface, thereby defining a seal thickness there between, and a plurality of mounting holes;a first fold having a first radius R 1 and connected to said mounting tabs;a plurality of flexible corrugations fixed to said first fold, each of said corrugations having two generally parallel walls of length L 2 , each of said walls having at least a feed hole and said walls are interconnected by a second fold, said second fold having a second radius R 2 ;a sealing member fixed to one of said corrugations opposite said first fold and having a third radius R 3 , a third surface, a fourth surface, a plurality of sealing points located along said fourth surface, and a plurality of cooling holes;a seal length;a first coating applied to said first surface of said mounting tabs, said first coating consisting essentially of a primarily Aluminum-Bronze based composition; anda second coating applied to said second folds and said fourth surface of said sealing member as a wear material, said second coating is selected from a group comprising Titanium Aluminum Nitride, Aluminum Titanium Nitride, Titanium Nitride, Stellite 31, and Stellite 694. 2. The sealing device of claim 1 wherein said first coating is applied by cathodic arc deposition. 3. The sealing device of claim 1 wherein said sealing device is fabricated from Inconnel 718. 4. The sealing device of claim 1 wherein said seal thickness is at least 0.015 inches. 5. The sealing device of claim 1 wherein each mounting hole in said mounting tabs has a diameter of at least 0.500 inches. 6. The sealing device of claim 1 wherein said first radius R 1 of said first fold is at least 0.150 inches. 7. The sealing device of claim 1 wherein said corrugations have a length L 2 of at least 0.500 inches and a second radius R 2 of said second fold of at least 0.062 inches. 8. The sealing device of claim 1 wherein said at least one feed hole has a diameter of at least 0.250 inches. 9. The sealing device of claim 1 wherein said third radius R 3 of said sealing member is at least 0.350 inches. 10. The sealing device of claim 1 wherein said plurality of cooling holes of said sealing member have an equal diameter of at least 0.100 inches. 11. The sealing device of claim 1 wherein said cooling holes of said sealing member have a varying diameter wherein the smallest cooling hole diameter is proximate said first and second ends and the largest cooling hole diameter is proximate said centerpoint of said arc-shaped seal. 12. The sealing device of claim 1 wherein said first coating application is applied to said first surface at least 0.003 inches thick. 13. The sealing device of claim 1 wherein said second coating application is applied to said second folds and said fourth surface at a thickness greater than 0.000 inches but less than 0.002 inches. 14. The sealing device of claim 1 wherein said second folds and said fourth surface further include an Aluminum Bronze based overcoating applied at least 0.0003 inches thick over a second coating consisting of either Titanium Aluminum Nitride, Aluminum Titanium Nitride, or Titanium Nitride.