CPC F01D 11/005 (2013.01) [F16J 15/0887 (2013.01); F23R 3/46 (2013.01); F05D 2240/35 (2013.01); F05D 2240/55 (2013.01); F23R 2900/00012 (2013.01)] | 20 Claims |
1. A flexible seal for sealing between two adjacent gas turbine components, the flexible seal comprising:
a forward end, an aft end axially separated from the forward end, and an intermediate portion extending from the forward end to the aft end, the intermediate portion defining a continuous curve in the circumferential direction from the forward end to the aft end, such that the aft end is circumferentially offset from the forward end, wherein the two adjacent gas turbine components are integrated combustor nozzles.
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