| 摘要 |
<p>A system for sealing a gas path in a turbine (10) includes a stator ring segment (30), a shroud segment (40) adjacent to the stator ring segment (30), and a first load-bearing surface (62) between the stator ring segment (30) and the shroud segment (40). A first non-metallic gasket (70) is in contact with the first load-bearing surface (62) between the stator ring segment (30) and the shroud segment (40). A method for sealing a gas path in a turbine (10) includes placing a non-metallic gasket (70) between any two of a stator ring segment (30), a shroud segment (40), and a casing (12).</p> |
