Stator vane assembly for a gas turbine

摘要

A stator vane assembly for a gas turbine engine includes a plurality of circumferentially-spaced stator vane doublets. Each doublet includes a pair of stator vanes (66) coupled together at a respective outer stator vane platform (70) of each vane. Each stator vane platform is configured to slidably couple each doublet to a vane rail (88) extending from a compressor casing (36) that extends at least partially circumferentially around the stator vane assembly.