METHOD AND DEVICE FOR ASSEMBLING GAS TURBINE ENGINE

摘要

PROBLEM TO BE SOLVED: To provide a stator vane assembly body 52 for a gas turbine engine 10. SOLUTION: This stator vane assembly body 52 includes a plurality of stator vane doublets 80 arranged at an interval in the circumferential direction. Each doublet includes a pair of stator vanes 66 connected mutually at respective outer side stator vane platforms 70 of each stator vane. Each stator vane platform is constituted to connect each doublet with a vane rail 88 extended from a compressor casing 36 extending in the circumferential direction at least partially around the stator vane assembly body slidably. COPYRIGHT: (C)2006,JPO&NCIPI