Gas turbine and repair method therefor

Details Gas turbine and repair method therefor Gas turbine and repair method therefor

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/00 (2006.01) B23P 6/00 (2006.01) F01D 9/02 (2006.01) F23R 3/00 (2006.01) F23R 3/06 (2006.01)

Patent

CA 2342809

A gas turbine has a compressor for compressing air as a working fluid, a combustor for producing combustion gas by mixing fuel with the compressed air, and a turbine for generating a rotating force at the time of expansion of combustion gas. The gas turbine further includes a cylindrical liner; a transition piece for transferring the working fluid from the liner to the turbine; an outlet portion of the transition piece, which has a region parallel with a direction of a rotating shaft of the turbine; cooling holes formed in the region so that intervals thereof are lengthened partially; and a picture frame portion provided to secure stiffness at an outlet of the outlet portion.

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