Shroud integral type moving blade of a gas turbine

Details Shroud integral type moving blade of a gas turbine Shroud integral type moving blade of a gas turbine

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/20 (2006.01) F01D 11/08 (2006.01)

Patent

CA 2390580

A gas turbine comprises a shroud integral type moving blade and a split ring. The moving blade includes a shroud provided from a leading edge of a tip of a moving blade to a trailing edge and whose outer side surface is provided with a seal fin. A radius of a tip end of the seal fin is substantially equal to a radius of a shroud trailing edge end. The split ring has a structure in which a radius of its inner peripheral surface is slightly larger than a radius of the seal fin tip end and the radius of the shroud trailing edge end.

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