GAS TURBINE

摘要

In this gas turbine, at a downstream part of a tail pipe of a combustor, the inner surfaces of a pair of lateral walls facing each other in the circumferential direction of a turbine rotor form inclination surfaces that, going in the downstream axial direction of the tail pipe, incline in a direction approaching the tail pipe of an adjacent other combustor that gradually draws closer, until the inclination surfaces reach the downstream end of the tail pipe.