A low pressure turbine, in particular for a gas turbine engine, extends along an axis (3), has an annular conduit (6) for guiding a gas flow and is provided with a plurality of stator arrays of blades and a plurality of rotor arrays of blades; the last of ...

A geared axial multistage expander system and assembly method including a casing (42) and a plurality of stages (R1 to R6). A stage includes a stator part (44) connected to the casing and having plural statoric airfoils (55) and a rotor part (50) configure...

A gas turbine that can effectively cool an axial cavity between a stator blade and a rotor blade and a blade-end surface is provided. In a gas turbine in which a blade-count difference between stator-blade segments (17) of a second-stage stator blade and a...