An assembly (200) of a gas turbine engine (20) includes a low pressure compressor (44), a high pressure compressor (52), an intermediate case (45) between the low pressure compressor (44) and the high pressure compressor (52), and a cleaning apparatus (70)...

A turbine engine (20) with an axis (22) includes a fan section (28), a turbine engine core (34), a bypass flowpath (46; 56), an engine housing (36), an evaporator (112), a condenser (113) and a core flowpath (62). The turbine engine core (34) is configured...

An axial compressor that can remove an attachment within a groove of a casing and recover an effect of suppressing stall on rotor blades, and a gas turbine provided with the axial compressor, are provided. The axial compressor includes a compressor body 6 ...

The present application provides a turbine inlet air system (100). The turbine inlet air system (100) may include a small droplet coalescer (230), a moisture eliminator (220) positioned about the small droplet coalescer (230), and a filter (210) downstream...

A gas turbine electric power generation equipment comprises: a humidifier (3) for increasing at least one of a quantity of steam, relative humidity, and absolute humidity of air: a combustor (5) for generating combustion gas by humidified air obtained by s...

The present invention relates to an air humidifier for adding moisture to a working medium of a gas turbine for humidification, and gas turbine electric power generation equipment for driving the gas turbine by the working medium of high moisture to genera...