A gas turbine engine (20) includes an intercooling turbine section (24) along an engine axis (X) aft of a fan section (22) and forward of a combustor section (30).

A gas turbine engine (10) includes an intercooling turbine section (24A) to at least partially drive one of a low spool (42') and a high spool (46'). An intercooling turbine section bypass is provided to selectively bypass at least a portion of a core flow...

A gas turbine engine (10) includes a fan section (22) and an intercooling turbine section (24) along an engine axis aft of the fan section (22) and forward of a combustor section (30).

A chiller coil system for an asymmetric gas turbine filter house (10) includes a plurality of chiller coil modules (22) arranged in a substantially vertical array, each chiller coil module provided with a cooled fluid inlet pipe (42-52) and a fluid outlet ...

Method and apparatus for cooling a hydrocarbon stream (520) to produce an at least partially liquefied hydrocarbon stream (530). A cooled main refrigerant stream (245) is further cooled against at least a part of one or more expanded cooled pre-cooling ref...

A method for operating a gas turbine engine (10) including a first compressor (14), a second compressor (16), a combustor (18) and a turbine (20), coupled together in serial flow arrangement. The method includes channeling compressed airflow discharged fro...

The intercooling method is for a gas turbine engine with first (1) and second (2) compressor stages and a combustion chamber (3) and turbine (4). The intercooler (9) is positioned between the two compressor stages. The intercooler is at least partially or ...

The gas turbine assembly has a cooling system for the combustion air, using a suitable coolant (20,21). At least a part of the air mass flow is cooled before or within the compressor (1,2) so that critical temperatures are not breached at critical points (...