The gas turbine plant (1) comprises a compressor (2), a first combustion chamber (6) followed by a high pressure turbine (4), a second combustion chamber (10) and a low pressure turbine (5). In the first combustion chamber (6) a first gaseous fuel (8) is i...

A method for operating a gas turbine engine (10) includes channeling compressed airflow (53) discharged from a first compressor (14) through an intercooler (50) having a cooling medium flowing therethrough, channeling a working fluid (72) through the inter...

The standard gas turbo group (1) is combined with a compressed gas storage (4) and means to lead the gas mass flow into the gas flow path downstream of the compressor (3). Preferably air is used as the compressed or storage gas instead of water or steam. S...

This invention relates to a recuperator for heating compressed air containing moisture by utilizing exhaust heat. A plate fin type recuperator (60) is provided which can prevent clogging of a channel caused by a drift of liquid phase water even when compre...

Gas turbine plant (1) operating method in which a generator (4) is driven by turbine (2) to produce a current with a predefined frequency (f0) and whereby a combustion air flow (L) is supplied, and the operating frequency (f(t)) is monitored in a time-reso...

A gas turbine engine (10) comprises a second compressor (14), a first compressor (16), a heat exchanger (18), a combustor (20), a first turbine (22), a second turbine (24) and a third turbine (26) arranged in flow series. The first turbine (22) is arranged...