The present disclosure provides a tuning system for tuning the operation of a gas turbine. The system comprises operational turbine controls (30) for controlling operational control elements of the turbine, including at least one of turbine fuel distributi...

An aft liner seal (20) for a combustor for a gas turbine includes an inner shell (30) having an inner and outer surface and central axis. The aft liner seal has an outer shell (38) positioned over the inner shell that has an inner and outer surface and cen...

The present invention is spray system such as a nozzle array, for more effectively and efficiently delivering liquid spray to air before its intake into an engine, a power augmentation system for an engine comprising the spray system and a method for more ...

A method and system augments shaft output of gas turbine engines that can be used in multiple modes of operation. The system comprises a washing unit capable of injecting atomized water into the gas turbine engine, thereby obtaining a release of fouling ma...