The gas turbine engine (1) comprises a compressor (2), a combustion system (3) and a turbine (4). The combustion system (3) comprises a heat exchanger (6) for heating compressed air from the compressor (2) to a predefined temperature, a burner (7) for mixi...

A method for operating a gas turbine assembly for a power plant comprises the steps of:- providing a gas turbine assembly (1) comprising a compressor (2), a combustor assembly (4), a turbine (5) and an generator; the compressor (2), the turbine (5) and the...

A gas turbine engine includes an annular combustion chamber (7) and a plurality of combustors (6) communicating with the annular combustion chamber (7). Each combustor (6) defines a respective gas flow path (20) along a respective combustor axis (C) and ha...

A gas turbine engine includes a combustor assembly (5) having a plurality of can combustor units (8) and a control unit (20). Each combustor unit (8) has a first-stage combustor (12), a second-stage combustor (13) and a mixer (15), arranged between the fir...

A gas turbine for power plant; the gas turbine comprising: at least a turbine provided with a first row of stator vanes configured for guiding an hot gas flow; each vane comprising a platform; a combustor comprising an inner casing (52); a seal arrangement...

A method for controlling a sequential combustor (10) of a gas turbine engine (2) includes the method comprising supplying the first combustor stage (12) of the sequential combustor (10) with a first air/fuel mixture (M1) and supplying a second combustor st...

A combustor assembly (3) for a gas turbine assembly (1) comprising: • at least one combustor unit (10) provided with a premix combustor (15); • a water/steam injection assembly (48) comprising a water/steam source (49) and a water/steam circuit (50) co...