Abstract: The present invention relates to a gas storage power station (1) having a turbine group (3) and a compressor group (4). The turbine group (3) has at least one turbine (5, 6) and a generator (10). During normal operation of the turbine group (3), the generator (10) emits power directly to a main load (11). The compressor group (4) has at least one compressor (12) and one electric motor (15). The gas storage power station (1) furthermore has a power consumption device (20), which can be activated in order to consume turbine and/or generator power.

Abstract: The invention relates to a power plant (1), with at least one turbo group (2) comprising at least one turbine (3) and at least one main burner (5) which is arranged upstream of the turbine (3), with at least one recuperator (11) which is arranged, on the one hand, in a first flow path (15) leading gas toward the turbo group (2) and, on the other hand, in a second flow path (12) leading the gas away from the turbo group (2), with at least one auxiliary burner (19) which is arranged outside the second flow path (12) and which is connected on the outlet side, at or upstream of the recuperator (11), to the second flow path (12).

Abstract: The invention provides a method of operating a gas turbine arranged in a power generation system and comprising a source of compressed air, a combustor having a combustion chamber and multiple burners. A gas turbine controller controls the activation and deactivation of the single burners and/or burner groups according to a switching criterion that is proportional to the difference between a combustion chamber air inlet temperature and a temperature downstream of the combustion chamber. The switching criterion according to the invention fully accounts for large temperature fluctuations of the combustion chamber inlet air, which then result in only relatively small variations in burner equivalence ratio. The invention is particularly suited for application in compressed air energy power generation plants.

Abstract: The invention relates to a method for starting a power plant (1), in particular a gas storage power plant, with the following steps: S1: ignition of an auxiliary combustion chamber (19), S2: operation of the auxiliary combustion chamber (19) in such a way that the consequently heated gas introduced into a first flow path (13) has a temperature which is below a self-ignition temperature of a fuel/oxidizer/gas mixture delivered to the main combustion chamber (5) for starting the latter, S3: operation of the auxiliary combustion chamber (19) according to step S2, until a recuperator (12) has a predetermined preheating temperature, S4: Starting of a turbine (3) and ignition of the main combustion chamber (5).

Abstract: The invention provides a method of operating a gas turbine arranged in a power generation system and comprising a source of compressed air, a combustor having a combustion chamber and multiple burners. A gas turbine controller controls the activation and deactivation of the single burners and/or burner groups according to a switching criterion that is proportional to the difference between a combustion chamber air inlet temperature and a temperature downstream of the combustion chamber. The switching criterion according to the invention fully accounts for large temperature fluctuations of the combustion chamber inlet air, which then result in only relatively small variations in burner equivalence ratio. The invention is particularly suited for application in compressed air energy power generation plants.

Abstract: The present invention relates to a gas storage power station (1) having a turbine group (3) and a compressor group (4). The turbine group (3) has at least one turbine (5, 6) and a generator (10). During normal operation of the turbine group (3), the generator (10) emits power directly to a main load (11). The compressor group (4) has at least one compressor (12) and one electric motor (15). The gas storage power station (1) furthermore has a power consumption device (20), which can be activated in order to consume turbine and/or generator power.

Abstract: The present invention relates to a method for cooling the blades/vanes of a main turbine 3 of a gas storage power plant 1, comprising at least:

Abstract: The invention relates to a power plant (1),

Abstract: The invention relates to a method for starting a power plant (1), in particular a gas storage power plant, with the following steps: