Air storage gas turbine power station with fluidized bed firing

Claim 2

An air storage gas turbine power station with fluidized bed firing whose gas turbine group comprises a turbine, a compressor, an electrical machine which can be operated alternatively as a generator and an electric motor, a first clutch between the turbine and the electrical machine, a second clutch between the electrical machine and the compressor, an air storage chamber, a coal-fired fluidized bed combustion chamber, a combustion gas duct which communicates the fluidized bed combustion chamber with the turbine, a main air duct; and which communicates an outlet of the compressor with the air storage chamber and communicates both the air storage chamber and the outlet of the compressor with the fluidized bed combustion chamber, a first shut-off valve for selectively shutting-off the outlet of the compressor from said main air duct, a second shut-off valve for selectively shutting-off the air storage chamber from the main air duct, a throttle unit at a location along the main air duct upstream of the fluidized bed combustion chamber and a separator cyclone at a location along the combustion gas duct between the fluidized bed combustion chamber and the turbine, a low load air duct which communicates tapping means on the compressor with a section of the main air duct between the throttle unit and the fluidized bed combustion chamber and a third shut-off valve at a location along the low load air duct.

Claim 3

The air storage gas turbine power station according to claim 1, wherein the compressor has a low pressure compressor stage, a high pressure compressor stage and an intercooler operatively located between the low and high compressor stages and the turbine includes a high pressure turbine stage and a low pressure turbine stage, the second clutch including a mechanically lockable hydraulic torque convertor, a mechanical clutch operatively located between the high pressure turbine stage and the low pressure turbine stage, the tapping means located upstream of the intercooler of the compressor, the main air duct including a heater tube bundle, a high pressure hot air duct and a low pressure hot air duct, the heater tube bundle located in the fluidized bed combustion chamber and arranged so that air flows through the heater tube bundle in a direction opposite to a flow of the fluidized bed, the high pressure hot air duct communicating an outlet of the heater tube bundle with an inlet of the high pressure turbine stage, the low pressure hot air duct communicating an outlet of the high pressure turbine stage with an inlet to a lower region of the fluidized bed combustion chamber, the combustion gas duct communicating an outlet of the fluidized bed combustion chamber with an inlet of the low pressure turbine stage, a separator cyclone at a location along the combustion gas duct, a low load by-pass duct communicating an outlet of the separator cyclone with an exhaust gas duct of the low pressure turbine stage, a low load by-pass valve at a location along the low load by-pass duct, and a regenerator including a counterflow heat exchanger at a location along the main air duct opposite of the second shut-off valve from the air storage chamber, a hot water reservoir and pump means for circulating water from the hot water reservoir through the counterflow heat exchanger alternately in mutually opposed flow directions.

Claim 4

The air storage gas turbine power station according to claim 1, wherein the compressor has a low pressure compressor stage, a high pressure compressor stage and an intercooler operatively located between the low and high pressure compressor stages, and the turbine includes a high pressure stage and a low pressure turbine stage mounted on a common shaft, the second clutch including a mechanically lockable hydraulic torque convertor, the main air duct including a heater tube bundle, a high pressure hot air duct and a low pressure hot air duct, the heater tube bundle located in the fluidized bed combustion chamber and arranged so that air flows through the heater tube bundle in a direction opposite to a flow of the fluidized bed, the high pressure hot air duct communicating an outlet of the heater tube bundle with an inlet of the high pressure turbine stage, the low pressure hot air duct communicating the outlet of the high pressure turbine stage with an inlet to a lower region of the fluidized bed combustion chamber, the combustion gas duct communicating an outlet of the fluidized bed combustion chamber with an inlet of the low pressure turbine stage, a separator cyclone at a location along the combustion gas duct, a low load by-pass duct communicating an outlet of the separator cyclone with an exhaust gas duct of the low pressure turbine stage, a low load by-pass valve at a location along the low load by-pass duct, said gas turbine group further comprising intercoolers in the high pressure compressor stage, a low load turbine drivingly connected with a generator, a high pressure low load hot air duct communicating the high pressure hot air duct to an inlet of the low load turbine, a third control valve at a location along the high pressure low load hot air duct, a low pressure low load hot air duct communicating an outlet of the low load turbine with the lower region of the fluidized bed combustion chamber, a fourth shut-off valve at a location along the high pressure hot air duct, a fifth shut-off valve at a location along the combustion gas duct, a storage air cooler at a location along the main air duct opposite of the second shut-off valve from the air storage chamber and recuperator means for heating high pressure air in the main air duct with heat from the exhaust gas duct.