A control device for adjusting an amount of fuel to be supplied to a gas turbine based on a rotational speed of the gas turbine, such that a frequency of electric power output by a power generator that generates electric power using the gas turbine is within a given range, includes a load value acquisition unit configured to acquire a load value that is a value of a load applied to the power generator after cutoff of a part of the load applied to the power generator when the part of the load applied to the power generator is cut off, an arithmetic unit configured to calculate an adjusted value that is a value of the load different from the load value by carrying out an arithmetic operation on the load value and a bias, and a command unit configured to adjust the amount of fuel by outputting a first signal for causing the power generator to output electric power corresponding to the adjusted value.

A control device for adjusting an amount of fuel to be supplied to a gas turbine based on a rotational speed of the gas turbine, such that a frequency of electric power output by a power generator that generates electric power using the gas turbine is within a given range, includes a load value acquisition unit configured to acquire a load value that is a value of a load applied to the power generator after cutoff of a part of the load applied to the power generator when the part of the load applied to the power generator is cut off, an arithmetic unit configured to calculate an adjusted value that is a value of the load different from the load value by carrying out an arithmetic operation on the load value and a bias, and a command unit configured to adjust the amount of fuel by outputting a first signal for causing the power generator to output electric power corresponding to the adjusted value.

A method of assembling a gas turbine engine includes setting a build clearance at assembly in response to a running tip clearance defined with a cooled cooling air. A method of operating a gas turbine engine includes supplying a cooled cooling air to a high pressure turbine in response to an engine rotor speed.

A device capable of working done by compressed air and a dual-pressure jet engine thereof are provided, a first compressed air chamber for cooperating with the air intake turbine is arranged between the air intake turbine and the screw gas compressor so as to pressurize the air. The first compressed air chamber is communicated with the screw gas compressor, the air intake end of the screw gas compressor is provided with the fuel injection mechanism for injecting fuel inside the screw gas compressor. The air outlet end of the screw gas compressor is provided with the second compressed air chamber for cooperating with the screw gas compressor so as to pressurize the air. The second compressed air chamber is communicated with the combustion chamber which is used to be injected with fuel.

A device capable of working done by compressed air and a dual-pressure jet engine thereof are provided, a first compressed air chamber for cooperating with the air intake turbine is arranged between the air intake turbine and the screw gas compressor so as to pressurize the air. The first compressed air chamber is communicated with the screw gas compressor, the air intake end of the screw gas compressor is provided with the fuel injection mechanism for injecting fuel inside the screw gas compressor. The air outlet end of the screw gas compressor is provided with the second compressed air chamber for cooperating with the screw gas compressor so as to pressurize the air. The second compressed air chamber is communicated with the combustion chamber which is used to be injected with fuel.

In order to improve a machine for depressurizing or compressing substantially gaseous media, comprising a machine casing and at least one screw rotor, which is arranged in a screw rotor bore in the machine casing, extends between a low-pressure side and a high-pressure side of the screw rotor bore, cooperates with the substantially gaseous medium and is mounted on both sides in the machine casing by means of a respective bearing set, and a motor/generator unit that is coupled or couplable to the at least one screw rotor, it is proposed that the at least one screw rotor should be provided with at least one axial support bearing that axially supports the at least one screw rotor such that a high-pressure end face of the at least one screw rotor is guided, without making contact, to an end wall, which faces this end face, of the machine casing that receives the at least one screw rotor.

A device for work done by compressed air and a dual-pressure jet engine thereof are provided, a first compressed air storage chamber for cooperating with the air intake compressor is arranged between the air intake compressor and the screw gas compressor so as to pressurize the air. The first compressed air storage chamber is communicated with the screw gas compressor, the air intake end of the screw gas compressor is provided with the fuel injection mechanism for injecting fuel inside the screw gas compressor. The air outlet end of the screw gas compressor is provided with the second compressed air storage chamber for cooperating with the screw gas compressor so as to pressurize the air. The second compressed air storage chamber is communicated with the combustion chamber which is used to be injected with fuel.

A device for work done by compressed air and a dual-pressure jet engine thereof are provided, a first compressed air storage chamber for cooperating with the air intake compressor is arranged between the air intake compressor and the screw gas compressor so as to pressurize the air. The first compressed air storage chamber is communicated with the screw gas compressor, the air intake end of the screw gas compressor is provided with the fuel injection mechanism for injecting fuel inside the screw gas compressor. The air outlet end of the screw gas compressor is provided with the second compressed air storage chamber for cooperating with the screw gas compressor so as to pressurize the air. The second compressed air storage chamber is communicated with the combustion chamber which is used to be injected with fuel.

A control device for adjusting an amount of fuel to be supplied to a gas turbine based on a rotational speed of the gas turbine, such that a frequency of electric power output by a power generator that generates electric power using the gas turbine is within a given range, includes a load value acquisition unit configured to acquire a load value that is a value of a load applied to the power generator after cutoff of a part of the load applied to the power generator when the part of the load applied to the power generator is cut off, an arithmetic unit configured to calculate an adjusted value that is a value of the load different from the load value by carrying out an arithmetic operation on the load value and a bias, and a command unit configured to adjust the amount of fuel by outputting a first signal for causing the power generator to output electric power corresponding to the adjusted value.

A control device for adjusting an amount of fuel to be supplied to a gas turbine based on a rotational speed of the gas turbine, such that a frequency of electric power output by a power generator that generates electric power using the gas turbine is within a given range, includes a load value acquisition unit configured to acquire a load value that is a value of a load applied to the power generator after cutoff of a part of the load applied to the power generator when the part of the load applied to the power generator is cut off, an arithmetic unit configured to calculate an adjusted value that is a value of the load different from the load value by carrying out an arithmetic operation on the load value and a bias, and a command unit configured to adjust the amount of fuel by outputting a first signal for causing the power generator to output electric power corresponding to the adjusted value.