Gas turbine assembly and method for operating said gas turbine assembly
A gas turbine and unit technology, applied to engine components, machines/engines, mechanical equipment, etc., can solve problems such as separation changes
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[0046] exist figure 1 In reference numeral 1 refers to the gas turbine assembly (in figure 1 shown schematically).
[0047] The gas turbine assembly 1 includes a compressor 3 , a combustor 4 , and a turbine 5 .
[0048] In particular, the gas turbine assembly 1 includes a stator 6 defining at least a compression working channel 8 and an expansion working channel 9 .
[0049] The compressor 3 and the turbine 5 are mounted on the same shaft to form a rotor 11 which is housed in the stator 6 and extends along the axis A.
[0050] In more detail, the rotor 11 includes a front axle 12 , a plurality of rotor stages 13 and a rear axle 14 .
[0051] Each rotor stage 13 includes a rotor disk 16 and a plurality of rotor blades 17 coupled to the rotor disk 16 and arranged radially.
[0052] A plurality of rotor discs 16 are arranged in succession between the front axle 12 and the rear axle 14 and are preferably sandwiched into a stack by a central tie rod 18 . Alternatively, the rot...
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