Gas turbine
A technology of gas turbines and turbines, applied in the direction of gas turbine devices, mechanical equipment, engine components, etc., can solve the problem of not providing auxiliary blades to cool turbine blades, etc.
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[0022] The idea that is part of the invention is to integrate independent compressor stages on the gas turbine shaft, with the explicit primary goal of producing cooling air only at the required pressure level. Thus, the individual stages can be designed in an optimized manner to meet the cooling requirements and no specific cooling needs to be taken into account during the compression of the main mass flow of combustion air. The generation of the necessary pressure levels can be achieved by all available types of compressors (axial, radial or diagonal). It is also conceivable to use the surge effect through a simple channel on / in the rotor.
[0023] figure 2 and figure 1 Similarly, a schematic diagram of a (generally) exemplary embodiment of a gas turbine according to the invention is shown. figure 2 The gas turbine 20 shown has and figure 1 The gas turbine 10 shown has the same core elements 11 to 17 . However, the cooling design of the gas turbine is different. To g...
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