Gas turbine with exhaust gas diffuser and support ribs
A gas turbine and diffuser technology, which is applied in gas turbine installations, machines/engines, mechanical equipment, etc., can solve problems such as restricting the working mode of gas turbines and afterburners
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[0013] figure 1 A partial longitudinal section of a stationary gas turbine 10 is shown. The gas turbine 10 internally has a rotor 14 mounted in rotation about an axis of rotation 12 , which is also referred to as a turbine rotor. Along the rotor 14 are the suction housing 16 , the axial turbocompressor 18 , the toroidal annular combustion chamber 20 with a plurality of burners 22 arranged rotationally symmetrically to one another, the turbine unit 24 and the turbine exhaust housing 26. A turbine exhaust gas distributor, not shown in further detail, is connected to the turbine output housing 26 of the gas turbine 10 . These two components are part of the gas turbine exhaust diffuser 21 . Instead of an annular combustion chamber, the gas turbine can also be constructed with a plurality of tubular combustion chambers.
[0014] The axial turbocompressor 18 comprises a ring-shaped compressor channel with compression stages formed successively in cascade fashion in it, formed of...
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