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  5. The splitting blades for the regulation system of aviation engines compressors

The splitting blades for the regulation system of aviation engines compressors

V. Dykhanovsky, О. Shapovalov
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On the base of analyses of speed triangles behind inlet stator blades of the prototype of engine АI-450-MC had shown, that on the off designed regimes of gas turbine engine functioning the modern regulation systems can’t to guarantee continuous flow along the length of the rotor blade. Proposed the method of change the designed inlet and outlet angels of inlet stator blades accordingly to regime of gas turbine engine functioning.