FIELD: aircraft engines. SUBSTANCE: gas turbine has stator with nozzle vanes 1, rotor with working blades 2, case of turbine 3 with cooling air supply holes 4 and deflector 5. Cooling air after compressor or secondary air from combustion chamber contaminated with foreign matter strikes against deflector 5 while approaching hole 4; as a result, foreign particles are thrown to flow section of engine turbine and purified air enters the turbine cooling system through slit between deflector and case. EFFECT: enhanced efficiency. 3 cl, 1 dwg
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Authors
Dates
1996-11-27—Published
1992-02-19—Filed