FIELD: engine-driven plants, off-line drives, and power plant drives. SUBSTANCE: gas turbine concentric to annular outlet of compressor has combustion chambers uniformly arranged over inner surface of runner; entry in each combustion chamber is located in annular outlet above compressor guide vanes and faces its outlet; exit of each combustion chamber protrudes beyond external surface of runner in the form of convergent-divergent nozzle. EFFECT: improved design. 4 cl, 2 dwg
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Authors
Dates
1997-05-10—Published
1993-06-08—Filed