FIELD: mechanical engineering; internal combustion engines.
SUBSTANCE: proposed internal combustion turbine engine has body, shaft, turbine with radial blades, compressor, combustion chamber, fuel mixture supply and ignition system and exhaust system. At least one row of additional blades is found at least on one side surface of turbine. Channels-nozzles are made on surface of body adjoining said side surface of turbine. Channels-nozzles direct working gases, when registering with combustion chamber, from space formed by radial blades into space formed by additional blades.
EFFECT: increased efficiency.
17 cl, 8 dwg
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Authors
Dates
2007-01-10—Published
2004-07-22—Filed