FIELD: engines and pumps.
SUBSTANCE: invention relates to power engineering. Gas turbine of cyclic internal combustion comprises at least one combustion chamber equipped with intake valves and igniters. Note here that at least one combustion chamber on gas exhaust side incorporates no shutoff devices to make it permanently exposed on gas outlet side. Under at least one combustion chamber arranged is the turbine along the flow to feed working gas therein contained in combustion chamber. Note here that flow-through chamber is arranged between one combustion chamber and said turbine axially behind said combustion chamber. Flow-through chamber is separated from said combustion chamber by guide disc or extra turbine. Invention covers also the method gas turbine operation and drive for machine including said gas turbine.
EFFECT: simple design.
14 cl, 4 dwg
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