FIELD: engines and pumps.
SUBSTANCE: proposed turbo machine comprises combustion chamber, radial-flow compressor, annular diffuser to dissipate compressor gas flow and direct it into combustion chamber. Diffuser comprises radially directed inlet with diffuser channels communicated with compressor outlet, bent intermediate part and outlet incorporating several straightener vanes regularly spaced apart along the circle, and outer jacket surrounding combustion chamber and outlet. Flow section is confined by outer jacket at outlet. Outer jacket has flange for intermediate part outlet edge to thrust against.
EFFECT: simplified assembly.
9 cl, 5 dwg
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