FIELD: machine building.
SUBSTANCE: double-flow turbojet engine comprises gas generator of internal circuit with compressor, combustion chamber and turbine, connected by gas generator shaft with compressor, intermediate housing and fan connected by shaft to turbine of fan, auxiliary units are driven by inner circuit gas generator shaft via central conical drive and set of gears. Auxiliary units are installed on annular separator of intermediate housing. Set of gears for driving auxiliary units is arranged inside annular separator.
EFFECT: invention is aimed at simplification of the design.
1 cl, 1 dwg
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