FIELD: laser engineering. SUBSTANCE: axial-flow compressor case of assembly is placed in shell in a spaced relation to allow gas passage between them; inlet shaper and outlet splitter are connected on two sides to this shell. In addition, shell of proposed assembly is conical in shaped and functions at the same time as part of inlet gas-flow shaper; edge of heat-transfer system is located at inlet end of shell; axial-flow compressor is provided with device for adjusting clearance between case and shell. EFFECT: improved design. 2 dwg
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