发明名称 AXIAL FLOW COMPRESSOR
摘要 <p>A device for moving air from the jet flow of an axial compressor of a gas turbine group, to be conducted along the axis of the group to the turbine to be cooled. The air is moved by a wheel having an outer rim serving as a brace between two adjacent compressor disks and centripetal blading which moves the air through openings formed in the rim, to accelerate it and discharge it into a space surrounding the axis of the compressor.</p>
申请公布号 GB2003230(A) 申请公布日期 1979.03.07
申请号 GB19780031942 申请日期 1978.08.02
申请人 SOC NAT ETUDE CONSTR MOTEURS AVIATION 发明人
分类号 F01D5/08;F02C7/18;F04D27/02;(IPC1-7):04D25/16 主分类号 F01D5/08
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