发明名称 DOUBLE-FLOW TURBOJET ENGINE
摘要 FIELD: aero-engine manufacture. SUBSTANCE: blade roots of guide vanes are made in form of profiles straightening the flow of air of second loop twisted by fan and having cooling air passages open to second loop. EFFECT: reduction of resistance of air flowing through second loop; reduction of blade mass; reduction of losses. 4 cl, 3 dwg
申请公布号 RU2127370(C1) 申请公布日期 1999.03.10
申请号 RU19920007825 申请日期 1992.11.24
申请人 SERKOV ANATOLIJ GAVRILOVICH 发明人 SERKOV ANATOLIJ GAVRILOVICH
分类号 F02K3/04;(IPC1-7):F02K3/04 主分类号 F02K3/04
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