发明名称 STAGE OF GAS TURBINE ENGINE AXIAL COMPRESSOR
摘要 FIELD: non-positive displacement pumps. ^ SUBSTANCE: stage comprises blades mounted in the metallic part of the ring bandage by means of a lock mounted in the inner metallic ring (2) that is set inside the outer ring (1) made of a composite material. The lock consists of head (4) secured to bushing (5) that goes into flexible tubs (7) that are ended with hooks (6) overlapping blade (3) and inner metallic ring (2). ^ EFFECT: simplified structure and enhanced reliability. ^ 3 dwg
申请公布号 RU2299357(C1) 申请公布日期 2007.05.20
申请号 RU20060104569 申请日期 2006.02.14
申请人 KOVALEV VJACHESLAV DANILOVICH;ZAJNULIN ISKANDER GAJFIEVICH;VAJCHIS GEORGIJ IVANOVICH;ZAJNULINA IRINA NIKOLAEVNA 发明人 KOVALEV VJACHESLAV DANILOVICH;ZAJNULIN ISKANDER GAJFIEVICH;VAJCHIS GEORGIJ IVANOVICH;ZAJNULINA IRINA NIKOLAEVNA
分类号 F04D29/34 主分类号 F04D29/34
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