发明名称 GAS TURBINE ENGINE
摘要 FIELD: engines and pumps. ^ SUBSTANCE: gas turbine engine comprises at least one turbo compressor rotor with labyrinth seal that runs in bearing and at least one electrical machine built in turbo compressor. Electrical machine comprises set of permanent magnets fitted on turbo compressor rotor, and electrical machine stator arranged on bearing support housing face surface and having its winding arranged on bearing support housing. Set of permanent magnets is fitted to axially move in collar arranged on turbo compressor rotor inner surface between stator winding. Aforesaid magnets are spring loaded in direction opposite electrical machine stator to rest against piston fitted inside collar circular chamber. Said circular chamber communicates, via channel, with turbo compressor air passage. ^ EFFECT: higher power output and efficiency. ^ 4 cl, 2 dwg
申请公布号 RU2382210(C1) 申请公布日期 2010.02.20
申请号 RU20080140992 申请日期 2008.10.15
申请人 BOLOTIN NIKOLAJ BORISOVICH 发明人 BOLOTIN NIKOLAJ BORISOVICH
分类号 F01D15/10 主分类号 F01D15/10
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