发明名称 GAS-TURBINE COMBUSTION CHAMBER
摘要 FIELD: power plants burning compressed natural gas. SUBSTANCE: each flame tube of combustion chamber has flame mixer placed inside tube downstream of flow as well as external and internal blade-type axial vortex generator arranged concentrically to mixer. Blades of external vortex generator are hollow structures fixed with walls of flame tubes and mixer as well as with central body placed concentrically to mixer. The latter and central body are made in the form of cone or hyperboloid of revolution. EFFECT: reduced emission of nitrogen oxides into the atmosphere. 2 dwgF
申请公布号 RU2107229(C1) 申请公布日期 1998.03.20
申请号 RU19960102244 申请日期 1996.02.06
申请人 AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 KUZMENKO M.L.;SNITKO A.A.;TOKAREV V.V.;BRYNDIN O.V.;KIRIEVSKIJ JU.E.;KHRJASHCHIKOV M.S.;KHAJRULLIN M.F.;KUZMENKO M.L.;SNITKO A.A.;TOKAREV V.V.;BRYNDIN O.V.;KIRIEVSKIJ JU.E.;KHRJASHCHIKOV M.S.;KHAJRULLIN M.F.
分类号 F23R3/16;(IPC1-7):F23R3/16 主分类号 F23R3/16
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