发明名称 TUBULAR-ANNULAR COMBUSTION CHAMBER OF GAS-TURBINE POWER PLANT
摘要 FIELD: gas-turbine engineering. SUBSTANCE: combustion chamber has flame tubes each incorporating mixer placed inside downstream of flame and connected through pipe to front wall of flame tube; it is built up of bottom and shell provided with rows of holes; mixer shell is made in the form of truncated cone with straight generating line or that in the form of circle arcs whose convex part faces of flame tube; shell surface opposes the flow; in addition, rows of slits are made in bottom and shell; in flame tube wall there are rows of holes and slits within its length. EFFECT: improved design. 3 dwgm
申请公布号 RU2107228(C1) 申请公布日期 1998.03.20
申请号 RU19950118607 申请日期 1995.11.01
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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