发明名称 GAS TURBINE COMBUSTION CHAMBER
摘要 In an annular combustion chamber (A), there is arranged on the inflow side in circumferential direction a row of pre-mix burners (B, C). The large pre-mix burners (B), which are the main burners of the annular combustion chamber (A), and the small pre-mix burners (C), which are the pilot burners of the annular combustion chamber, are positioned alternately and at a uniform distance from one another. Both the main burners (B) and the pilot burners (C) open into a single annular front wall (10). <IMAGE>
申请公布号 RU1835031(C) 申请公布日期 1993.08.15
申请号 SU19904743324 申请日期 1990.03.14
申请人 ASEA BRAUN BOVERI AG 发明人 YAKOB KELLER;TOMAS ZATTELMAJER
分类号 F23R3/02;F23C7/00;F23D11/40;F23R3/00;F23R3/12;F23R3/30;F23R3/34;F23R3/44;F23R3/50 主分类号 F23R3/02
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