| 发明名称 |
BURNER OF GAS-TURBINE ENGINE COMBUSTION CHAMBER |
| 摘要 |
FIELD: combustion chambers of gas-turbine engines working mainly on gaseous fuel. SUBSTANCE: each burner of combustion zone and pilot combustion zone. Combustion process in pilot zone is organized at excess air coefficient of alpha = 1.2 to 1.4 and in main combustion zone at excess air coefficient of alpha = 1.8 to 2.0. EFFECT: enhanced efficiency. 2 cl, 2 dwga
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| 申请公布号 |
RU2107869(C1) |
申请公布日期 |
1998.03.27 |
| 申请号 |
RU19930034343 |
申请日期 |
1993.07.01 |
| 申请人 |
AKTSIONERNOE OBSHCHESTVO OTKRYTOGO TIPA SAMARSKIJ;AKTSIONERNOE OBSHCHESTVO OTKRY |
发明人 |
POSTNIKOV A.M.;MARKUSHIN A.N.;DENISOV I.S.;SAVCHENKO V.P.;POSTNIKOV A.M.;MARKUSHIN A.N.;DENISOV I.S.;SAVCHENKO V.P. |
| 分类号 |
F23R3/00;(IPC1-7):F23R3/00 |
主分类号 |
F23R3/00 |
| 代理机构 |
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代理人 |
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