发明名称 Combustor of gas turbine and combustion control method for gas turbine
摘要 In a combustor, divisional fluid passages of a first group, and divisional fluid passages of a second group are present on an inner peripheral side, and divisional fluid passages are also present on an outer peripheral side, and swirl air flows are gushed from the divisional fluid passages. When the total amount of fuel supplied to the combustor is small as in a speed increasing state or in a low load state, fuel is injected only into the divisional fluid passages of the first group. Since a fuel injection region is limited to a position on the inner peripheral side, particularly, a specific position, the concentration of a fuel gas comprising a mixture of fuel and air is lean, but is higher than a flammability limit concentration, even when the total amount of fuel is small.
申请公布号 US7673454(B2) 申请公布日期 2010.03.09
申请号 US20070700214 申请日期 2007.01.31
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 SAITO KEIJIRO;TANIMURA SATOSHI;YUASA ATSUSHI;SAITO TOSHIHIKO
分类号 F02C3/00 主分类号 F02C3/00
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