发明名称 GAS-TURBINE BURNER AND OPERATING METHOD THEREFOR
摘要 PURPOSE:To enable the starting of an operation to be completed in a short period of time by a method wherein columnar members, whose tip ends with a fuel nozzle are projected from the side wall of a combustion subchamber, are provided in the combustion subchamber, and an air-fuel ratio is increased at the increasing time of the number of revolutions of the columnar members. CONSTITUTION:At the starting of an operation, fuel l is fed, and ignition for cross firing is effected. Thus, the feed amount of the fuel l is increased and, when it approaches an upper limit blowing-off limited flow rate, the feed of the fuel l is kept constant and fuel m is fed. When fuel nozzles 3 reach the number of revolutions capable of singly burning, the flow rate of the fuel lis increased while the flow rate of the fuel m is gradually decreased and, prior to reaching the rated number of revolutions with no load, the flow rate of the fuel m is reduced to zero. According to this constitution, the starting of the operation can be completed within a short period of time.
申请公布号 JPH02208417(A) 申请公布日期 1990.08.20
申请号 JP19890023884 申请日期 1989.02.03
申请人 HITACHI LTD 发明人 URUSHIYA HARUO;KIRIKAMI SEIICHI;SATO ISAO;SHIMIZU NOBUO;ARAI OSAMU;SHIMURA AKIRA;KURODA MICHIO;KOGA TSUGUAKI;KUROKAWA SUNAO;ISHIBASHI YOJI;KUNO KATSUKUNI
分类号 F02C7/26;F02C9/34;F23C99/00;F23R3/16;F23R3/20;F23R3/26;F23R3/34 主分类号 F02C7/26
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