发明名称 STRUCTURE OF COMBUSTOR FOR GAS TURBINE
摘要 PROBLEM TO BE SOLVED: To provide a combustor for gas turbine in which good combustion can be attained by mixing fuel and air, and combustion gas and air smoothly in the inner tube of the combustor. SOLUTION: In a gas turbine where air taken in from the outside is mixed with fuel ejected from a fuel ejection valve and mixed gas is combusted in a combustor, a tubular air passage is formed on the circumference of the combustor such that the air flows into the combustor while advancing in the same direction as the advancing direction of combustion gas generated in the combustor.
申请公布号 JP2002005443(A) 申请公布日期 2002.01.09
申请号 JP20000187685 申请日期 2000.06.22
申请人 YANMAR DIESEL ENGINE CO LTD 发明人 ARAKAWA SADAO
分类号 F23R3/42;F23R3/06;(IPC1-7):F23R3/42 主分类号 F23R3/42
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