发明名称 FUEL PULSATION-SUPPRESSION FOR GAS TURBINE COMBUSTION SYSTEM
摘要 <p>Rupture of the transition piece in one or more combustors of a gas turbine, due to resonance at the transition piece natural modal frequency, is avoided by interconnecting pairs of fuel lines having sinusoidal fluctuations in fuel flow that are 180.degree. out of phase with each other through opposite ends of an accumulator containing a movable partition displaced according to relative pressure on either side of the partition.</p>
申请公布号 CA1124089(A) 申请公布日期 1982.05.25
申请号 CA19780310435 申请日期 1978.08.31
申请人 GENERAL ELECTRIC COMPANY 发明人 SAVKAR, SUDHIR D.
分类号 F02C7/22;(IPC1-7):02C7/22 主分类号 F02C7/22
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