发明名称 Method and apparatus to decrease combustor acoustics
摘要 A method for operating a gas turbine engine includes coupling an anti-resonant frequency system to a combustor including a premixer assembly and a plurality of damper tubes, and adjusting the anti-resonant frequency system until the anti-resonant frequency of the damper tubes is approximately equal to the combustor resonant frequency.
申请公布号 US7272931(B2) 申请公布日期 2007.09.25
申请号 US20030663008 申请日期 2003.09.16
申请人 GENERAL ELECTRIC COMPANY 发明人 HELD TIMOTHY JAMES;HSIAO GEORGE CHIACHUN
分类号 F02C1/00;F23R3/00;F02C7/24;F23M99/00;F23R3/04;F23R3/10;F23R3/42 主分类号 F02C1/00
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