发明名称 TURBINE ENGINE AUGMENTER, AND METHOD FOR OPERATING THE SAME
摘要 PROBLEM TO BE SOLVED: To provide an augmenter (32) which is characterized in a plurality of flame holders (42) to cause combustion of additional fuel and uses a pilot device to stabilize flame of the flame holders (42). SOLUTION: The turbine engine augmenter (32) has a center body (38) provided within a gas flowpath. The flame holders (42) are disposed within the flowpath and outside the center body (38). A burner having the center body has an outlet to emit combustion product of a first pilot fuel. A pilot fuel line has an outlet disposed so as to charge additional pilot fuel to the emitted combustion product. COPYRIGHT: (C)2005,JPO&NCIPI
申请公布号 JP2004332729(A) 申请公布日期 2004.11.25
申请号 JP20040132325 申请日期 2004.04.28
申请人 UNITED TECHNOL CORP <UTC> 发明人 LOVETT JEFFERY A
分类号 F23R3/20;F02K3/10;F23R3/18;F23R3/34;(IPC1-7):F02K3/10 主分类号 F23R3/20
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