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
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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