发明名称 |
Turbomachine combustor and method for adjusting combustion dynamics in the same |
摘要 |
<p>A turbomachine (2) combustor includes a combustor cap (16) having a cap surface (32) and a wall (35) that define, at least in part, a resonator volume (40). A plurality of injection nozzle members extend from the cap surface (32). Each of the plurality of injection nozzle members include an inner nozzle member (60) and a plurality of outer nozzle members (62). An adjustable conduit (80) extends through the wall (35) into the resonator volume (40). The adjustable conduit (80) includes an internal passage (82) having a dimensional parameter. A combustor dynamics mitigation system (90) is operably connected to the combustor cap (16). The combustor dynamics mitigation system (90) includes a controller (160) configured and disposed to control one a size of the resonator volume (40) and the dimensional parameter of the adjustable conduit (80) to modify combustor dynamics in the combustor.</p> |
申请公布号 |
EP2667096(A2) |
申请公布日期 |
2013.11.27 |
申请号 |
EP20130168239 |
申请日期 |
2013.05.17 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
BATHINA, MAHESH;MANOHARAN, MADANMOHAN |
分类号 |
F23R3/00;F23R3/04;F23R3/28 |
主分类号 |
F23R3/00 |
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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