发明名称 TURBOMACHINE COMBUSTOR AND METHOD FOR ADJUSTING COMBUSTION DYNAMICS IN THE SAME
摘要 A turbomachine combustor includes a combustor cap having a cap surface and a wall that define, at least in part, a resonator volume. A plurality of injection nozzle members extend from the cap surface. Each of the plurality of injection nozzle members include an inner nozzle member and a plurality of outer nozzle members. An adjustable conduit extends through the wall into the resonator volume. The adjustable conduit includes an internal passage having a dimensional parameter. A combustor dynamics mitigation system is operably connected to the combustor cap. The combustor dynamics mitigation system includes a controller configured and disposed to control one a size of the resonator volume and the dimensional parameter of the adjustable conduit to modify combustor dynamics in the combustor.
申请公布号 US2013305729(A1) 申请公布日期 2013.11.21
申请号 US201213476413 申请日期 2012.05.21
申请人 BATHINA MAHESH;MANOHARAN MADANMOHAN;GENERAL ELECTRIC COMPANY 发明人 BATHINA MAHESH;MANOHARAN MADANMOHAN
分类号 F02C7/24;F02C3/04 主分类号 F02C7/24
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