发明名称 EXHAUST SYSTEM FOR GAS TURBINE
摘要 The invention relates to an exhaust system (100) for directing the flow from a gas turbine, that comprises a flow directing nozzle and an exhaust casing (110) for connecting the duct nozzle to the outlet of the gas turbine. The duct nozzle includes a primary duct (120) attached to the exhaust casing (110) and a secondary nozzle (130) arranged about the primary nozzle. The exhaust system further includes a means for directly attaching the secondary nozzle (130) to the exhaust casing (110), the secondary nozzle being held by the exhaust casing independently from the primary nozzle (120).
申请公布号 WO2008148999(A2) 申请公布日期 2008.12.11
申请号 WO2008FR50801 申请日期 2008.05.07
申请人 SNECMA PROPULSION SOLIDE;CONETE, ERIC;BAROUMES, LAURENT;HABAROU, GEORGES 发明人 CONETE, ERIC;BAROUMES, LAURENT;HABAROU, GEORGES
分类号 F02C7/20;F02K1/52;F02K1/80 主分类号 F02C7/20
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