发明名称 Exhaust system for gas turbine
摘要 The invention relates to an exhaust system (100) for channeling the streams from a by-pass gas turbine, the system comprising a stream channeling nozzle and an exhaust casing (110) for connecting the channeling nozzle to the outlet of the gas turbine, said channeling nozzle comprising a primary nozzle (120) fastened to the exhaust casing (110) and a secondary nozzle (130) placed around the primary nozzle. The exhaust system further comprises means for fastening the secondary nozzle (130) directly to the exhaust casing (110), said secondary nozzle being supported by the exhaust casing independently of the primary nozzle (120).
申请公布号 US8424312(B2) 申请公布日期 2013.04.23
申请号 US20080599345 申请日期 2008.05.07
申请人 CONETE ERIC;BAROUMES LAURENT;HABAROU GEORGES;SNECMA PROPULSION SOLIDE 发明人 CONETE ERIC;BAROUMES LAURENT;HABAROU GEORGES
分类号 F02K1/40 主分类号 F02K1/40
代理机构 代理人
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