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 |
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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