发明名称 Exhaust plenum for a turbine engine
摘要 <p>An exhaust system for gas turbine engine (12) is provided that reduces turbulence and backflow within the exhaust system and, thus, increases the efficiency of the turbine engine (12). In various embodiments, the system includes an exhaust plenum (32) that provides a gradual expansion of the exhaust gases. The exhaust plenum (32) may also include one or more flow splitters (84, 130) that further reduce turbulence in the plenum or symmetrical arrangements and provide a more uniform gas flow in the plenum and other downstream exhaust components.</p>
申请公布号 EP2239428(A2) 申请公布日期 2010.10.13
申请号 EP20100158248 申请日期 2010.03.29
申请人 GENERAL ELECTRIC COMPANY 发明人 MERCHANT, LAXMIKANT;RAJESH, PRABHAKARAN SARASWATHI
分类号 F01D25/30;F02K1/00 主分类号 F01D25/30
代理机构 代理人
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