发明名称 EXHAUST DUCT WITH BYPASS CHANNEL
摘要 An exhaust duct for directing a stream of exhaust gases in a gas turbine engine is provided. The exhaust duct comprises an inlet for receiving the stream of exhaust gases from a turbine section of the gas turbine engine; an outlet in fluid communication with the inlet; and a transition portion defining a passage between the inlet and the outlet. The passage comprises an annular region having a first side portion and a second side portion that are separated by a flow splitter. At least one bypass channel interconnects the first side portion and the second side portion of the annular region.
申请公布号 CA2638661(C) 申请公布日期 2016.10.18
申请号 CA20082638661 申请日期 2008.08.13
申请人 PRATT & WHITNEY CANADA CORP. 发明人 FARBER, STEVEN
分类号 F01D25/30;F01D25/24;F02K1/78 主分类号 F01D25/30
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