发明名称 EXHAUST FOR A GAS TURBINE ENGINE
摘要 <p>A gas turbine engine is provided having an offtake passage that in one form is capable of extracting a bypass flow from the engine. The airflow traversing the offtake passage is introduced to an exhaust flow of the gas turbine engine through an offtake outlet. The offtake outlet includes an airflow member that is moveable. A nozzle is also provided for exhaust from the gas turbine engine. In one form the nozzle includes moveable duct members. Flows exiting the offtake outlet and the nozzle can be combined after passing the airflow member and the moveable duct members, respectively.</p>
申请公布号 EP2519729(A1) 申请公布日期 2012.11.07
申请号 EP20100841678 申请日期 2010.12.29
申请人 ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC. 发明人 SUTTERFIELD, DAVID, LEVI
分类号 F02K1/12;B64D33/04;F02C9/18;F02K1/38;F02K3/02;F02K3/06;F02K3/075 主分类号 F02K1/12
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