发明名称 GAS TURBINE ENGINE COMPRISING EXHAUST CONE WITH INTEGRATED MUFFLER
摘要 A gas turbine engine, in which gases flow upstream to downstream, including a combustion chamber, a high-pressure turbine placed downstream from the combustion chamber, arranged so as to receive combustion gases from the combustion chamber, a free turbine, and an exhaust-gas guide cone attached to the free turbine downstream from the free turbine, the turbine engine emitting sound waves during operation. The guide cone includes a sound suppressor, for example with a Helmholtz resonator structure, with a resonant cavity and a resonator neck in communication with an opening, arranged so as to suppress the sound waves emitted by the turbine engine.
申请公布号 EP2435685(B1) 申请公布日期 2017.03.29
申请号 EP20100724370 申请日期 2010.05.27
申请人 Safran Helicopter Engines 发明人 BOUTY, Eric, Jean-Louis;REGAUD, Pierre-Luc;VALLON, Antoine
分类号 F02K1/82 主分类号 F02K1/82
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