发明名称 Turbine engine tailcone resonator
摘要 A turbine engine resonator comprising a panel and a vessel. The panel is along a flow path within the engine and has an aperture. The vessel has a mounting flange secured to the panel. The flange has an aperture mated to the aperture of the panel. The vessel has a body secured to the mounting flange with an interior of the body in communication with the flange aperture. A first portion of the panel extends into the mounting flange aperture and may redirect a leakage flow, if any, to limit an effect of leakage upon resonator performance.
申请公布号 US7552796(B2) 申请公布日期 2009.06.30
申请号 US20060412756 申请日期 2006.04.27
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BAARCK JENNY N.;KRAYENVENGER DAREN;PROSCIA WILLIAM;JONES CHRISTOPHER D.
分类号 F01N1/02 主分类号 F01N1/02
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