发明名称 Turbine engine tailcone resonator
摘要 A turbine engine resonator (80) comprising a panel (52) and a vessel (82). The panel (52) is along a flow path within the engine and has an aperture (72). The vessel (82) has a mounting flange (92) secured to the panel (52). The flange (92) has an aperture mated to the aperture (72) of the panel (52). The vessel (82) has a body secured to the mounting flange (92) with an interior of the body in communication with the flange aperture. A first portion (182) of the panel (52) 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 EP1849974(A2) 申请公布日期 2007.10.31
申请号 EP20070250806 申请日期 2007.02.27
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BAARCK, JENNY N.;PROSCIA, WILLIAM;KRAYENVENGER, DAREN;JONES, CHRISTOPHER D.
分类号 F02C5/10;F01D25/30;F02C5/11;F02C7/045;F02C7/24;F02K1/04;F02K1/34;F02K1/82;G10K11/172 主分类号 F02C5/10
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