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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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