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.
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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 |
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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