发明名称 |
Turbine engine tailcone resonator |
摘要 |
A turbine engine comprises a case (42)and a centerbody (40) within the case (42) and separated from the case (42) by a core flowpath. A circumferential array of augmentor vanes (50) extends between the centerbody (40) and case (42). A circumferential array of resonators (80) is arranged within the centerbody (40) each having a port open to the core flowpath. Each resonator (80) comprises a resonator body having a neck (84) and an enlarged main body (86) inboard of the neck (84). The main body (86) has a convex first circumferential side and a concave second circumferential side converging inboard, each first circumferential side nested with the second adjacent side of a first adjacent one of the resonators (80) and each second circumferential side nested with the first adjacent side of a second adjacent one of the resonators (80). |
申请公布号 |
EP2484881(A1) |
申请公布日期 |
2012.08.08 |
申请号 |
EP20120160989 |
申请日期 |
2007.02.27 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BAARCK, JENNY N.;KRAYENVENGER, DAREN;PROSCIA, WILLIAM;JONES, CHRISTOPHER D. |
分类号 |
F02C5/10;F01D25/30;F02C5/11;F02C7/045;F02C7/24;F02K1/04;F02K1/34;F02K1/82;F02K3/10;F23R3/00;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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