发明名称 |
Jet exhaust noise reduction system and method |
摘要 |
A system for reducing jet noise emission from an internally mixed gas turbine engine exhaust, comprising a fan/core flow mixer having a plurality of mixer lobes and a common flow nozzle having an equal number of tabs located along a circumferential edge of an aft end of the nozzle. There is a predetermined clocking relationship between the plurality of mixer lobes and the plurality of nozzle tabs that results in reduced exhaust noise emission, most evident in the lower frequency range. A method for reducing jet noise emission from an internally mixed gas turbine engine exhaust comprises selectively aligning a circumferential distribution of a mixed flow vorticity field produced by a fan/core mixer with a circumferentially distributed exhaust flow vorticity field produced by a modified common flow nozzle at an exit plane of the engine exhaust.
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申请公布号 |
US2005193716(A1) |
申请公布日期 |
2005.09.08 |
申请号 |
US20040794968 |
申请日期 |
2004.03.05 |
申请人 |
SCHLINKER ROBERT;NARAYANAN SATISH;LORD WESLEY K.;KOHLENBERG GREGORY A.;REBA RAMONS;SIMONICH JOHN;SOTERIOU MARIOS C.;MAEDER THIERRY |
发明人 |
SCHLINKER ROBERT;NARAYANAN SATISH;LORD WESLEY K.;KOHLENBERG GREGORY A.;REBA RAMONS;SIMONICH JOHN;SOTERIOU MARIOS C.;MAEDER THIERRY |
分类号 |
F02K1/34;(IPC1-7):F02K1/34 |
主分类号 |
F02K1/34 |
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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