发明名称 |
GAS TURBINE ENGINE HAVING CONFIGURABLE BYPASS PASSAGE |
摘要 |
A gas turbine engine (50) is disclosed which includes a bypass passage (58) that in some embodiments is capable of being configured to act as a resonance space. The resonance space can be used to attenuate or accentuate a noise produced elsewhere. The bypass passage can be configured in a number of ways to form the resonance space. In one form the resonance space can attenuate a noise forward of the bypass duct. In another form the resonance space can. attenuate a noise aft of the bypass duct. |
申请公布号 |
WO2014133645(A3) |
申请公布日期 |
2014.12.11 |
申请号 |
WO2013US75286 |
申请日期 |
2013.12.16 |
申请人 |
ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES INC. |
发明人 |
DUGE, ROBERT T. |
分类号 |
F02K3/02;F02C9/18;F02K3/06 |
主分类号 |
F02K3/02 |
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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