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 代理人
主权项
地址