发明名称 Jet nozzle having noise attenuating shield and method therefor
摘要 An arcuate or semi-circumferential shield in the shape of a visor that is adapted to be secured to an external surface of a nozzle housing of a jet nozzle to attenuate jet noise generated by the jet nozzle. The shield may be fixedly secured to the nozzle housing or movably supported so that it can be moved between retracted and deployed positions. When used as a fixedly mounted component, or when positioned in its deployed position, a downstream edge of the shield extends past a downstream edge of the nozzle housing and the shield is spaced apart from an outer surface of the nozzle housing to form a channel therebetween. The shield is preferably orientated at approximately a bottom dead center of the nozzle housing. The shield operates to attenuate jet installation noise, and particularly jet installation noise experienced during the takeoff phase of flight of a jet aircraft, as well as to reduce jet installation noise that would otherwise propagate forwardly toward the cockpit of the aircraft.
申请公布号 US7883049(B2) 申请公布日期 2011.02.08
申请号 US20070741457 申请日期 2007.04.27
申请人 THE BOEING COMPANY 发明人 NESBITT ERIC H.;YEE MARK;ELKOBY RONEN;HEBERT LEONARD J.;ALSTON THOMAS E.
分类号 F02K1/44 主分类号 F02K1/44
代理机构 代理人
主权项
地址