<p>An aircraft noise-reduction apparatus comprise a flow-facing element(1)and a flow control device(2)positioned downstream of the flow-facing element(1). The flow (5) control device (2) is arranged, in use, to reduce noise induced by unsteady flow downstream of the flow-facing element (1).</p>
申请公布号
WO2009053745(A1)
申请公布日期
2009.04.30
申请号
WO2008GB50983
申请日期
2008.10.23
申请人
AIRBUS UK LIMITED;CHOW, LEUNG CHOI;SPITERI, MATTHEW;ZHANG, XIN;ANGLAND, DAVID;GOODYER, MICHAEL
发明人
CHOW, LEUNG CHOI;SPITERI, MATTHEW;ZHANG, XIN;ANGLAND, DAVID;GOODYER, MICHAEL
