AIRCRAFT WING ARRANGEMENT COMPRISING AN ENGINE ATTACHMENT PYLON DEFINING, IN THE FORWARD REGION, A LATERAL AIRFLOW CHANNEL
摘要
<p>The invention relates to an aircraft wing arrangement (1) comprising a wing (2) and at least one aircraft engine attachment pylon (4) for attaching an engine suspended under the wing and comprising a forward region (8) protruding forward from an leading edge (10) of the wing. According to the invention, the forward region (8) comprises a lateral projection (12) delimiting a lateral airflow channel (14) extending towards a proximal end of the wing.</p>
申请公布号
WO2007113183(A1)
申请公布日期
2007.10.11
申请号
WO2007EP52957
申请日期
2007.03.28
申请人
AIRBUS FRANCE;DANTIN, STEPHANIE;FOL, THIERRY;GERARD, LUDOVIC;JIMENEZ, PHILIPPE
发明人
DANTIN, STEPHANIE;FOL, THIERRY;GERARD, LUDOVIC;JIMENEZ, PHILIPPE