发明名称 A HIGH LIFT SYSTEM FOR AN AIRCRAFT
摘要 A high lift system with a main wing and control flaps, wherein the respective guiding device are at least partially provided with a fairing, having a flow control device for purposes of controlling the flow around the high lift system with at least two inlet ducts running along the main wing chordwise direction with in each case at least one inlet, which device is located on or underneath the lower surface of the high lift system, wherein at least one outlet duct for air is furthermore provided, which is connected with the inlet ducts in a fluid-communicating manner, and has at least one outlet, which is located on the upper surface of at least one regulating flap and/or with respect to the main wing chordwise direction in the rear third of the main wing of the high lift system.
申请公布号 EP2544946(A2) 申请公布日期 2013.01.16
申请号 EP20110708724 申请日期 2011.03.08
申请人 AIRBUS OPERATIONS GMBH 发明人 GOELLING, BURKHARD
分类号 B64C9/16 主分类号 B64C9/16
代理机构 代理人
主权项
地址