发明名称 HIGH-LIFT SYSTEM FOR AN AIRCRAFT
摘要 A high-lift system with a main wing and adjustable flaps as well as guiding devices for holding the adjustable flaps and adjustment devices for adjusting the adjustable flaps, wherein the respective guiding device and/or adjustment device at least in part include/includes a fairing, including a flow influencing device for influencing the flow around the high-lift system, with at least one inlet line with at least one inlet that is situated on or below the bottom of the high-lift system, wherein, furthermore, at least one outlet line for air is provided that includes a fluid-communicating connection to the inlet line and includes at least one outlet situated at the top in the region of at least one adjustable flap of the high-lift system.
申请公布号 US2013009015(A1) 申请公布日期 2013.01.10
申请号 US201213530156 申请日期 2012.06.22
申请人 AIRBUS OPERATIONS GMBH;GOELLING BURKHARD 发明人 GOELLING BURKHARD
分类号 B64C21/08 主分类号 B64C21/08
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