发明名称 Flap arrangement for an aircraft mainplane (wing)
摘要 A flap arrangement for an aircraft mainplane consists of in each case at least one extendable high-lift flap, which is arranged on the trailing edge of the mainplane, and of at least one spoiler which is allocated to this flap. Furthermore, it has in each case one actuating device which is allocated to the high-lift flap and/or to the spoiler. The control and regulating device which is connected upstream of the actuating device for the spoiler is in this case acted on by a proximity sensor, which is arranged in the region of the gap formed by the high-lift flap and the spoiler and causes the spoiler to follow up a change in the position of the high-lift flap in such a manner that the required separation between the flap and the spoiler is maintained. <IMAGE>
申请公布号 DE3621401(C1) 申请公布日期 1988.01.14
申请号 DE19863621401 申请日期 1986.06.26
申请人 MESSERSCHMITT-BOELKOW-BLOHM GMBH, 2800 BREMEN, DE 发明人 MARTENS, WILHELM, 2870 DELMENHORST, DE
分类号 B64C9/12;B64C13/26;B64C13/50;(IPC1-7):B64C9/04 主分类号 B64C9/12
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