发明名称 ADJUSTING DEVICE FOR ADJUSTING A HIGH-LIFT FLAP AND AIRFOIL WING COMPRISING SUCH AN ADJUSTING DEVICE
摘要 Adjusting device for adjusting a high-lift flap (2; 102) and airfoil wing provided with the same, comprising at lest one flap drive (20) for operating the flap (2; 102), and comprising several drive stations (3, 4, 5) which movably connect the high-lift flap (2; 102) to the airfoil wing (1) for guiding the flap (2; 102) by means of tension/compression elements (7; 107), the flap drive (20) being connected to several drive stations (3, 4, 5) for adjusting the high-lift flap (2; 102). According to the invention, at least one compensation element (10; 110) is provided at least at one drive station (4) for compensation of constraining forces occurring in the drive links comprising the tension/compression elements (7; 107) due to relative movements in wing chord direction between the flap (2; 102) and the wing (1).
申请公布号 CA2656442(C) 申请公布日期 2014.10.14
申请号 CA20072656442 申请日期 2007.07.02
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 SCHLIPF, BERNHARD
分类号 B64C3/50;B64C13/30 主分类号 B64C3/50
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