发明名称 AIRCRAFT WING FLAP DEVICE AND METHOD OF OPERATING THE SAME
摘要 A wing flap control system on a wing comprising at least two control plates having an opening sized to accommodate a drive shaft, a drive shaft that engages each of the openings in each of the plurality of plates, a sprocket rotatively affixed the drive shaft with the drive shaft penetrating the other control plate, at least two idler sprockets between the control plates, a chain wrapped around the sprocket and idler sprockets, a support arm rotatively coupled to the chain by a chain shoe and to a foreflap, a link arm rotatively coupled to the support arm and to a flap, where movement of the drive shaft causes the foreflap and flap to extend and retract to increase or decrease the surface area of the wing.
申请公布号 CA2898490(A1) 申请公布日期 2014.10.16
申请号 CA20142898490 申请日期 2014.01.15
申请人 OTTO, WILLIAM M. 发明人 OTTO, WILLIAM M.
分类号 B64C13/30;B64C9/04 主分类号 B64C13/30
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