发明名称 AIRCRAFT WING WITH FLAP
摘要 A vertical take-off and landing aircraft comprises a fuselage, a wing, engines, equipment, a horizontal empennage and a vertical empennage in the form of four consoles with spars, ribs, tips installed at the ends of the horizontal empennage, gear shock struts built along the end ribs of vertical empennage. At the end ribs of the vertical empennage a hinge unit is located, on which a sliding bar is mounted which is made in the form of a two-armed lever and pivoting up to connection by its upper arm to the front spar of the vertical empennage, while the above-mentioned bars are made ​​in the form of tips of the vertical empennage. The hinge unit is attached to the gear shock strut together with a spring of turting of the vertical bar.
申请公布号 UA79974(U) 申请公布日期 2013.05.13
申请号 UA20120012610U 申请日期 2012.11.05
申请人 NATIONAL AVIATION UNIVERSITY 发明人 KHARCHENKO VOLODYMYR PETROVYCH;SVIASCHENKO YURII IVANOVYCH
分类号 B64C3/48 主分类号 B64C3/48
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