发明名称 Modified biplane aircraft with increased lift
摘要 The small-span extra support wing (5) can be displaced over the fuselage (2) via rollers under a U-shaped rail in controlled manner w.r.t. the centre of gravity of the aircraft. The extra wing may have grooves (6) on its underside and may have extending flaps. The lower support wing (4), is usually of wider span than the top wing. It has at its tips downwards pointing end plates (4a), or stabilisers. The whole assembly provides a biplane aircraft with improved reliability and low takeoff and landing speeds.
申请公布号 DE19500412(A1) 申请公布日期 1996.08.14
申请号 DE19951000412 申请日期 1995.01.10
申请人 SCHUBERT, WERNER, DR.MED., 45468 MUELHEIM, DE 发明人 SCHUBERT, WERNER, DR.MED., 45468 MUELHEIM, DE
分类号 B64C3/00;B64C39/08;(IPC1-7):B64C39/08;B64C3/16;B64C3/38;B64C5/08;B64C15/02 主分类号 B64C3/00
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