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GROUND EFFECT WING, ROTARY WING, ROTARY WING AIRCRAFT, AND FIXED WING AIRCRAFT

机译:地效翼,旋转翼,旋转翼飞机和固定翼飞机

摘要

PROBLEM TO BE SOLVED: To provide a ground effect wing capable of obtaining sufficient ground effect at a low speed, and an aircraft, a rotary wing aircraft and a ground effect wing aircraft equipped with the ground effect wing.;SOLUTION: The ground effect wing comprises a main wing 1 generating lift by advancing in a predetermined direction and a leading edge flap wing 10 disposed in front in the direction of the main wing 1 and introducing an airstream to below the main wing 1 by advancing in the direction.;COPYRIGHT: (C)2010,JPO&INPIT
机译:要解决的问题:提供一种能够在低速下获得足够地面效果的地效机翼,以及配备有该地效机翼的飞机,旋翼飞机和地效机翼飞机;解决方案:地效机翼包括:主翼1,其通过沿预定方向前进来产生升力;以及前缘襟翼10,其布置在主翼1的方向上的前方,并且通过沿该方向前进而将气流引入到主翼1的下方。 (C)2010,日本特许厅&INPIT

著录项

  • 公开/公告号JP2009286345A

    专利类型

  • 公开/公告日2009-12-10

    原文格式PDF

  • 申请/专利权人 TOKYO UNIV OF SCIENCE;

    申请/专利号JP20080143055

  • 发明设计人 OGAWA NOBUO;

    申请日2008-05-30

  • 分类号B60V3/08;B64C27/467;

  • 国家 JP

  • 入库时间 2022-08-21 19:02:16

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