首页> 外国专利> REUSABLE-TYPE SPACE COMING-AND-GOING AIRCRAFT OF COMPRESSED AIR CIRCULATION TYPE OR THE LIKE LOCALLY APPLYING VERTICAL TAKEOFF AND LANDING AIRCRAFT HAVING BOTH WINGS WITH SPECIAL SAIL OF MEMBRANE TYPE AND THE LIKE USING PRINCIPALLY ARTIFICIALLY GENERATED RISING CURRENT AND A PART OF VERTICAL FLIGHT SYSTEM AND THE LIKE OF THE SAME

REUSABLE-TYPE SPACE COMING-AND-GOING AIRCRAFT OF COMPRESSED AIR CIRCULATION TYPE OR THE LIKE LOCALLY APPLYING VERTICAL TAKEOFF AND LANDING AIRCRAFT HAVING BOTH WINGS WITH SPECIAL SAIL OF MEMBRANE TYPE AND THE LIKE USING PRINCIPALLY ARTIFICIALLY GENERATED RISING CURRENT AND A PART OF VERTICAL FLIGHT SYSTEM AND THE LIKE OF THE SAME

机译:可重复使用的空间,包括压缩空气循环类型的进出飞机,或者像本地应用垂直起飞和着陆的飞机,其中两个机翼都有特殊的膜片类型,并且主要是通过使用特定的系统和特定的人工系统和一样的

摘要

PROBLEM TO BE SOLVED: To widely provide reusable-type space coming-and-going aircraft applying vertical takeoff and landing aircraft, which do not require a special high-performance (high-cost) engine and the like, and a part of a vertical flight system of a specific VTOL aircraft of the vertical takeoff and landing aircraft.;SOLUTION: An upward force not considered in the conventional method (downward ejection by means of ducted fans) when performing vertical flight of vertical takeoff and landing aircraft, which generally use the ducted fans or the like (are under development), that is, a thrust force (rising force) in the vertical direction using a rising current that is principally artificially generated is preferably added while appropriately learning a part of a flight principle of rocket overlooked heretofore. In conclusion, the principle of conservation of angular momentum operating on special rotation bodies (of impeller type or the like) arranged locally in place is applied and, moreover, the rising force naturally generated from an airframe thereof is increased (is doubled) without generating a falling force on reaction during artificial generation of the rising current.;COPYRIGHT: (C)2014,JPO&INPIT
机译:解决的问题:广泛地提供使用垂直起降飞机的可重复使用的空间进出飞机,这些飞机不需要特殊的高性能(高成本)发动机等,并且不需要垂直的一部分垂直起降飞机的特定VTOL飞机的飞行系统;解决方案:进行垂直起降飞机的垂直飞行时,常规方法未考虑的向上力(通过管道风扇向下弹出)优选地,在适当学习被忽略的火箭飞行原理的一部分的同时,添加管道风扇等(正在开发中),即,使用主要由人工产生的上升电流在垂直方向上的推力(上升力)。迄今为止。总之,采用了在局部就位的特殊旋转体(叶轮式等)上作用的角动量守恒原理,此外,从其机身自然产生的上升力增大(成倍)而不产生人工产生的上升电流对反应产生的下降力。;版权所有:(C)2014,JPO&INPIT

著录项

  • 公开/公告号JP2013248968A

    专利类型

  • 公开/公告日2013-12-12

    原文格式PDF

  • 申请/专利权人 GRACEMARIE WORLD CORP;

    申请/专利号JP20120124789

  • 发明设计人 KAMIUCHI KINGO;

    申请日2012-05-31

  • 分类号B64C29;B64G1/14;

  • 国家 JP

  • 入库时间 2022-08-21 16:17:13

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