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FLAPPING MODELPLANE OF NON-STATIONARY TYPE FLAPPING WING

机译:非固定式扑翼的扑翼模型

摘要

PROBLEM TO BE SOLVED: To solve the problems of a conventional flapping modelplane that the backbone sections of flapping wing surface are fixed and the difference between the ascent quantity acquired by stroking down of the flapping wings and the descent quantity arising by stroking up is small and then the ascent performance is poor.;SOLUTION: The backbone sections of the flapping wings of this modelplane are non-fixed to minimize the descent loss arising during the stroking up of the flapping wings, by which the ascent performance is tremendously improved. In order to achieve this purpose, the conventional fixed wings, backbones and rear braces are eliminated and in turn, a material, such as a leaf spring, having elasticity is adopted for the backbone section and a main wing trailing edge material provided with a trailing edge height adjusting thread capable of freely setting the trailing edge height of the wings is connected to the rear end of this spring.;COPYRIGHT: (C)2002,JPO
机译:要解决的问题:为了解决传统的襟翼模型飞机的问题,即襟翼表面的主干部分是固定的,并且通过向下挥动襟翼获得的上升量与通过向上挥动产生的下降量之间的差异较小,并且解决方案:此模型飞机的襟翼的主干部分未固定,以最大程度地减小在襟翼抬起时产生的下降损失,从而极大地提高了上升性能。为了实现该目的,省去了常规的固定机翼,主干和后支架,并且,主干部分采用了具有弹性的材料,例如板簧,主翼后缘材料设有尾翼。可以自由设定机翼后缘高度的边缘高度调节线连接到该弹簧的后端。;版权所有:(C)2002,JPO

著录项

  • 公开/公告号JP2002085860A

    专利类型

  • 公开/公告日2002-03-26

    原文格式PDF

  • 申请/专利权人 TAKATANI YOHEI;

    申请/专利号JP20000317198

  • 发明设计人 TAKATANI YOHEI;

    申请日2000-09-11

  • 分类号A63H27/28;A63H27/18;

  • 国家 JP

  • 入库时间 2022-08-22 00:56:37

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