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3-wing rotor of model helicopter using elastic force of rubber band

机译:利用橡皮筋弹力的直升机模型三翼旋翼

摘要

The present invention relates to a structure of a model helicopter, in which a real helicopter drives a rotor located at a tail portion of a fuselage to prevent the fuselage from rotating due to rotation of the rotor due to rotation of the rotor located at the upper end of the fuselage, A 3-wing rotor of the same size as a 3-wing rotor located at the upper end of the fuselage at the lower part of the fuselage without the rotor of the tail part is mounted so that the direction of the wing of the rotor is opposite and the center of the two rotors is connected by a single rubber band. The generated restoring force acts on each of the rotors located at the upper and lower ends in the same direction and rotates in the directions opposite to each other, thereby canceling the rotational forces of the rotors on the helicopter's fuselage to cancel each other so that the fuselage of the helicopter does not rotate, To increase the number of
机译:直升飞机模型的结构技术领域本发明涉及直升飞机模型的结构,其中,实际的直升飞机驱动位于机身尾部的旋翼,以防止由于位于上部的旋翼的旋转而使旋翼的机身旋转。机身末端安装了一个3翼旋翼,其尺寸与位于机身下部的机身上端的3翼旋翼的尺寸相同,但没有尾部旋翼,因此转子的机翼相对,两个转子的中心通过一条橡皮筋相连。产生的恢复力沿相同方向作用于位于上端和下端的每个转子,并沿彼此相反的方向旋转,从而抵消了直升机机身上转子的旋转力,从而使彼此抵消,从而使直升机的机身不旋转,要增加数量

著录项

  • 公开/公告号KR19990014324U

    专利类型

  • 公开/公告日1999-04-26

    原文格式PDF

  • 申请/专利权人 장순욱;

    申请/专利号KR19980028205U

  • 发明设计人 장순욱;

    申请日1998-12-31

  • 分类号A63H27/22;

  • 国家 KR

  • 入库时间 2022-08-22 02:14:22

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