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Remotely piloted helicopter and rotor head of remote control helicopter

机译:遥控直升机和遥控直升机的旋翼头

摘要

To improve the operability and to stabilize its flight operations when forming the compact and light in indoor for the R / C helicopter rotor of a single type. Is divided into a lower and upper center hub center hub center hub that supports the rotor head to the main mast, to freely set appropriately fixed angle around the axis of the main mast, respectively. I mounted for operation input from the swash plate, the phase angle of the main rotor to be output is an acute angle, so as to rotate the stabilizer and main rotor while maintaining the phase difference between the acute angle.
机译:当在室内为单一类型的R / C直升机旋翼形成紧凑而轻巧的结构时,要提高可操作性并稳定其飞行操作。分为上下中心轮毂中心轮毂,中心轮毂将转子头支撑到主桅杆,分别围绕主桅杆的轴线自由设定适当的固定角度。我安装了用于从斜盘进行操作输入的输出,要输出的主转子的相位角为锐角,以便在保持锐角之间的相位差的同时旋转稳定器和主转子。

著录项

  • 公开/公告号JPWO2009004705A1

    专利类型

  • 公开/公告日2010-08-26

    原文格式PDF

  • 申请/专利权人 ヒロボー株式会社;

    申请/专利号JP20080539180

  • 发明设计人 中村 公勇;上堀 高和;

    申请日2007-07-02

  • 分类号B64C27/72;B64C39/02;

  • 国家 JP

  • 入库时间 2022-08-21 18:57:49

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