首页> 外国专利> ANTI ROTATION APPARATUS FOR MAIN ROTER OF MODEL HELICOPTER

ANTI ROTATION APPARATUS FOR MAIN ROTER OF MODEL HELICOPTER

机译:模型直升机主旋翼的防转装置

摘要

An anti-rotation apparatus for a main rotor of a model helicopter is provided to prevent a main rotor from being rotated even if an engine is started and an accelerating lever is operated to prevent an accident. A model helicopter includes a main rotor(161) that rotates a main blade by receiving engine power and has a space portion(163) formed therein. The main rotor and a main shaft(160) are supported by a bracket. A hole is formed on a bracket(200) supporting the main rotor, and a pin(205) is installed to make the lower end thereof inserted into the space portion through the hole(202) to control the rotation of the main rotor. A gear portion is formed on the upper part of the pin. A separate motor gear is engaged with the gear portion to perform the vertical motion of the pin.
机译:提供了一种用于模型直升机的主旋翼的防旋转装置,以即使在发动机启动并且操作加速杆以防止事故的情况下也防止主旋翼旋转。一种模型直升机,包括主转子(161),该主转子通过接收发动机动力来旋转主叶片,并具有形成在其中的空间部分(163)。主转子和主轴(160)由支架支撑。在支撑主转子的托架(200)上形成孔,并且安装销(205)以使其下端通过孔(202)插入空间部分,以控制主转子的旋转。在销的上部形成有齿轮部。单独的电动机齿轮与齿轮部分啮合,以执行销的垂直运动。

著录项

  • 公开/公告号KR20070119417A

    专利类型

  • 公开/公告日2007-12-20

    原文格式PDF

  • 申请/专利权人 LEE CHONG SOO;

    申请/专利号KR20060054034

  • 发明设计人 LEE CHONG SOO;

    申请日2006-06-15

  • 分类号A63H27/133;

  • 国家 KR

  • 入库时间 2022-08-21 19:54:41

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