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Wing Self-transformation Type Turbine

机译:机翼自转化式涡轮机

摘要

Conventional fixed blade turbines have a smooth angle at a certain angle of attack, so that the pressure of the water flow acting is inevitably dispersed, and is particularly typical for fixed blades on the wing of the retrograde trajectory. There was no way to solve the rotational resistance in the reverse direction, which was found to be relatively low driving efficiency.;The present invention has been made to solve the problem of the inefficient angle of attack of the conventional fixed blade turbine, and the rotation of the rotary substrate (turbine) in which the drive shaft is fixed in a vertical rotary shaft (turbine) Several eccentric rotary vanes are mounted at the edges so that this eccentric variable vane can exert its own maximum driving force according to each trajectory position corresponding to the flow of fluid. By maintaining the angle of attack of the turbine, the turbine in such an attempt can exhibit maximum angular velocity (rpm) and torque performance even with relatively slow fluid flows, such as wind and tidal currents. It relates to an eccentric variable wing turbine characterized in that it is greatly improved.
机译:常规的固定叶片涡轮在一定的迎角下具有光滑的角度,从而不可避免地分散了作用的水流的压力,并且这对于逆行轨迹的机翼上的固定叶片而言尤其典型。没有办法解决反方向的旋转阻力,这被认为是相对较低的驱动效率。;已经做出本发明以解决常规固定叶片涡轮的低攻角的问题,并且将驱动轴固定在垂直旋转轴(涡轮)中的旋转基板(涡轮)的旋转在边缘处安装了几个偏心旋转叶片,以便该偏心可变叶片可以根据每个轨迹位置施加其自身的最大驱动力对应于流体的流动。通过保持涡轮的迎角,即使在相对较慢的流体流(例如风和潮流)下,这种尝试中的涡轮也可以表现出最大角速度(rpm)和扭矩性能。本发明涉及一种偏心可变翼涡轮,其特征在于它得到了极大的改进。

著录项

  • 公开/公告号KR19990078593A

    专利类型

  • 公开/公告日1999-11-05

    原文格式PDF

  • 申请/专利权人 황용안;

    申请/专利号KR19990022804

  • 发明设计人 황용안;

    申请日1999-06-14

  • 分类号F04D29/30;

  • 国家 KR

  • 入库时间 2022-08-22 02:16:35

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