首页> 外国专利> Drive system for e.g. ultra-light aircraft, has gear-wheels standing in engagement at bevel-gears of blades, and electro-motors driving wheels independent of each other, where blades are rotatably supported for adjusting engaging angles

Drive system for e.g. ultra-light aircraft, has gear-wheels standing in engagement at bevel-gears of blades, and electro-motors driving wheels independent of each other, where blades are rotatably supported for adjusting engaging angles

机译:驱动系统例如超轻型飞机,其齿轮啮合在叶片的锥齿轮上,电动机驱动彼此独立的轮子,其中叶片可旋转地支撑着调节啮合角度

摘要

The system has a variable pitch propeller with a symmetrical axis (1) and three blades (10), which are rotatably supported for adjusting blade engaging angles along a longitudinal axis of the blades and exhibit bevel-gears (11). Two drive gear wheels (45, 55) are arranged at the symmetrical axis and stand in engagement at the bevel-gears of the blades. Two electro-motors (40, 50) are connected with the gear-wheels, which are driven by the electro-motors independent of each other.
机译:该系统具有可变螺距螺旋桨,​​该螺旋桨具有对称的轴线(1)和三个叶片(10),它们可旋转地支撑着,用于调节沿叶片纵轴的叶片啮合角,并具有锥齿轮(11)。两个驱动齿轮(45、55)布置在对称轴上,并在叶片的锥齿轮上啮合。两个电动机(40、50)与齿轮连接,齿轮由彼此独立的电动机驱动。

著录项

  • 公开/公告号DE102006007915A1

    专利类型

  • 公开/公告日2007-08-30

    原文格式PDF

  • 申请/专利权人 BADER INGO;

    申请/专利号DE20061007915

  • 发明设计人 BADER INGO;

    申请日2006-02-16

  • 分类号B64C11/30;B63H1/06;B63H3/00;

  • 国家 DE

  • 入库时间 2022-08-21 20:29:22

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