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Universal aeroplane with electric drive

机译:带电驱动的通用飞机

摘要

Universal aeroplane with electric driveo with passenger cabin (10,11,2),o with carrying surfaces (3, 6, 7,25),o with tilt -rotors in rotation (4,5)o with adjusting organs and shafts (8) by which the tilting rotors can be adjusted in their tilting angle position, as required;o with an electronic control for the speed and angular position of the tilting rotors,o with stowage compartments for the lower passenger compartment performance batteries, characterized by the fact that the carrying surfaces (3,6,7) with the tiltrotators (4,5) in the upper part of the passenger compartment, the tilt -rotors (12) shall be fitted with propellers (5);whose leaf lengths are optimized in a vertical direction when the tilters are positioned in a bold position so that they do not touch the floor of the runway.
机译:带电驱动的通用飞机o带客舱(10,11,2),o具有承载面(3,6,7,25),o倾斜-旋转中的转子(4,5)o带有调节机构和轴(8),根据需要,调节机构和轴(8)可以将倾斜转子调节到其倾斜角度位置;o通过电子控制倾斜转子的速度和角位置,o具有用于下部乘客舱功能电池的储物舱,其特征在于,在乘客舱上部带有倾斜旋转器(4,5)的承载面(3,6,7),倾斜旋转器(12 )应装有螺旋桨(5);当倾斜器置于粗体位置时,其叶片长度应在垂直方向上进行优化,以使它们不接触跑道地板。

著录项

  • 公开/公告号DE202019000936U1

    专利类型

  • 公开/公告日2019-05-16

    原文格式PDF

  • 申请/专利权人 SIEGFRIED ALEXANDER EISENMANN;

    申请/专利号DE202019000936U1

  • 发明设计人

    申请日2019-02-26

  • 分类号B64C27/28;B64C29;B64D27/24;

  • 国家 DE

  • 入库时间 2022-08-21 11:44:09

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