首页> 外国专利> Drive system for vertical starting and horizontal flight of aircraft e.g. drone, has tilting and drive shaft over center of aircraft to propel rotor systems of aircraft in opposing directions and change tilting angle of each rotor system

Drive system for vertical starting and horizontal flight of aircraft e.g. drone, has tilting and drive shaft over center of aircraft to propel rotor systems of aircraft in opposing directions and change tilting angle of each rotor system

机译:飞机垂直启动和水平飞行的驱动系统无人机,在飞机中心上方具有倾斜和驱动轴,以沿相反方向推动飞机的旋翼系统,并改变每个旋翼系统的倾斜角度

摘要

A tilting and drive shaft (9), located over the center of the aircraft body, is connected to an engine at the cockpit and drive platform (1) via gearwheel or belt-based system. The aircraft also has two rotor systems, each with a drive ring (3,6) and four rotor blades (4,7). The tilting and drive shaft propels both rotor systems in opposite directions as well as change the tilting angle of each rotor system with respect to the horizontal. The speed of each rotor system can be changed by axially shifting the drive shaft according to engine speed change.
机译:位于飞机主体中心上方的倾斜和驱动轴(9)通过齿轮或基于皮带的系统连接至驾驶舱和驱动平台(1)上的发动机。该飞机还具有两个旋翼系统,每个旋翼系统都有一个驱动环(3,6)和四个旋翼叶片(4,7)。倾斜轴和驱动轴沿相反的方向推动两个转子系统,并改变每个转子系统相对于水平方向的倾斜角度。可以通过根据发动机转速的变化轴向移动驱动轴来改变每个转子系统的转速。

著录项

  • 公开/公告号DE102005058805A1

    专利类型

  • 公开/公告日2007-06-14

    原文格式PDF

  • 申请/专利权人 BACHELIER VOLKER;

    申请/专利号DE20051058805

  • 发明设计人 BACHELIER VOLKER;

    申请日2005-12-06

  • 分类号B64C27/10;

  • 国家 DE

  • 入库时间 2022-08-21 20:29:38

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