首页> 外国专利> Contrarotative rotor integrated vertical takeoff and landing flying machine e.g. reduced helicopter module, has orientation module mounted on frame and comprising orientation unit to pivot contrarotative motor around pitch and rolling axes

Contrarotative rotor integrated vertical takeoff and landing flying machine e.g. reduced helicopter module, has orientation module mounted on frame and comprising orientation unit to pivot contrarotative motor around pitch and rolling axes

机译:同向旋翼一体式垂直起降飞行器,例如简化的直升飞机模块,具有安装在框架上的定向模块,并包括定向单元,以使俯仰轴和滚动轴使反向旋转的电动机旋转

摘要

The machine (100) has a frame (102), and a motor (104) comprising a lower output shaft (106) and an upper output shaft (108). A lower assembly of blades is fixed to the lower output shaft, and an upper assembly of blades is fixed to the upper output shaft. An orientation module (150) is mounted on the frame, and the motor is fixed on the module. The module includes an orientation unit to pivot the motor around a pitch axis (156) and a rolling axis (160). The orientation unit comprises a plate (302) mounted on the frame via a pivot link around the pitch axis.
机译:机器(100)具有框架(102)和包括下部输出轴(106)和上部输出轴(108)的电动机(104)。下部叶片组件固定到下部输出轴,上部叶片组件固定到上部输出轴。定向模块(150)安装在框架上,电机固定在模块上。该模块包括定向单元,以使电动机绕俯仰轴线(156)和滚动轴线(160)枢转。定向单元包括板(302),该板通过绕俯仰轴的枢轴连接安装在框架上。

著录项

  • 公开/公告号FR2980117A1

    专利类型

  • 公开/公告日2013-03-22

    原文格式PDF

  • 申请/专利权人 VIGUIER FRANCOIS;

    申请/专利号FR20110058251

  • 发明设计人 VIGUIER FRANCOIS;

    申请日2011-09-16

  • 分类号A63H27/133;

  • 国家 FR

  • 入库时间 2022-08-21 16:21:07

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