首页> 外国专利> Element for control of the rotor head and command devices for rotary wing aircraft (Machine-translation by Google Translate, not legally binding)

Element for control of the rotor head and command devices for rotary wing aircraft (Machine-translation by Google Translate, not legally binding)

机译:旋翼飞机旋翼头和指挥装置的控制元件(由Google Translate进行机器翻译,无法律约束力)

摘要

Element for control of the rotor head and control devices for rotary wing aircraft, in constructional variants known as heavy structure or light structure, and structured by two resistant tubes assembled by means of fittings in slight skewing with each other on the perpendicular, supporting and all the constituent elements and components of the airplane are located in them, and which characterizes, in the execution for light structure, by comprising a rectangular base piece on which are lodged two ball joints of different size joined by two lateral plates of conical shape, the larger axis influencing the axis of rotation and affecting it in the movement in all directions on the upper rotor connected to it by a crosshead, and having an axially displaceable cardan transmission, connecting at its lower end to a box of reducing gears of the corresponding motor, while the end opposite is geared to a casting pinion solidarity to the rotor head, both sets being actuated by a control lever supported by the structural central beam by means of a guide bushing, presenting mobility in all directions and being connected by two "T" arms to two command rods ascending and interconnected to the upper base pieces (Machine-translation by Google Translate, not legally binding)
机译:用于控制旋翼飞机的旋翼头的元件和控制装置,在结构变型中被称为重型结构或轻型结构,由两个阻力管构成,这些阻力管通过在垂直方向,支撑端和所有方向上彼此稍微倾斜的配件组装而成飞机的组成元件和组件位于其中,在执行轻型结构时,其特征在于包括一个矩形底座,在底座上放置两个不同尺寸的球形接头,两个球形接头由圆锥形的侧板连接,较大的轴,它影响旋转轴,并在通过十字头连接到其的上转子的各个方向上的运动中产生影响,并具有可轴向移动的万向传动装置,该万向传动装置的下端连接到相应电动机的减速齿轮箱,而另一端与铸件小齿轮紧密配合,与转子头保持一致,两组均由控制杆驱动由结构中心梁通过导向衬套移植,具有全方位的移动性,并通过两个“ T”形臂连接到两个上升并与上部基础件互连的命令杆(Google Translate进行机器翻译,不具有法律约束力)

著录项

  • 公开/公告号ES282281U

    专利类型

  • 公开/公告日1985-04-01

    原文格式PDF

  • 申请/专利权人 SALLEN AVIACION SOCIEDAD ANONIMA;

    申请/专利号ES19840282281U

  • 发明设计人

    申请日1984-10-26

  • 分类号B64C13/00;

  • 国家 ES

  • 入库时间 2022-08-22 08:06:55

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