首页> 外国专利> Tactile flight control for glider - has transducer strips up at each side of control stick with vibration providing sensory feedback

Tactile flight control for glider - has transducer strips up at each side of control stick with vibration providing sensory feedback

机译:滑翔机的触觉飞行控制-在操纵杆的每一侧都有换能器条并带有振动,可提供感官反馈

摘要

A tactile flight control has two transducer strips along the handgrip of the control stick which give tactile information related to the dynamic situation of the aircraft. In a glider the relevant information can be rate of climb or descent as well as airspeed. The transducers are linked to a control motor which provides the variable frequency and amplitude vibration, controlled from the flight instrumentation. The pilot does not have to look at the instruments to determine the aircraft attitude and can devote all his attention to flying. The tactile controls provide a rapid response and are monitored correctly even with poor visibility and in a noisy cockpit.
机译:触觉飞行控制器沿操纵杆的手柄具有两个传感器条,它们提供与飞机动态情况有关的触觉信息。在滑翔机中,相关信息可以是爬升或下降的速度以及空速。换能器连接到控制电机,该控制电机提供由飞行仪表控制的可变频率和振幅的振动。飞行员不必查看仪器即可确定飞机的姿态,而可以将所有精力投入到飞行中。触觉控件提供了快速响应,即使在可见性差且座舱嘈杂的情况下也能得到正确监控。

著录项

  • 公开/公告号DE2856892A1

    专利类型

  • 公开/公告日1980-07-17

    原文格式PDF

  • 申请/专利权人 AKADEMISCHE FLIEGERGRUPPE DARMSTADT E.V.;

    申请/专利号DE19782856892

  • 发明设计人 HORBRUEGGERHERBERT;

    申请日1978-12-30

  • 分类号B64C13/04;

  • 国家 DE

  • 入库时间 2022-08-22 17:33:46

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