首页> 外国专利> DEVICE FOR MANAGING THE MECHANICAL ENERGY OF AN AIRCRAFT WITH A FORCE APPLICATION SYSTEM IN A CONTROL LEVER, RELATED AIRCRAFT AND PROCESS

DEVICE FOR MANAGING THE MECHANICAL ENERGY OF AN AIRCRAFT WITH A FORCE APPLICATION SYSTEM IN A CONTROL LEVER, RELATED AIRCRAFT AND PROCESS

机译:用力控制系统控制飞机的机械能的装置,相关的飞机和过程

摘要

device (12) comprises: - a support (40) defining a guide; - a movable control lever (30) for controlling the variation of a mechanical energy variation of the aircraft (10) movably mounted through the guide; - at least one position sensor (42) which detects the position of the movable lever (30) in the guide, capable of creating position information for the position of the movable lever (30) in the guide intended to be sent to a control unit. flight (18) of the aircraft (10). The device also includes an active system (44) for applying a force to the movable lever (30) capable of generating a force applied to the movable lever (30). The force depends on the position of the movable lever (30) in the guide.
机译:装置(12)包括:-限定引导件的支撑件(40); -可移动的控制杆(30),用于控制通过导向装置可移动地安装的飞机(10)的机械能变化。 -至少一个位置传感器(42),其检测可移动杆(30)在导向装置中的位置,能够为该可移动杆(30)在导向装置中的位置创建位置信息,该位置信息将被发送到控制单元。飞机(10)的飞行(18)。该装置还包括主动系统(44),用于将力施加到可动杆(30),该系统能够产生施加到可动杆(30)的力。该力取决于可动杆(30)在导向装置中的位置。

著录项

  • 公开/公告号BR102017024209A2

    专利类型

  • 公开/公告日2018-05-29

    原文格式PDF

  • 申请/专利权人 DASSAULT AVIATION;

    申请/专利号BR20171024209

  • 发明设计人 ERIC GRANIER;JÉRÔME LE BORLOCH;

    申请日2017-11-10

  • 分类号B64C13/12;B64C13/24;

  • 国家 BR

  • 入库时间 2022-08-21 12:53:57

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