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发明申请
US20120234985A1 CYCLIC STICK FOR MECHANICALLY TRANSMITTING COMMANDS FOR CONTROLLING A ROTORCRAFT, THE STICK HAVING A LEVER ARM THAT IS AMPLIFIED SELECTIVELY IN THE EVENT OF AN EMERGENCY 有权
用于控制旋转机械的机械传动指令的循环线，具有在紧急情况下选择性极限的杆的手柄

  • 专利标题： CYCLIC STICK FOR MECHANICALLY TRANSMITTING COMMANDS FOR CONTROLLING A ROTORCRAFT, THE STICK HAVING A LEVER ARM THAT IS AMPLIFIED SELECTIVELY IN THE EVENT OF AN EMERGENCY
  • 专利标题（中）： 用于控制旋转机械的机械传动指令的循环线，具有在紧急情况下选择性极限的杆的手柄
  • 申请号： US13411950
    申请日： 2012-03-05
  • 公开(公告)号： US20120234985A1
    公开(公告)日： 2012-09-20
  • 发明人: Romuald Biest , Robert Convers
  • 申请人： Romuald Biest , Robert Convers
  • 申请人地址： FR Marignane
  • 专利权人： EUROCOPTER
  • 当前专利权人： EUROCOPTER
  • 当前专利权人地址： FR Marignane
  • 优先权： FR1100820 20110318
  • 主分类号： B64C13/14
  • IPC分类号： B64C13/14
CYCLIC STICK FOR MECHANICALLY TRANSMITTING COMMANDS FOR CONTROLLING A ROTORCRAFT, THE STICK HAVING A LEVER ARM THAT IS AMPLIFIED SELECTIVELY IN THE EVENT OF AN EMERGENCY
摘要：
The invention provides a control mechanism for controlling flight of an aircraft, the control mechanism comprising a cyclic control stick (1) that is mounted to tilt (B1, B2) on a carrier structure (4) and that is in engagement with remote mechanical transmission members (2, 3). The stick (1) is arranged as a telescopic member provided with locking means (20) for locking it in a normal-use retracted position, and is equipped with deployment means (21). Unlocking of the locking means (20) and use of the deployment means (21) depend on an assistance device (17) associated with the stick (1) being in a defective state. In the event of such a defective state being detected, the stick (1) is suitable for being deployed so as to increase the comfort of the pilot while manipulating it.
摘要（中）：

本发明提供了一种用于控制飞行器飞行的控制机构，该控制机构包括一个循环控制杆（1），该循环控制杆安装成在载体结构（4）上倾斜（B1，B2）并与远程机械传动 会员（2,3）。 杆（1）被布置为具有用于将其锁定在正常使用的缩回位置的锁定装置（20）的伸缩构件，并且配备有展开装置（21）。 锁定装置（20）的解锁和展开装置（21）的使用取决于与棒（1）相关联的辅助装置（17）处于缺陷状态。 在检测到这样的缺陷状态的情况下，棒（1）适于被部署，以便在操纵该飞行员的同时增加飞行员的舒适性。

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