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1. 发明申请

US20120097800A1 LINE REPLACEABLE, FLY-BY-WIRE CONTROL COLUMNS WITH PUSH-PULL INTERCONNECT RODS 有权
标题翻译：线路可更换，带按钮式互连线的双列控制柱
公开(公告)号：US20120097800A1
公开(公告)日：2012-04-26
申请号：US12910193
申请日：2010-10-22
申请人： Michael A. Burroughs , Joel M. Hutchison , Darryl S. Stachniak
发明人： Michael A. Burroughs , Joel M. Hutchison , Darryl S. Stachniak
IPC分类号： B64C13/12 , G05G9/047
CPC分类号： B64C13/10 , B64C13/12 , B64C13/503 , Y10T74/20201
摘要： A control input system is provided. The system includes a pair of control columns that are selectively interconnected such that manipulation of one of the control columns is translated to the other one of the control columns. The system includes a disconnect arrangement for each of the degrees of freedom (pitch and roll) of the system that operably disconnects the two control columns such that the two control columns can operate independently such as in the event of failure of one of the control columns. The system may also include a discontinuous force profile for a restoring force mechanism that provides tactile feedback to the pilots simulating resistance provided by control surfaces of the aircraft. The system may also include an autopilot lockout mechanism that increases the force profile experienced by the pilots when autopilot mode is entered.
摘要翻译：提供控制输入系统。该系统包括一对选择性地互连的控制列，使得控制列中的一个的操纵被转换到另一个控制列。系统包括用于系统的每个自由度（俯仰和滚动）的断开装置，其可操作地断开两个控制柱，使得两个控制列可以独立地操作，例如在控制列之一发生故障的情况下。该系统还可以包括用于向飞行员提供触觉反馈的恢复力机构的不连续力分布，该飞行员模拟由飞行器的控制表面提供的阻力。该系统还可以包括自动驾驶室锁定机构，其在进入自动驾驶模式时增加驾驶员经历的力分布。

2. 发明授权

US08469317B2 Line replaceable, fly-by-wire control columns with push-pull interconnect rods 有权
标题翻译：具有推拉式互连棒的线路可更换的线控式控制柱
公开(公告)号：US08469317B2
公开(公告)日：2013-06-25
申请号：US12910193
申请日：2010-10-22
申请人： Michael A. Burroughs , Joel M. Hutchison , Darryl S. Stachniak
发明人： Michael A. Burroughs , Joel M. Hutchison , Darryl S. Stachniak
IPC分类号： B64C13/12
CPC分类号： B64C13/10 , B64C13/12 , B64C13/503 , Y10T74/20201
摘要： A control input system is provided. The system includes a pair of control columns that are selectively interconnected such that manipulation of one of the control columns is translated to the other one of the control columns. The system includes a disconnect arrangement for each of the degrees of freedom (pitch and roll) of the system that operably disconnects the two control columns such that the two control columns can operate independently such as in the event of failure of one of the control columns. The system may also include a discontinuous force profile for a restoring force mechanism that provides tactile feedback to the pilots simulating resistance provided by control surfaces of the aircraft. The system may also include an autopilot lockout mechanism that increases the force profile experienced by the pilots when autopilot mode is entered.
摘要翻译：提供控制输入系统。该系统包括一对选择性地互连的控制列，使得控制列中的一个的操纵被转换到另一个控制列。系统包括用于系统的每个自由度（俯仰和滚动）的断开装置，其可操作地断开两个控制柱，使得两个控制列可以独立地操作，例如在控制列之一发生故障的情况下。该系统还可以包括用于向飞行员提供触觉反馈的恢复力机构的不连续力分布，该飞行员模拟由飞行器的控制表面提供的阻力。该系统还可以包括自动驾驶室锁定机构，其在进入自动驾驶模式时增加驾驶员经历的力分布。

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