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1. 发明授权

US09051045B2 Indirect drive active control column 有权
标题翻译：间接驱动主动控制列
公开(公告)号：US09051045B2
公开(公告)日：2015-06-09
申请号：US12845160
申请日：2010-07-28
申请人： Darryl S. Stachniak , Thomas M. Rusak , Brian P. Dyra
发明人： Darryl S. Stachniak , Thomas M. Rusak , Brian P. Dyra
IPC分类号： B64C13/12 , B64C13/50 , B64C13/04 , G05G5/03 , G05G11/00
CPC分类号： B64C13/503 , B64C13/04 , B64C13/12 , G05G5/03 , G05G11/00
摘要： An indirect drive active control column for an aircraft control system is provided. The indirect drive active control column provides both active and passive feedback to the control stick. The passive feedback relates to adjustments of the control stick relative to a feedback neutral position. The active feedback actively adjusts the position of the feedback neutral position to adjust a feedback profile of the passive feedback.
摘要翻译：提供了一种用于飞机控制系统的间接驱动主动控制柱。间接驱动主动控制列为控制杆提供主动和无源反馈。无源反馈涉及控制棒相对于反馈中性位置的调节。主动反馈主动调整反馈中性位置的位置，以调整无源反馈的反馈曲线。

2. 发明申请

US20120025030A1 Indirect Drive Active Control Column 有权
标题翻译：间接驱动器主动控制列
公开(公告)号：US20120025030A1
公开(公告)日：2012-02-02
申请号：US12845160
申请日：2010-07-28
申请人： Darryl S. Stachniak , Thomas M. Rusak , Brian P. Dyra
发明人： Darryl S. Stachniak , Thomas M. Rusak , Brian P. Dyra
IPC分类号： B64C13/04
CPC分类号： B64C13/503 , B64C13/04 , B64C13/12 , G05G5/03 , G05G11/00
摘要： An indirect drive active control column for an aircraft control system is provided. The indirect drive active control column provides both active and passive feedback to the control stick. The passive feedback relates to adjustments of the control stick relative to a feedback neutral position. The active feedback actively adjusts the position of the feedback neutral position to adjust a feedback profile of the passive feedback.
摘要翻译：提供了一种用于飞机控制系统的间接驱动主动控制柱。间接驱动主动控制列为控制棒提供主动和无源反馈。无源反馈涉及控制棒相对于反馈中性位置的调节。主动反馈主动调整反馈中性位置的位置，以调整无源反馈的反馈曲线。

3. 发明授权

US09405312B2 Active control column with manually activated reversion to passive control column 有权
标题翻译：主动控制列手动启动回归到被动控制列
公开(公告)号：US09405312B2
公开(公告)日：2016-08-02
申请号：US12845246
申请日：2010-07-28
申请人： Darryl S. Stachniak , Thomas M. Rusak
发明人： Darryl S. Stachniak , Thomas M. Rusak
IPC分类号： G05G5/03 , B64C13/12 , B64C13/50 , G05G11/00
CPC分类号： G05G5/03 , B64C13/12 , B64C13/503 , G05G11/00 , Y10T29/49716
摘要： An active control column transitionable to a fully passive state for an aircraft and methods of use are provided. The control column includes a passive feedback arrangement, a stick and a ground lock mechanism is provided. The passive feedback arrangement is moveable relative to a mechanical ground to adjust a feedback profile provided to the stick. The stick is movable relative to the mechanical ground and the passive feedback arrangement. The ground lock mechanism has a locked state in which the passive feedback arrangement is maintained in a fixed position relative to the mechanical ground. This places the control column in a fully passive state. The ground lock mechanism also has a normal state in which the passive feedback arrangement is permitted to move relative to the mechanical ground such that active feedback can be provided to the stick.
摘要翻译：提供了可转换到飞行器的完全被动状态的主动控制列和使用方法。控制柱包括无源反馈装置，提供棒和地锁机构。无源反馈装置可相对于机械地移动以调节提供给棒的反馈曲线。该棒可相对于机械接地和被动反馈装置移动。接地锁定机构具有锁定状态，其中无源反馈装置相对于机械接地保持在固定位置。这将使控制列处于完全被动状态。接地锁定机构还具有正常状态，其中无源反馈装置被允许相对于机械接地移动，使得能够向棒提供主动反馈。

4. 发明申请

US20120025031A1 Active Control Column With Manually Activated Reversion to Passive Control Column 有权
标题翻译：主动控制列手动激活返回到被动控制列
公开(公告)号：US20120025031A1
公开(公告)日：2012-02-02
申请号：US12845246
申请日：2010-07-28
申请人： Darryl S. Stachniak , Thomas M. Rusak
发明人： Darryl S. Stachniak , Thomas M. Rusak
IPC分类号： B64C13/04 , B23P17/00
CPC分类号： G05G5/03 , B64C13/12 , B64C13/503 , G05G11/00 , Y10T29/49716
摘要： An active control column transitionable to a fully passive state for an aircraft and methods of use are provided. The control column includes a passive feedback arrangement, a stick and a ground lock mechanism is provided. The passive feedback arrangement is moveable relative to a mechanical ground to adjust a feedback profile provided to the stick. The stick is movable relative to the mechanical ground and the passive feedback arrangement. The ground lock mechanism has a locked state in which the passive feedback arrangement is maintained in a fixed position relative to the mechanical ground. This places the control column in a fully passive state. The ground lock mechanism also has a normal state in which the passive feedback arrangement is permitted to move relative to the mechanical ground such that active feedback can be provided to the stick.
摘要翻译：提供了可转换到飞行器的完全被动状态的主动控制列和使用方法。控制柱包括无源反馈装置，提供棒和地锁机构。无源反馈装置可相对于机械地移动以调节提供给棒的反馈曲线。该棒可相对于机械接地和被动反馈装置移动。接地锁定机构具有锁定状态，其中无源反馈装置相对于机械接地保持在固定位置。这将使控制列处于完全被动状态。接地锁定机构还具有正常状态，其中无源反馈装置被允许相对于机械接地移动，使得能够向棒提供主动反馈。

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