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1. 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。

2. 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。

3. 发明申请

US20170350480A1 Linear Actuator with Selective Disengagement 审中-公开
公开(公告)号：US20170350480A1
公开(公告)日：2017-12-07
申请号：US15170604
申请日：2016-06-01
申请人： Darryl S. Stachniak
发明人： Darryl S. Stachniak
IPC分类号： F16H25/20
CPC分类号： F16H25/2025
摘要： An actuator is provided. The actuator includes a housing and a ram linearly movable relative to the housing. The ram is selectively mechanically coupled to a drive screw of the actuator such that in one configuration, the ram is decoupled from the drive screw to allow it to linearly move independently from rotation of the drive screw.

4. 发明授权

US09261894B2 Multiple degrees of translational adjustment pedals 有权
标题翻译：多重度的平移调整踏板
公开(公告)号：US09261894B2
公开(公告)日：2016-02-16
申请号：US13791221
申请日：2013-03-08
申请人： Darryl S. Stachniak
发明人： Darryl S. Stachniak
IPC分类号： G05G9/00 , G05G1/30 , B64C13/04 , G05G1/405 , B64C13/06
CPC分类号： G05G1/405 , B64C13/06 , Y10T74/20528
摘要： A pedal system for an aircraft comprising a pedal and a pedal mounting mechanism is provided. The pedal is configured for manipulation through at least one operational degree of freedom by a pilot to provide control inputs to the aircraft. The pedal mounting mechanism is configured for supporting the pedal within a cockpit of the aircraft for manipulation by the pilot. The pedal mounting mechanism provides at least two adjustment degrees of freedom for adjusting the position of the pedal within the cockpit.
摘要翻译：提供了一种用于包括踏板和踏板安装机构的飞机的踏板系统。踏板被配置成通过飞行员通过至少一个操作自由度进行操纵以向飞行器提供控制输入。踏板安装机构被配置为将踏板支撑在飞行器的驾驶舱内，以由飞行员操纵。踏板安装机构提供至少两个调整自由度以调节驾驶舱内踏板的位置。

5. 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。

6. 发明授权

US08814103B2 Position control system for cross coupled operation of fly-by-wire control columns 有权
标题翻译：线控控制柱交叉耦合运行的位置控制系统
公开(公告)号：US08814103B2
公开(公告)日：2014-08-26
申请号：US12844867
申请日：2010-07-28
申请人： Zenon P. Szulyk , Ganga P. Jayaraman , Charles C. Frayman , Brian P. Dyra , Darryl S. Stachniak
发明人： Zenon P. Szulyk , Ganga P. Jayaraman , Charles C. Frayman , Brian P. Dyra , Darryl S. Stachniak
IPC分类号： B64C13/04
CPC分类号： G05G11/00 , B64C13/12 , B64C13/503 , G05G5/03
摘要： A aircraft control system is provided that provides tactile feedback between control columns of the aircraft relating to discrepancies in the control inputs to the sticks of the respective control columns. In one implementation, the sticks each have an associated feedback assembly that is adjustable relative to mechanical ground to adjust the feedback profile applied to the corresponding stick. The position of each feedback assembly is adjusted based on a relative displacement between the other feedback assembly and its corresponding stick to provide active feedback relating to the control of the other control column.
摘要翻译：提供一种飞行器控制系统，其提供与飞机相关控制列的控制输入中的差异的飞机的控制列之间的触觉反馈。在一个实施方案中，棒各自具有相对于机械接地可调节的相关联的反馈组件，以调整施加到相应棒的反馈轮廓。基于其他反馈组件与其对应的杆之间的相对位移来调整每个反馈组件的位置，以提供与另一控制列的控制有关的主动反馈。

7. 发明申请

US20120160967A1 FAIL-PASSIVE VARIABLE GRADIENT CONTROL STICK DRIVE SYSTEM 有权
标题翻译：失效的可变梯度控制系统驱动系统
公开(公告)号：US20120160967A1
公开(公告)日：2012-06-28
申请号：US12976723
申请日：2010-12-22
申请人： Craig Scott , Darryl S. Stachniak
发明人： Craig Scott , Darryl S. Stachniak
IPC分类号： B64C13/46 , B64C13/50
CPC分类号： B64C13/02
摘要： A control system for an aircraft including a passive feedback arrangement, a stick and a positioning arrangement is provided that provides for user adjustability of the resistance applied to the stick, such as in a fly-by-wire system. The passive feedback arrangement is movable relative to a mechanical ground. The stick is moveable relative to the mechanical ground and the passive feedback arrangement. The passive feedback arrangement acts on the stick to resist movement of the stick relative to the passive feedback arrangement. This resistance provides passive feedback to the pilot for the fly-by-wire system. The positioning arrangement is coupled to the passive feedback arrangement for adjusting the position of the passive feedback arrangement relative to the mechanical ground in response to movement of the stick relative to the mechanical ground.
摘要翻译：提供了一种用于飞行器的控制系统，其包括被动反馈装置，杆和定位装置，其提供了用于对施加到杆的电阻的用户可调节性，例如在线控飞行系统中。无源反馈装置相对于机械地可移动。该棒可相对于机械接地和被动反馈装置移动。无源反馈装置作用在棒上以抵抗棒相对于被动反馈装置的移动。该电阻为飞行线控系统提供无源反馈。定位装置耦合到无源反馈装置，以响应于棒相对于机械接地的移动而调节无源反馈装置相对于机械接地的位置。

8. 发明授权

US06227066B1 Joystick centering device supporting multiple compound torque profiles 有权
标题翻译：支撑多个复合扭矩曲线的操纵杆定心装置
公开(公告)号：US06227066B1
公开(公告)日：2001-05-08
申请号：US09360911
申请日：1999-07-26
申请人： Darryl S. Stachniak
发明人： Darryl S. Stachniak
IPC分类号： G05G9047
CPC分类号： G05G9/047 , G05G2009/04718 , G05G2009/04725 , Y10T74/20201
摘要： A self centering, angularly displacable joystick allowing multiple compound torque profiles is provided. The self centering joystick includes a first mount and a base. The first mount located a fixed distance away from the base. The joystick extends from a restoring plate having an upper surface and a multi-faceted lower surface pivotally mounted to said first mount to partially rotate about a first axis. A linearly displaceable force plate having a substantially flat upper surface is disposed between said base and said multi-faceted surface, and a spring is provide between the base and the force plate, the spring biasing the force plate against the multi-faceted surface to provide a centering force there against. The multifaceted surface includes a center position facet oriented such that the centering force applied by the force plate is evenly distributed on each side of the first axis when said center position facet is aligned parallel with the upper surface of the force plate.
摘要翻译：提供允许多个复合扭矩曲线的自定心，角度可置换的操纵杆。自定心操纵杆包括第一安装座和底座。第一个安装座位于离基座一定距离处。操纵杆从具有上表面和多面下表面的恢复板延伸，所述下表面枢转地安装到所述第一安装件以围绕第一轴线部分旋转。具有基本上平坦的上表面的线性可移动力板设置在所述底座和所述多面平面之间，并且在所述基座和所述力板之间提供弹簧，所述弹簧将所述力板偏置抵靠所述多面平面以提供反对的中心力量。所述多面面包括中心位置小平面，所述中心位置小平面定向成使得当所述中心位置小平面与所述力板的上表面平行对准时，由所述力板施加的定心力均匀地分布在所述第一轴线的每一侧上。

9. 发明申请

US20220185453A1 RUDDER AND BRAKE PEDAL ASSEMBLY 有权
公开(公告)号：US20220185453A1
公开(公告)日：2022-06-16
申请号：US17689435
申请日：2022-03-08
申请人： Jeffrey T. Voiles , Darryl S. Stachniak , Roy Romana
发明人： Jeffrey T. Voiles , Darryl S. Stachniak , Roy Romana
IPC分类号： B64C13/04 , B64C13/10 , B64C13/18
摘要： An airplane rudder and brake pedal assembly includes a rudder arm assembly having one rudder arm with first upper and lower arm portions, and another rudder arm with second upper and lower arm portions. The rudder arm assembly is assembled to a beam at an intersection of the first upper and lower arm portions, and an intersection of the second upper and lower arm portions. The first and second rudder arms are configured to rotate about the beam at the intersection. The rotation of the first and second rudder arms is configured to adjust control surfaces that control a yaw axis of the airplane. A brake pedal is attached to the first and second lower arm portions. Rotation of the brake pedal brakes the airplane. A rotary sensor is assembled to the brake pedal and the lower arm portion, and configured to determine an extent of the brake pedal rotation.

10. 发明申请

US20140251066A1 MULTIPLE DEGREES OF TRANSLATIONAL ADJUSTMENT PEDALS 有权
标题翻译：多层次的翻译调整方案
公开(公告)号：US20140251066A1
公开(公告)日：2014-09-11
申请号：US13791221
申请日：2013-03-08
申请人： Darryl S. Stachniak
发明人： Darryl S. Stachniak
IPC分类号： G05G1/40
CPC分类号： G05G1/405 , B64C13/06 , Y10T74/20528
摘要： A pedal system for an aircraft comprising a pedal and a pedal mounting mechanism is provided. The pedal is configured for manipulation through at least one operational degree of freedom by a pilot to provide control inputs to the aircraft. The pedal mounting mechanism is configured for supporting the pedal within a cockpit of the aircraft for manipulation by the pilot. The pedal mounting mechanism provides at least two adjustment degrees of freedom for adjusting the position of the pedal within the cockpit.
摘要翻译：提供了一种用于包括踏板和踏板安装机构的飞机的踏板系统。踏板被配置成通过飞行员通过至少一个操作自由度进行操纵以向飞行器提供控制输入。踏板安装机构被配置为将踏板支撑在飞行器的驾驶舱内，以由飞行员操纵。踏板安装机构提供至少两个调整自由度以调节驾驶舱内踏板的位置。

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