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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。

3. 发明申请

US20120176124A1 Method and Apparatus for a Half-Bridge Variable Differential Transformer Position Sensing System 有权
标题翻译：半桥可变差动变压器位置传感系统的方法与装置
公开(公告)号：US20120176124A1
公开(公告)日：2012-07-12
申请号：US13345048
申请日：2012-01-06
申请人： Zenon P. Szulyk , Ganga P. Jayaraman , Brian M. Hahn
发明人： Zenon P. Szulyk , Ganga P. Jayaraman , Brian M. Hahn
IPC分类号： G01B7/14
CPC分类号： G01B7/003
摘要： A half-bridge variable differential transformer position sensing system that includes a transducer having a stator with an inductive coil having a center tap configured to provide an output signal. The transducer also has an armature with a magnetically permeable core configured to move within the inductive coil, such that movement of the magnetically permeable core causes a change in the output signal. The position sensing system includes a first circuit configured to provide an excitation signal at one terminal of the inductive coil. The system includes no more than three electrical interface wires, and a microcontroller configured to calculate the degree of change in the position of the magnetically permeable core, and is configured to correct for variations in the voltage of the output signal due to the temperature of the transducer and due to non-linear effects on the output signal caused by movement of the magnetically permeable core.
摘要翻译：一种半桥可变差分变压器位置传感系统，其包括具有定子的换能器，所述定子具有感应线圈，所述感应线圈具有构造成提供输出信号的中心抽头。换能器还具有一个具有导磁芯的电枢，该磁芯构造成在感应线圈内移动，使得导磁芯的运动导致输出信号的变化。位置检测系统包括被配置为在感应线圈的一个端子处提供激励信号的第一电路。该系统包括不超过三个电接口导线，以及被配置为计算导磁芯位置的变化程度的微控制器，并且被配置为校正输出信号的电压由于温度的变化并且由于导磁芯的运动引起的对输出信号的非线性影响。

4. 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。

5. 发明授权

US09581226B2 Barrel cam rudder pedal system 有权
标题翻译：桶凸轮方向舵踏板系统
公开(公告)号：US09581226B2
公开(公告)日：2017-02-28
申请号：US14721754
申请日：2015-05-26
申请人： Anton A. Petrou , Maciej J. Piotrowski
发明人： Anton A. Petrou , Maciej J. Piotrowski
IPC分类号： B64C13/04 , F16H25/12
CPC分类号： F16H25/12 , B64C13/04 , B64C13/06 , B64C27/56 , Y02T50/44
摘要： A barrel cam rudder pedal system is provided. The system includes an outer housing with a chassis assembly carried by the outer housing. A barrel cam arrangement is rotationally mounted within an interior space of the chassis assembly. A pair of pedal assemblies is mechanically coupled to the barrel cam arrangement such that linear movement of either of the pair of pedal assemblies results in a rotation of the barrel cam arrangement about a central longitudinal axis defined by the barrel cam arrangement.
摘要翻译：提供桶式舵舵踏板系统。该系统包括具有由外壳承载的底盘组件的外壳。桶形凸轮装置旋转地安装在底盘组件的内部空间内。一对踏板组件机械地联接到筒形凸轮装置，使得一对踏板组件中的任何一个的直线运动导致圆筒凸轮装置围绕由筒形凸轮装置限定的中心纵向轴线的旋转。

6. 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。

7. 发明授权

US09423128B2 Control system for exhaust gas fan system 有权
标题翻译：废气风机系统控制系统
公开(公告)号：US09423128B2
公开(公告)日：2016-08-23
申请号：US12863328
申请日：2008-12-19
申请人： Charles Alexander Gans , Paul A. Tetley , Brian Jay Merritt
发明人： Charles Alexander Gans , Paul A. Tetley , Brian Jay Merritt
IPC分类号： F24F7/007 , F23L17/00 , B08B15/00 , F24F7/02 , F24F11/00 , F24F11/02
CPC分类号： F24F7/025 , B08B15/002 , F23L17/005 , F24F11/72 , F24F11/77 , F24F13/10 , F24F13/26 , F24F2110/40 , Y02B30/746
摘要： Systems and methods for controlling an exhaust gas fan system. The control system may control one or more components of the exhaust system to optimize system performance and improve energy efficiency. The control system may be designed to maintain a substantially constant pressure in the exhaust header and provide a substantially constant flow through the exhaust fans. The control system may include software and hardware that allow the control system to control one or more of: modulation of one or more by-pass dampers; adjustment of the nozzle outlet area; varying the speed of the fans; the number and staging of fans. By utilizing and controlling one or more of these functions, the amount of energy being used may be minimized/optimized.
摘要翻译：用于控制废气风扇系统的系统和方法。控制系统可以控制排气系统的一个或多个部件以优化系统性能并提高能量效率。控制系统可以设计成在排气集管中保持基本上恒定的压力，并提供通过排气风扇的基本恒定的流量。控制系统可以包括允许控制系统控制一个或多个：一个或多个旁路减振器的调制的软件和硬件; 调整喷嘴出口面积; 改变风扇的速度; 球迷的数量和分期。通过利用和控制这些功能中的一个或多个，所使用的能量的量可以被最小化/优化。

8. 发明授权

US09347456B2 Non-metallic vertical turbine pump 有权
标题翻译：非金属立式涡轮泵
公开(公告)号：US09347456B2
公开(公告)日：2016-05-24
申请号：US13211929
申请日：2011-08-17
申请人： William W. Parry , Erik Burachinsky
发明人： William W. Parry , Erik Burachinsky
IPC分类号： F04D29/02 , F04D13/08 , B29C33/52 , B29C70/30 , B29D99/00 , F04D29/22 , F04D29/44 , B29L31/00
CPC分类号： F01D5/282 , B29C33/3842 , B29C33/40 , B29C33/52 , B29C70/06 , B29C70/30 , B29C70/46 , B29C70/48 , B29D99/0025 , B29K2031/00 , B29K2063/00 , B29K2105/06 , B29K2309/08 , B29K2995/0063 , B29K2995/007 , B29L2031/08 , B29L2031/7504 , F01D5/147 , F01D9/041 , F04D13/08 , F04D29/026 , F04D29/2227 , F04D29/448 , F05C2253/04 , F05D2220/30 , F05D2230/21 , F05D2260/95 , F05D2300/43 , F05D2300/44 , F05D2300/603
摘要： A non-metallic vertical turbine pump and a method of manufacturing same are provided. In accordance with one embodiment, the vertical turbine pump can include a motor, and a drive shaft coupled to the motor for rotation, a casing with a mixed flow diffuser including a diffuser hub and diffuser vanes that project out from the diffuser hub, and a mixed flow impeller configured to rotatably fit inside the casing, having an impeller hub, impeller vanes, extending from the hub, and a front and a back shroud connected to opposing ends of the impeller vanes. At least one of the mixed flow impeller and the mixed flow diffuser can be made of a non-metallic material and is a singular homogenous component.
摘要翻译：提供一种非金属立式涡轮泵及其制造方法。根据一个实施例，垂直涡轮泵可以包括马达和联接到马达以用于旋转的驱动轴，具有混合流动扩散器的壳体，其包括扩散器毂和从扩散器毂突出的扩散器叶片，以及混合流动叶轮，其构造成可旋转地装配在壳体内，具有叶轮毂，从轮毂延伸的叶轮叶片，以及连接到叶轮叶片的相对端的前后罩。混合流动叶轮和混合流动扩散器中的至少一个可以由非金属材料制成，并且是单一均匀的组分。

9. 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。

10. 发明申请

US20130105634A1 COMPACT TWO AXIS GIMBAL FOR CONTROL STICK 有权
标题翻译：紧凑型双轴吉他控制杆
公开(公告)号：US20130105634A1
公开(公告)日：2013-05-02
申请号：US13657294
申请日：2012-10-22
申请人： Woodward MPC, Inc.
发明人： Matthew P. DeCraene , Matthew Kramer , Nathan Thompson , Anton Petrou
IPC分类号： B64C13/04
CPC分类号： B64C13/04 , B64C13/46 , G05G5/03 , G05G9/047 , G05G2009/04718
摘要： An electromechanical portion of the control stick includes a two-axis gimbal, with each axis including a mechanical gimbal structure supported by rolling element bearings, cam based centering mechanisms, linkages to connect a geared power-drive including a resolver commutated brushless DC motor and compound-planetary gearhead to provide active force feedback, and several electrically independent RVDT position sensors. The gearing architecture uses a fixed-cage, rotating internal gear arrangement on a planetary gearhead, which may be single or multi-stage. The output torque of the gearhead is provided by a feature on the outer housing of the rotating internal ring gear, allowing an axial placement of the entire power-drive in a more central location, reducing the moment load on the gearhead output cage bearings, and facilitating a compact drive arrangement of the gimbal using linkages. Additionally, a common power-drive can be used for both the roll and pitch axes.
摘要翻译：控制杆的机电部分包括双轴万向架，每个轴包括由滚动元件轴承支撑的机械万向架结构，基于凸轮的定心机构，用于连接包括旋转变压器换向无刷直流电动机的齿轮传动动力驱动器和组合件行星减速机提供主动力反馈，以及几个电气独立的RVDT位置传感器。齿轮架构使用行星齿轮箱上的固定笼式旋转内齿轮装置，其可以是单级或多级。齿轮箱的输出扭矩由旋转内齿圈的外壳上的特征提供，允许整个动力驱动器在更中心的位置轴向放置，减少齿轮箱输出保持架轴承上的力矩负载，以及促进使用连杆的万向节的紧凑的驱动装置。另外，公共的功率驱动可以用于滚动轴和俯仰轴。

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