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1. 发明授权

US08417396B2 Air traffic control method 有权
标题翻译：空中交通管制办法
公开(公告)号：US08417396B2
公开(公告)日：2013-04-09
申请号：US13241189
申请日：2011-09-22
申请人： William L. Goodman , Syed T. Shafaat , John A. Brown , Jennifer L. Gertley , Robert P. Smith
发明人： William L. Goodman , Syed T. Shafaat , John A. Brown , Jennifer L. Gertley , Robert P. Smith
IPC分类号： G01C23/00
CPC分类号： G08G5/0013
摘要： A method of operating an air traffic control system may include receiving, by a control system, an instruction from a control system user. The method may further include providing, by the control system, the instruction to an airplane via a data link between the control system and a system of the airplane. In addition, the method may include adjusting, by the airplane system, at least one airplane control to correspond to the instruction.
摘要翻译：操作空中交通管制系统的方法可包括由控制系统接收来自控制系统用户的指令。该方法还可以包括通过控制系统和飞机的系统之间的数据链路向控制系统提供对飞机的指令。另外，该方法可以包括由飞机系统调整至少一个对应于指令的飞机控制。

2. 发明授权

US08060261B2 Method and system of determining effectiveness of an aircraft braking system on an aircraft during an aircraft landing 有权
标题翻译：在飞机着陆期间确定飞机制动系统在飞机上的有效性的方法和系统
公开(公告)号：US08060261B2
公开(公告)日：2011-11-15
申请号：US12124519
申请日：2008-05-21
申请人： William L. Goodman , Thomas Imrich
发明人： William L. Goodman , Thomas Imrich
IPC分类号： G06F19/00
CPC分类号： B64C25/42 , B60T8/1703 , G08G5/0013 , G08G5/0021 , G08G5/0091 , G08G5/025
摘要： A method of determining effectiveness of an aircraft braking system on an aircraft during an aircraft landing including generating a scalar deceleration value when a predefined braking event occurs that corresponds to effectiveness of a braking system associated with an aircraft landing operation during occurrence of a predefined braking event on an aircraft; and disseminating the generated scalar deceleration value to downstream users. A system includes a data collection module adapted to collect data relating to braking data associated with each of an associated plurality of segments of deceleration of the aircraft during a predefined braking event; a calculation module adapted to generate a scalar deceleration value based on data obtained; and a communication module in signal communication with the calculation module and with at least one downstream user of the system adapted to communicate the scalar deceleration value to at least one downstream user.
摘要翻译：一种在飞机着陆期间确定飞行器制动系统在飞行器上的有效性的方法，包括当发生预定义的制动事件时产生与标准飞机着陆操作相关联的制动系统的有效性的预定制动事件的生成时的标量减速度值的方法在飞机上并向下游用户传播产生的标量减速度值。一种系统包括数据采集模块，适于在预定制动事件期间收集与飞机相关联的多个段减速相关的制动数据相关的数据; 计算模块，适于基于获得的数据生成标量减法值; 以及通信模块，其与所述计算模块进行信号通信，以及所述系统的至少一个下游用户适于将所述标量减速度值传递给至少一个下游用户。

3. 发明授权

US07818100B2 System and method for optimized runway exiting 有权
标题翻译：优化跑道退出的系统和方法
公开(公告)号：US07818100B2
公开(公告)日：2010-10-19
申请号：US11777351
申请日：2007-07-13
申请人： William L. Goodman , Thomas Imrich
发明人： William L. Goodman , Thomas Imrich
IPC分类号： B64C13/16 , G05D1/00 , G05D13/00
CPC分类号： G05D1/0083 , B64C25/426
摘要： Methods and apparatus are provided for optimizing runway exiting. Prior to landing, the pilot may choose to input one or more new landing parameters. Then, based on current landing parameters (e.g., any new landing parameter(s) and remaining default landing parameters) and the aircraft performance parameters, predicted landing performance can be updated and indicia of the updated predicted landing performance can be displayed to the pilot on an updated airport map and display. The updated predicted landing performance can include, among other things, a display of AUTOBRAKE landing performance. When no further changes to the current landing parameters are desired, the automatic braking system can be set to provide dynamic braking to slow the aircraft to a selected velocity at a selected position on a particular runway.
摘要翻译：提供了优化跑道出口的方法和装置。在着陆之前，飞行员可以选择输入一个或多个新的着陆参数。然后，根据当前着陆参数（例如，任何新的着陆参数和剩余的默认着陆参数）和飞机性能参数，可以更新预测的着陆性能，并且可以向飞行员显示更新的预测着陆性能的标记更新的机场地图和展示。更新的预测着陆性能可以包括AUTOBRAKE着陆性能的显示。当不需要进一步改变当前着陆参数时，可以将自动制动系统设置成提供动态制动，以使飞机在特定跑道上的选定位置处以选定的速度减速。

4. 发明申请

US20080249675A1 SYSTEM AND METHOD FOR OPTIMIZED RUNWAY EXITING 有权
标题翻译：优化跑道出口系统与方法
公开(公告)号：US20080249675A1
公开(公告)日：2008-10-09
申请号：US11777351
申请日：2007-07-13
申请人： William L. Goodman , Thomas Imrich
发明人： William L. Goodman , Thomas Imrich
IPC分类号： B64C13/16 , G05D1/00 , G05D13/00
CPC分类号： G05D1/0083 , B64C25/426
摘要： Methods and apparatus are provided for optimizing runway exiting. Prior to landing, the pilot may choose to input one or more new landing parameters. Then, based on current landing parameters (e.g., any new landing parameter(s) and remaining default landing parameters) and the aircraft performance parameters, predicted landing performance can be updated and indicia of the updated predicted landing performance can be displayed to the pilot on an updated airport map and display. The updated predicted landing performance can include, among other things, a display of AUTOBRAKE landing performance. When no further changes to the current landing parameters are desired, the automatic braking system can be set to provide dynamic braking to slow the aircraft to a selected velocity at a selected position on a particular runway.
摘要翻译：提供了优化跑道出口的方法和装置。在着陆之前，飞行员可以选择输入一个或多个新的着陆参数。然后，根据当前着陆参数（例如，任何新的着陆参数和剩余的默认着陆参数）和飞机性能参数，可以更新预测的着陆性能，并且可以向飞行员显示更新的预测着陆性能的标记更新的机场地图和展示。更新的预测着陆性能可以包括AUTOBRAKE着陆性能的显示。当不需要进一步改变当前着陆参数时，可以将自动制动系统设置成提供动态制动，以使飞机在特定跑道上的选定位置处以选定的速度减速。

5. 发明授权

US06586937B2 Magnetic signature detector for detection of magnetic buried targets 有权
标题翻译：用于检测磁埋置靶的磁性签名检测器
公开(公告)号：US06586937B2
公开(公告)日：2003-07-01
申请号：US09945550
申请日：2001-08-30
申请人： William L. Goodman
发明人： William L. Goodman
IPC分类号： G01V308
CPC分类号： G01V3/15
摘要： An apparatus for measuring and detecting a magnetic signature of a magnetically detectable object from a distance includes a portable sensor group for detecting the magnetic signature. The portable sensor group includes three gradient sensors, each of the three gradient sensors adapted to independently measure both a magnitude and a direction of the magnetic signature, a first of said gradient sensors measuring an axial gradient in the vertical direction, a second of said gradient sensors measuring a first horizontal gradient in the vertical direction, and a third of said gradient sensors measuring a second horizontal gradient in the vertical direction.
摘要翻译：用于从远距离测量和检测可磁性检测物体的磁性签名的装置包括用于检测磁性签名的便携式传感器组。便携式传感器组包括三个梯度传感器，三个梯度传感器中的每一个适于独立地测量磁性特征的大小和方向，所述梯度传感器中的第一个测量垂直方向的轴向梯度，所述梯度的第二梯度传感器测量垂直方向上的第一水平梯度的传感器，以及测量垂直方向上的第二水平梯度的所述梯度传感器中的三分之一。

6. 发明授权

US06556054B1 Efficient transmitters for phase modulated signals 失效
标题翻译：用于相位调制信号的高效发射器
公开(公告)号：US06556054B1
公开(公告)日：2003-04-29
申请号：US09677282
申请日：2000-10-02
申请人： William L. Goodman , Mark Sweeny
发明人： William L. Goodman , Mark Sweeny
IPC分类号： H03K300
CPC分类号： H03J5/246 , E21B47/121 , H01Q1/04 , H01Q7/00 , H03C3/00
摘要： A circuit for driving a current into an inductor, which circuit includes at least one main capacitor, a power supply operably connected to the main capacitor, the inductor, and at least two pairs of switches connecting the main capacitor to the inductor, whereby the connection of the main capacitor to the inductor is made in either polarity. Current is driven into the inductor by applying a current to the main capacitor, applying a voltage to the inductor from the main capacitor resulting in generation of inductive energy, and recapturing the inductive energy with the main capacitor at the end of a cycle.
摘要翻译：一种用于将电流驱动到电感器中的电路，该电路包括至少一个主电容器，可操作地连接到主电容器的电源，电感器以及将主电容器连接到电感器的至少两对开关，由此连接电感器的主电容器以任一极性制成。通过向主电容器施加电流将电流驱动到电感器中，从主电容器向电感器施加电压，从而产生感应能量，并且在一个周期结束时重新捕获与主电容器的感应能量。

7. 再颁专利

USRE34701E Magnetically detectable plastic pipe 失效
标题翻译：磁性可检测塑料管
公开(公告)号：USRE34701E
公开(公告)日：1994-08-23
申请号：US29373
申请日：1993-03-08
申请人： William L. Goodman
发明人： William L. Goodman
IPC分类号： B29C47/04 , B32B37/00 , F16L1/11 , F16L9/12 , G01V15/00 , G02B6/44 , G06K19/06 , B32B31/04
CPC分类号： F16L9/12 , B29C47/0019 , B29C47/0023 , B29C47/062 , F16L1/11 , F16L9/125 , G01V15/00 , G02B6/447 , G06K19/06187 , B29K2023/06 , B29K2027/06 , B29K2105/16 , B29K2995/0008 , B29L2023/22
摘要： A magnetically detectable plastic, e.g., polyethylene, polyvinyl, etc., pipe for underground use comprises a hollow tubular plastic pipe having particles of magnetic material embedded in plastic and secured integrally with the wall of the pipe. The magnetic particles are of iron oxide or barium ferrite and of a size, shape, distribution and proportion such that the plastic pipe may be easily detected by magnetic detection apparatus on the surface when the plastic pipe is buried at a selected depth under the ground. The magnetic particles are uniformly distributed throughout the thickness and uniformly distributed around the entire circumference of the plastic pipe or the magnetic particles may be distributed in discrete portions of the plastic pipe, as for example, a uniform outer layer of the pipe or in stripes or strips extending along the pipe. The particles may be extruded with the plastic in forming the pipe, whether uniformly dispersed or in discrete regions or the pipe may be formed of plastic free of the magnetic particles and the magnetic particles provided in a separately applied strip which may be coextruded or fused or adhered to the wall of the pipe. The magnetic strips or magnetic portions of the plastic pipe may have selective areas or portions magnetized to encode information readable from the surface of the ground above the buried pipe or in inventorying pipe on the surface.

8. 再颁专利

USRE46480E1 Tilt-compensated laser rangefinder 有权
公开(公告)号：USRE46480E1
公开(公告)日：2017-07-18
申请号：US11729913
申请日：2007-03-29
申请人： Robin H. Hines , Patrick J. Murphy , William L. Goodman , Matthew A. Johnson , Robin H. Hines
发明人： Robin H. Hines , Patrick J. Murphy , William L. Goodman , Matthew A. Johnson
IPC分类号： G01B11/26 , G01C3/08 , F41G1/467 , F41G3/08 , G01S17/10 , G01S7/48
CPC分类号： G01S17/023 , F41G3/06 , F41G3/08 , G01S7/4808 , G01S7/4868 , G01S7/497 , G01S17/10
摘要： The present invention is a laser ranging device that incorporates an internal tilt sensor, an internal temperature sensor, and an internal pressure sensor. The tilt sensor is used to measure the target's vertical angle relative to the horizontal reference plane. Digital signal processing circuitry controls the firing of the laser pulse, calculation of time-of-flight range, measurement of the vertical angle of the tilt sensor, measurement of ambient temperature and storage of tilt sensor and temperature sensor calibration data. The digital signal processing circuitry then provides the user temperature corrected ballistic ranging information, including corrected horizontal range. Additionally, an automatic gain control system minimizes the effects of target to target variance in reflectivity and its associated errors. It is also an object of this invention to electronically minimize errors in the measurement of a vertical angle caused by housing vibration and by temperature variance errors.

9. 发明授权

US08027756B2 Integrated approach navigation system, method, and computer program product 有权
标题翻译：综合导航系统，方法和计算机程序产品
公开(公告)号：US08027756B2
公开(公告)日：2011-09-27
申请号：US11608064
申请日：2006-12-07
申请人： Robert B. Davis , Daniel J. Boorman , L. Kirk Gagnon , William L. Goodman , Alan R. Jacobsen , William A. Miller , James E. Mitchell , Victor A. Riley , William F. Royce , William D. Tafs
发明人： Robert B. Davis , Daniel J. Boorman , L. Kirk Gagnon , William L. Goodman , Alan R. Jacobsen , William A. Miller , James E. Mitchell , Victor A. Riley , William F. Royce , William D. Tafs
IPC分类号： G05D1/06
CPC分类号： G01C23/00 , G01C21/00 , G01C23/005 , G08G5/0021 , G08G5/025
摘要： Systems, computer program products, and methods for displaying navigation performance based flight path deviation information during the final approach segment to a runway and during landing of non-precision flight modes are provided. Improved graphical depictions of navigation performance based flight path deviation information provide pilots and flight crew members with clear, concise displays of the dynamic relationship between ANP and RNP, mode and aspect of flight and related procedures, intersecting flight paths, and current actual flight path deviation from a predefined flight path during the final approach segment to a runway and during landing. For example, an enhanced IAN display may include NPS-type deviation scales to show RNP/ANP relationships and predetermined RNP markers to alert the pilots and flight crew members that the FMC has transitioned from an NPS display for RNAV (LNAV/VNAV) flight procedures to an enhanced IAN display for a non-precision (non-xLS) approach and/or landing.
摘要翻译：提供了系统，计算机程序产品以及在最终进场段到跑道和非精确飞行模式着陆期间显示导航性能的飞行路径偏差信息的方法。基于导航性能的飞行路径偏差信息的改进图形描述为飞行员和飞行机组成员提供了ANP和RNP之间的动态关系，飞行模式和方面以及相关程序，相交飞行路径以及当前实际飞行路径偏差的清晰简明的显示在最终进场段期间从预定义的飞行路径到跑道和着陆期间。例如，增强的IAN显示器可以包括NPS型偏差标度以显示RNP / ANP关系和预定的RNP标记，以警告飞行员和飞行机组成员FMC已经从用于RNAV（LNAV / VNAV）飞行程序的NPS显示器转换到非精确（非xLS）方法和/或着陆的增强型IAN显示。

10. 发明申请

US20110046869A1 PROGRAMMING AIRPLANE SYSTEMS BASED ON INSTRUCTIONS 有权
标题翻译：基于指令编程飞机系统
公开(公告)号：US20110046869A1
公开(公告)日：2011-02-24
申请号：US12917424
申请日：2010-11-01
申请人： William L. Goodman , Syed T. Shafaat , John A. Brown , Jennifer L. Gertley , Robert P. Smith
发明人： William L. Goodman , Syed T. Shafaat , John A. Brown , Jennifer L. Gertley , Robert P. Smith
IPC分类号： G08G5/00
CPC分类号： G08G5/0013
摘要： A method of receiving an instruction by an airplane from a control system includes facilitating, by the airplane, a user of a system of the airplane in accepting or rejecting the instruction. The instruction may be received by the airplane via a data link between the control system and the airplane system. If the instruction is accepted, the method may further include loading, by the airplane, the instruction into the airplane system and/or adjusting, by the airplane, at least one airplane control to correspond to the instruction.
摘要翻译：由飞机从控制系统接收指令的方法包括由飞机帮助飞机系统的用户接受或拒绝该指示。该指令可以由飞机经由控制系统和飞机系统之间的数据链接接收。如果该指令被接受，该方法还可以包括由飞机将指令加载到飞机系统中和/或由飞机调整至少一个对应于该指令的飞机控制。

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