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1. 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。

2. 发明授权

US08423207B2 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：US08423207B2
公开(公告)日：2013-04-16
申请号：US13218978
申请日：2011-08-26
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： G05D1/00 , G05D1/06 , G05D3/00 , G06F17/00
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。

3. 发明申请

US20080140270A1 INTEGRATED APPROACH NAVIGATION SYSTEM, METHOD, AND COMPUTER PROGRAM PRODUCT 有权
标题翻译：综合方法导航系统，方法和计算机程序产品
公开(公告)号：US20080140270A1
公开(公告)日：2008-06-12
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： G01C21/00 , G05D1/00
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。

4. 发明申请

US20110313600A1 INTEGRATED APPROACH NAVIGATION SYSTEM, METHOD, AND COMPUTER PROGRAM PRODUCT 有权
标题翻译：综合方法导航系统，方法和计算机程序产品
公开(公告)号：US20110313600A1
公开(公告)日：2011-12-22
申请号：US13218978
申请日：2011-08-26
申请人： Robert B. Davis , Daniel J. Boorman , Kirk L. 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 , Kirk L. 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： G01C23/00 , G05D1/00
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。

5. 发明授权

US09043050B2 Programmable reverse thrust detent system and method 有权
标题翻译：可编程反推力制动系统及方法
公开(公告)号：US09043050B2
公开(公告)日：2015-05-26
申请号：US12191197
申请日：2008-08-13
申请人： William L. Goodman , Thomas Imrich
发明人： William L. Goodman , Thomas Imrich
IPC分类号： G01C23/00 , F02K1/76 , B64D31/04 , G05D1/00
CPC分类号： F02K1/76 , B64D31/04 , G05D1/0083
摘要： A reverse thrust detent system for an aircraft includes a throttle quadrant having an intermediate reverse thrust detent position, a reverse thrust scheduling system interfacing with the throttle quadrant, at least one aircraft engine interfacing with the reverse thrust scheduling system and a programmable input interfacing with the reverse thrust scheduling system and adapted to receive an engine reverse thrust setting. The reverse thrust scheduling system is adapted to operate the at least one aircraft engine according to the engine reverse thrust setting responsive to actuation of the intermediate reverse thrust detent position of the throttle quadrant. A reverse thrust detent method for an aircraft is also disclosed.
摘要翻译：用于飞行器的反向推力制动系统包括具有中间反向止推位置的节气门象限，与节气门象限接口的反向推力调度系统，与反向推力调度系统接口的至少一个飞机发动机以及与该反向推力调节系统接口的可编程输入反向推力调度系统，适用于接收发动机反推力设定。反向推力调度系统适于根据发动机反向推力设置来操作至少一个飞行器发动机，其响应于节气门象限的中间反向止推位置的致动。还公开了一种用于飞机的反推力制动方法。

6. 发明申请

US20090292433A1 METHOD AND SYSTEM OF DETERMINING EFFECTIVENESS OF AN AIRCRAFT BRAKING SYSTEM ON AN AIRCRAFT DURING AN AIRCRAFT LANDING 有权
标题翻译：航空器飞机上航空器制动系统有效性的确定方法与系统
公开(公告)号：US20090292433A1
公开(公告)日：2009-11-26
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。

7. 发明申请

US20090267798A1 THE COMMUNICATION OF LANDING CONDITIONS 有权
标题翻译：登陆条件通信
公开(公告)号：US20090267798A1
公开(公告)日：2009-10-29
申请号：US11464642
申请日：2006-08-15
申请人： William L. Goodman , Syed T. Shafaat , Thomas Imrich
发明人： William L. Goodman , Syed T. Shafaat , Thomas Imrich
IPC分类号： G08B21/00 , B60T8/32
CPC分类号： G08G1/161 , G08G5/0008 , G08G5/0013 , G08G5/025
摘要： The invention discloses differing embodiments of methods, aircraft, and apparatus for communicating the braking conditions of a runway. In one embodiment, braking information may be determined from a first aircraft which has landed on the runway. The braking information may be communicated to air traffic control and/or a second aircraft. Communication of the braking information may take place utilizing an Automatic Dependent Surveillance Broadcast system (ADS-B) and/or other type of automatic networking system.
摘要翻译：本发明公开了用于传达跑道制动条件的方法，飞行器和装置的不同实施例。在一个实施例中，可以从已经降落在跑道上的第一飞机确定制动信息。制动信息可以被传送到空中交通管制和/或第二飞行器。制动信息的通信可以利用自动相关监视广播系统（ADS-B）和/或其他类型的自动联网系统进行。

8. 发明授权

US07586422B2 Determination of runway landing conditions 有权
标题翻译：确定跑道着陆条件
公开(公告)号：US07586422B2
公开(公告)日：2009-09-08
申请号：US11461880
申请日：2006-08-02
申请人： William L. Goodman , Thomas Imrich , Syed T. Shafaat
发明人： William L. Goodman , Thomas Imrich , Syed T. Shafaat
IPC分类号： G08B21/00
CPC分类号： B60T8/1703 , B60T8/172 , B64C25/426 , G08G5/0091 , G08G5/025
摘要： The invention discloses differing embodiments of methods, aircraft, and apparatus for determining the landing conditions of a runway. In one embodiment, braking data may be collected from an aircraft which has landed on the runway; a braking performance measurement of the aircraft may be calculated based on the braking data; and a normalized braking performance measurement may be determined based on the braking performance measurement. The invention may be utilized to predict the expected braking performance of various types of aircraft on the runway. The invention may provide landing performance information to a broad host of users, and/or may be used as a basis for the development of a new aviation standard for the reporting of runway braking action.
摘要翻译：本发明公开了用于确定跑道着陆条件的方法，飞行器和装置的不同实施例。在一个实施例中，可以从已经降落在跑道上的飞机收集制动数据; 可以基于制动数据来计算飞行器的制动性能测量; 并且可以基于制动性能测量来确定归一化的制动性能测量。本发明可以用于预测跑道上各种类型的飞机的预期制动性能。本发明可以向广泛的用户主体提供着陆性能信息，和/或可以用作开发用于报告跑道制动动作的新的航空标准的基础。

9. 发明授权

US5933224A Hand-held distance-measurement apparatus and system 失效
标题翻译：手持式测距仪和系统
公开(公告)号：US5933224A
公开(公告)日：1999-08-03
申请号：US706904
申请日：1996-09-03
申请人： Robin H. Hines , Patrick J. Murphy , Michael R. Glasscock , William L. Goodman , Anthony R. Korba , Steven E. Harris
发明人： Robin H. Hines , Patrick J. Murphy , Michael R. Glasscock , William L. Goodman , Anthony R. Korba , Steven E. Harris
IPC分类号： G01C3/06 , G01S7/48 , G01S7/486 , G01S17/10 , G02B5/124 , G02B7/32 , G01C3/08 , F41G1/32 , G02F1/03
CPC分类号： G01S17/105 , G01S7/4865 , G02B5/124 , G01S7/486
摘要： The present invention relates to a portable, hand-held distance-measurement apparatus utilizing a laser range finder. The distance-measurement apparatus executes a number of distance-measurement cycles. In each cycle, a capacitor begins charging at approximately the same time that a light pulse is generated. An analog-to-digital converter generates a digital representation of the capacitor voltage at approximately the same time that a reflected light pulse is received. The lowest and the highest digital values are discarded and the remaining digital values are averaged and scaled to produce a distance measurement. A reflective target may be used at a remote location to reflect the light beam back to the distance-measurement apparatus. The distance-measurement apparatus has several power saving features that facilitate convenient battery operation. The distance-measurement apparatus may also have a view finder.
摘要翻译：本发明涉及利用激光测距仪的便携式手持式距离测量装置。距离测量装置执行多个距离测量循环。在每个周期中，电容器在与产生光脉冲的大致相同的时间开始充电。模拟 - 数字转换器在接收到反射光脉冲的大致相同的时间产生电容器电压的数字表示。丢弃最低和最高的数字值，并对剩余的数字值进行平均和缩放以产生距离测量。可以在远程位置使用反射目标以将光束反射回距离测量装置。距离测量装置具有几个省电特征，便于电池操作。距离测量装置也可以具有取景器。

10. 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。

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