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1.发明申请Method, system, and computer program product for performance monitored aircraft rejected takeoff braking 有权方法，系统和计算机程序产品，用于性能监控飞机拒绝起飞制动公开(公告)号：US20080154445A1
公开(公告)日：2008-06-26
申请号：US11642126
申请日：2006-12-20
IPC分类号： B60T8/17
CPC分类号： B60T8/1703 , B64C25/426
摘要： In exemplary embodiments, braking of an airplane is controlled during a rejected takeoff. A rejected takeoff of an airplane from a runway is initiated. Position of the airplane is determined, such as by inputting aircraft position from a global positioning system. Distance remaining on the runway is determined. Deceleration to stop the aircraft in the determined distance remaining on the runway is calculated, and the calculated deceleration is provided to an autobraking system of the airplane. When the aircraft can not be stopped in the determined distance remaining on the runway, a predetermined deceleration that correlates to maximum braking may be provided to the aircraft's autobraking system. The calculated deceleration may be provided to the autobraking system until a pilot takes command of the aircraft's brakes or the aircraft has stopped.
摘要翻译： 在示例性实施例中，在被拒绝的起飞期间控制飞机的制动。 启动飞机从跑道起飞的起飞。 确定飞机的位置，例如通过从全球定位系统输入飞机位置。 确定跑道上剩余的距离。 计算停止在跑道上残留的确定距离中的飞行器的减速，并且将计算出的减速度提供给飞机的自动制动系统。 当飞机不能以确定的距离停在跑道上时，可以向飞机的自动制动系统提供与最大制动相关的预定减速度。 计算出的减速度可以提供给自动制动系统，直到驾驶员对飞行器的制动器进行命令或飞行器停止。
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公开(公告)号：US07626513B2
公开(公告)日：2009-12-01
申请号：US11464642
申请日：2006-08-15
IPC分类号： G08B21/00
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。
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3.发明授权Method and system of determining effectiveness of an aircraft braking system on an aircraft during an aircraft landing 有权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。
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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
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。
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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
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。
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6.发明授权Method, system, and computer program product for performance monitored aircraft rejected takeoff braking 有权方法，系统和计算机程序产品，用于性能监控飞机拒绝起飞制动公开(公告)号：US07720579B2
公开(公告)日：2010-05-18
申请号：US11642126
申请日：2006-12-20
CPC分类号： B60T8/1703 , B64C25/426
摘要： In exemplary embodiments, braking of an airplane is controlled during a rejected takeoff. A rejected takeoff of an airplane from a runway is initiated. Position of the airplane is determined, such as by inputting aircraft position from a global positioning system. Distance remaining on the runway is determined. Deceleration to stop the aircraft in the determined distance remaining on the runway is calculated, and the calculated deceleration is provided to an autobraking system of the airplane. When the aircraft can not be stopped in the determined distance remaining on the runway, a predetermined deceleration that correlates to maximum braking may be provided to the aircraft's autobraking system. The calculated deceleration may be provided to the autobraking system until a pilot takes command of the aircraft's brakes or the aircraft has stopped.
摘要翻译： 在示例性实施例中，在被拒绝的起飞期间控制飞机的制动。 启动飞机从跑道起飞的起飞。 确定飞机的位置，例如通过从全球定位系统输入飞机位置。 确定跑道上剩余的距离。 计算停止在跑道上残留的确定距离中的飞行器的减速，并且将计算出的减速度提供给飞机的自动制动系统。 当飞机不能以确定的距离停在跑道上时，可以向飞机的自动制动系统提供与最大制动相关的预定减速度。 计算出的减速度可以提供给自动制动系统，直到驾驶员对飞行器的制动器进行命令或飞行器停止。
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公开(公告)号：US20100042267A1
公开(公告)日：2010-02-18
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
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。
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公开(公告)号：US20080030073A1
公开(公告)日：2008-02-07
申请号：US11461880
申请日：2006-08-02
IPC分类号： B60T8/32
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。
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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
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。
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10.发明申请公开(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。
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