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1.发明授权公开(公告)号：US09959774B2
公开(公告)日：2018-05-01
申请号：US13764701
申请日：2013-02-11
Applicant: Honeywell International Inc.
Inventor： Jiri Vasek , Ratan Khatwa , James C. Kirk , Olukayode Olofinboba , Pavel Kolcarek , Tomas Svoboda , Matej Dusik
CPC classification number: G08G5/04 , G01S13/93 , G01S13/931 , G01S2013/9335 , G08G5/0021 , G08G5/0078 , G08G5/045 , G08G5/065
Abstract: Systems and methods for aiding in pilot awareness of obstacles relative to aircraft features. An exemplary processor receives sensor information from one or more sensors mounted in an aircraft feature (e.g. light modules), determines if at least one obstacle is located within a predefined field of view based on the received sensor or database information and generates an image. The image includes an ownship icon having at least one feature representing wingtips of the aircraft and at least one indicator associated with the determined at least one obstacle. A display device presents the generated image. The display device presents a tip of a first sense coverage area adjacent to one wingtip feature associated with the port wing and a tip of the second sense coverage area adjacent to one wingtip feature associated with the starboard wing. The indicator is presented within at least one of the coverage areas.
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公开(公告)号：US20160052641A1
公开(公告)日：2016-02-25
申请号：US14467275
申请日：2014-08-25
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Olukayode Olofinboba , Joseph Nutaro , David Pepitone , Patrick Jackson
IPC: B64D45/00
CPC classification number: B64D45/00 , B64C25/405 , B64D43/02 , G01C23/00 , G08G5/0008 , G08G5/0013 , G08G5/0021 , G08G5/0078 , G08G5/045 , G08G5/065 , Y02T50/823
Abstract: A method of displaying aircraft operating and position information with an electronic display unit comprises determining a position of a first aircraft at an airport; determining an optimum speed range of the first aircraft; determining a first aircraft speed of the first aircraft; displaying on a screen of the display unit a map of at least part of the airport; displaying a first aircraft symbol on the map, the first aircraft symbol displayed in a position on the map indicative of position of the first aircraft; and displaying an optimum speed range symbol having a lower bound end and a higher bound end in a position on the map such that the first aircraft symbol is between the lower bound end and the higher bound end when the first aircraft speed is within the optimum speed range.
Abstract translation: 用电子显示单元显示飞行器操作和位置信息的方法包括：确定机场处的第一飞机的位置; 确定所述第一飞行器的最佳速度范围; 确定第一架飞机的第一架飞机速度; 在显示单元的屏幕上显示至少部分机场的地图; 在地图上显示第一飞机符号，第一飞行器符号显示在地图上指示第一飞机位置的位置上; 以及在所述地图上的位置中显示具有下限结束端和上限端的最佳速度范围符号，使得当所述第一飞行器速度在所述最佳速度内时，所述第一飞行器符号位于所述下限端和所述较高限制端之间 范围。
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公开(公告)号：US09575174B2
公开(公告)日：2017-02-21
申请号：US13741291
申请日：2013-01-14
Applicant: Honeywell International Inc.
Inventor： Jiri Vasek , Pavel Kolcarek , Olukayode Olofinboba
CPC classification number: G01S13/93 , G01S7/04 , G01S7/51 , G01S13/04 , G01S13/931 , G01S17/933 , G01S2013/9335 , G08G5/0021 , G08G5/0078 , G08G5/045 , G08G5/065
Abstract: Systems and methods for providing improved situational awareness for an aircraft while taxiing. An exemplary method generates reflectivity data based on an associated emission at a transceiver located on an aircraft. At a processor, targets are determined if a portion of the generated reflectivity data is greater than a predefined threshold. Then, the analyzed targets are determined as to whether they are within a dynamically defined three-dimensional envelope. The envelope is based on wingtip light module speed and trajectory. On a display device, an indication of the nearest target is presented at the associated range to the nearest target.
Abstract translation: 系统和方法，用于在滑行时为飞机提供改善的情境意识。 示例性方法基于位于飞机上的收发器处的相关发射产生反射率数据。 在处理器中，确定所生成的反射率数据的一部分是否大于预定阈值的目标。 然后，确定分析的目标是否在动态定义的三维包络内。 信封是基于机翼灯模块的速度和轨迹。 在显示设备上，将最近的目标的指示呈现在与最近的目标相关联的范围上。
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公开(公告)号：US09457896B2
公开(公告)日：2016-10-04
申请号：US14163332
申请日：2014-01-24
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Robert E. De Mers , Olukayode Olofinboba , Keith Hughes , Joseph Ott
CPC classification number: B64C25/405 , B64D31/04 , Y02T50/823
Abstract: An electric taxi system (ETS) for an aircraft may include a ground speed sensor, a speed selection unit and a speed computer coupled to the ground speed sensor and to the speed selection unit. The speed computer may produce a speed error signal. A motor controller coupled to a wheel motor may control speed of the wheel motor responsively to the speed error signal.
Abstract translation: 用于飞机的电动出租车系统（ETS）可以包括地面速度传感器，速度选择单元和耦合到地面速度传感器和速度选择单元的速度计算机。 速度计算机可能产生速度误差信号。 耦合到车轮电动机的电动机控制器可以响应于速度误差信号来控制车轮电动机的速度。
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公开(公告)号：US20130321193A1
公开(公告)日：2013-12-05
申请号：US13741291
申请日：2013-01-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Jiri Vasek , Pavel Kolcarek , Olukayode Olofinboba
CPC classification number: G01S13/93 , G01S7/04 , G01S7/51 , G01S13/04 , G01S13/931 , G01S17/933 , G01S2013/9335 , G08G5/0021 , G08G5/0078 , G08G5/045 , G08G5/065
Abstract: Systems and methods for providing improved situational awareness for an aircraft while taxiing. An exemplary method generates reflectivity data based on an associated emission at a transceiver located on an aircraft. At a processor, targets are determined if a portion of the generated reflectivity data is greater than a predefined threshold. Then, the analyzed targets are determined as to whether they are within a dynamically defined three-dimensional envelope. The envelope is based on wingtip light module speed and trajectory. On a display device, an indication of the nearest target is presented at the associated range to the nearest target.
Abstract translation: 系统和方法，用于在滑行时为飞机提供改善的情境意识。 示例性方法基于位于飞机上的收发器处的相关发射产生反射率数据。 在处理器中，确定所生成的反射率数据的一部分是否大于预定阈值的目标。 然后，确定分析的目标是否在动态定义的三维包络内。 信封是基于机翼灯模块的速度和轨迹。 在显示设备上，将最近的目标的指示呈现在与最近的目标相关联的范围上。
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Patent Agency Ranking
公开(公告)号：US20150210383A1
公开(公告)日：2015-07-30
申请号：US14163332
申请日：2014-01-24
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Robert E. De Mers , Olukayode Olofinboba , Keith Hughes , Joseph Ott
CPC classification number: B64C25/405 , B64D31/04 , Y02T50/823
Abstract: An electric taxi system (ETS) for an aircraft may include a ground speed sensor, a speed selection unit and a speed computer coupled to the ground speed sensor and to the speed selection unit. The speed computer may produce a speed error signal. A motor controller coupled to a wheel motor may control speed of the wheel motor responsively to the speed error signal.
Abstract translation: 用于飞机的电动出租车系统（ETS）可以包括地面速度传感器，速度选择单元和耦合到地面速度传感器和速度选择单元的速度计算机。 速度计算机可能产生速度误差信号。 耦合到车轮电动机的电动机控制器可以响应于速度误差信号来控制车轮电动机的速度。
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公开(公告)号：US09121487B2
公开(公告)日：2015-09-01
申请号：US14079445
申请日：2013-11-13
Applicant: HONEYWELL INTERNATIONAL, INC.
Inventor： Robert E. De Mers , Olukayode Olofinboba , Keith Hughes , Joseph Ott , Alan Griesbach
CPC classification number: F16H59/02 , B64C13/04 , B64C25/405 , B64D31/04 , F16H61/0202 , G05G1/00 , Y02T50/823 , Y10T74/20085 , Y10T74/2011
Abstract: A pilot interface panel may comprise at least one input mechanism configured to receive at least one user input, generate at least one input signal corresponding to the at least one user input, and send the at least one input signal to a controller. The controller may be configured to control movement of an electric taxi system of an aircraft in a manner according to the at least one input signal, wherein the electric taxi system may be configured to rotate at least one wheel of the aircraft by force from a purely electromotive source. The pilot interface panel may further comprise at least one safety mechanism, which may be configured to prevent at least one of the at least one input mechanisms from receiving an inadvertent user input resulting from an unintended action by the user.
Abstract translation: 导频接口面板可以包括至少一个输入机构，其被配置为接收至少一个用户输入，产生对应于至少一个用户输入的至少一个输入信号，并将至少一个输入信号发送到控制器。 控制器可以被配置成以根据至少一个输入信号的方式控制飞行器的电动滑行系统的移动，其中电动滑行系统可以被配置成通过强制从一个纯粹的方式旋转飞行器的至少一个车轮 电动源。 导频接口面板还可以包括至少一个安全机构，其可以被配置为防止至少一个输入机构中的至少一个输入机构接收由用户的非预期动作导致的无意的用户输入。
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8.发明申请SYSTEMS AND METHODS FOR DISPLAYING AIRCRAFT BRAKING DISTANCE DURING SURFACE OPERATIONS 有权用于在表面操作期间显示飞机制动距离的系统和方法公开(公告)号：US20130325245A1
公开(公告)日：2013-12-05
申请号：US13804294
申请日：2013-03-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Pavel Kolcarek , Jiri Vasek , Tomas Svoboda , Olukayode Olofinboba
IPC: G06F17/00
CPC classification number: G06F17/00 , B64C25/42 , B64C25/426 , B64D43/00 , B64D45/00 , G01S2013/9335 , G08G5/0021 , G08G5/065
Abstract: Systems and methods are operable to present braking distance information to crew of an installation aircraft. An exemplary embodiment determines a braking distance for a braking maneuver of the installation aircraft, wherein the braking distance is based on a current ground speed of the aircraft; and generates a graphical representation that is presented on a display, wherein a location of a graphical icon on the graphical representation indicates the determined braking distance from the installation aircraft.
Abstract translation: 系统和方法可操作以向安装飞机的乘务员呈现制动距离信息。 一个示例性实施例确定了用于安装飞机的制动操纵的制动距离，其中制动距离基于飞行器的当前地面速度; 并且生成呈现在显示器上的图形表示，其中图形表示上的图形图标的位置指示从所述安装飞机确定的制动距离。
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9.发明申请SYSTEMS AND METHODS FOR DISPLAYING OBSTACLE-AVOIDANCE INFORMATION DURING SURFACE OPERATIONS 有权用于在表面操作期间显示异常避风信息的系统和方法公开(公告)号：US20130321176A1
公开(公告)日：2013-12-05
申请号：US13764701
申请日：2013-02-11
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Jiri Vasek , Ratan Khatwa , James C. Kirk , Olukayode Olofinboba , Pavel Kolcarek , Tomas Svoboda , Matej Dusik
IPC: G08G5/04
CPC classification number: G08G5/04 , G01S13/93 , G01S13/931 , G01S2013/9335 , G08G5/0021 , G08G5/0078 , G08G5/045 , G08G5/065
Abstract: Systems and methods for aiding in pilot awareness of obstacles relative to aircraft features. An exemplary processor receives sensor information from one or more sensors mounted in an aircraft feature (e.g. light modules), determines if at least one obstacle is located within a predefined field of view based on the received sensor or database information and generates an image. The image includes an ownship icon having at least one feature representing wingtips of the aircraft and at least one indicator associated with the determined at least one obstacle. A display device presents the generated image. The display device presents a tip of a first sense coverage area adjacent to one wingtip feature associated with the port wing and a tip of the second sense coverage area adjacent to one wingtip feature associated with the starboard wing. The indicator is presented within at least one of the coverage areas.
Abstract translation: 帮助驾驶员了解相对于飞机特征的障碍的系统和方法。 示例性处理器从安装在飞行器特征（例如，光模块）中的一个或多个传感器接收传感器信息，基于接收到的传感器或数据库信息确定至少一个障碍物是否位于预定视场内，并产生图像。 图像包括具有至少一个表示飞机的翼尖的特征的自身图标以及与所确定的至少一个障碍物相关联的至少一个指示符。 显示装置呈现生成的图像。 所述显示装置呈现与所述端口翼相关联的一个翼尖特征附近的第一感测覆盖区域的尖端和与所述右舷翼相关联的一个翼尖特征相邻的所述第二感测覆盖区域的尖端。 该指示符被呈现在至少一个覆盖区域内。
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公开(公告)号：US09296490B2
公开(公告)日：2016-03-29
申请号：US14467275
申请日：2014-08-25
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Olukayode Olofinboba , Joseph Nutaro , David Pepitone , Patrick Jackson
CPC classification number: B64D45/00 , B64C25/405 , B64D43/02 , G01C23/00 , G08G5/0008 , G08G5/0013 , G08G5/0021 , G08G5/0078 , G08G5/045 , G08G5/065 , Y02T50/823
Abstract: A method of displaying aircraft operating and position information with an electronic display unit comprises determining a position of a first aircraft at an airport; determining an optimum speed range of the first aircraft; determining a first aircraft speed of the first aircraft; displaying on a screen of the display unit a map of at least part of the airport; displaying a first aircraft symbol on the map, the first aircraft symbol displayed in a position on the map indicative of position of the first aircraft; and displaying an optimum speed range symbol having a lower bound end and a higher bound end in a position on the map such that the first aircraft symbol is between the lower bound end and the higher bound end when the first aircraft speed is within the optimum speed range.
Abstract translation: 用电子显示单元显示飞行器操作和位置信息的方法包括：确定机场处的第一飞机的位置; 确定所述第一飞行器的最佳速度范围; 确定第一架飞机的第一架飞机速度; 在显示单元的屏幕上显示至少部分机场的地图; 在地图上显示第一飞机符号，第一飞行器符号显示在地图上指示第一飞机位置的位置上; 以及在所述地图上的位置中显示具有下限结束端和上限端的最佳速度范围符号，使得当所述第一飞行器速度在所述最佳速度内时，所述第一飞行器符号位于所述下限端和所述较高限制端之间 范围。
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