公开(公告)号：US09592921B2

公开(公告)日：2017-03-14

申请号：US13794089

申请日：2013-03-11

Applicant: Honeywell International Inc.

Inventor： Maria John Paul Dominic ,  Thomas D. Judd ,  Rakesh Kumar ,  Gurunadha Reddy Mallela ,  John Azariah Rajadurai ,  Saurabh Harshadbhai Gohil ,  David Pepitone

IPC: G08B21/00 ,  B64F1/18 ,  G08G5/00 ,  G08B23/00 ,  G01C21/00 ,  B64D45/00 ,  G01C23/00

CPC classification number: B64D45/00 ,  G01C23/00 ,  G08G5/0013 ,  G08G5/0021

Abstract: A graphical in-flight message representation system comprises a sensor configured to measure a characteristic of a flight of an aircraft and a communication device configured to send and receive in-flight messages. An in-flight message is a message communicated during the flight of the aircraft. The system also comprises a display unit configured to display a graphical flight progress indicator and one or more message icons, each of the one or more message icons corresponding to a respective in-flight message. The graphical flight progress indicator is representative of the characteristic of the flight measured by the sensor. Each of the one or more message icons are displayed in location relative to the graphical flight progress indicator based on the measured characteristic of the flight when the respective in-flight message was communicated.

Abstract translation: 图形飞行中消息表示系统包括被配置为测量飞行器的飞行特性的传感器和被配置为发送和接收飞行中消息的通信设备。 飞行中的消息是在飞机飞行期间传达的消息。 该系统还包括显示单元，其被配置为显示图形飞行进度指示符和一个或多个消息图标，所述一个或多个消息图标中的每一个对应于相应的飞行中消息。 图形飞行进度指示器代表传感器测量的飞行特性。 当相关的飞行中消息被传达时，基于所测量的飞行特性，一个或多个消息图标中的每一个显示在相对于图形飞行进度指示器的位置。

公开(公告)号：US09280903B2

公开(公告)日：2016-03-08

申请号：US14156164

申请日：2014-01-15

Applicant: Honeywell International Inc.

Inventor： Victoria Judy ,  David Pepitone

IPC: G01C23/00 ,  G08G5/00

CPC classification number: G08G5/003 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0039

Abstract: In one embodiment an in-aircraft system that implements a flight planning module is provided. The flight planning module is configured to display on the display unit a pending flight plan and implement a first button associated with a display of the pending flight plan. The first button, if selected, directs the one or more processing units to convert the pending flight plan to a format for sending in a datalink message, and to cause the pending flight plan to be sent to a ground station in a downlink datalink message without human input to a message applications module, the message applications module including instructions to display information corresponding to datalink messages on a display unit and to maintain a message log of datalink messages.

Abstract translation: 在一个实施例中，提供了实现飞行计划模块的飞机内系统。 飞行计划模块被配置为在显示单元上显示待定飞行计划，并且实现与待决飞行计划的显示相关联的第一按钮。 第一个按钮（如果选择）指示一个或多个处理单元将待定飞行计划转换为用于在数据链路消息中发送的格式，并且使未完成的飞行计划在下行链路数据链路消息中发送到地面站，而没有 消息应用模块包括用于显示对应于显示单元上的数据链路消息的信息并维护数据链路消息的消息日志的指令。

公开(公告)号：US20160161283A1

公开(公告)日：2016-06-09

申请号：US14559755

申请日：2014-12-03

Applicant: Honeywell International Inc.

Inventor： Raghu Shamasundar ,  Prasadrao Rao Piradi ,  Thomas D. Judd ,  David Pepitone ,  Abhishek Gupta ,  Adib Bouanani ,  Prashanth Ramanna

IPC: G01C23/00 ,  G06F3/0484 ,  H04L29/08 ,  G06F3/0481

CPC classification number: G01C23/005 ,  G06F3/0481

Abstract: Systems and methods for displaying position sensitive datalink messages on avionics displays are provided. In one embodiment, a flight deck instrument display system for an aircraft comprises: a flight plan display screen that displays a graphical representation of at least a part of an aircraft's planned flight path together with symbology representing a position of the aircraft with respect to the aircraft's planned flight path; wherein the flight plan display screen further displays at least one symbol positioned along the graphical representation of at least a part of the aircraft's planned flight path that indicates a point of applicability for a received uplink datalink message.

Abstract translation: 提供了在航空电子显示屏上显示位置敏感数据链路消息的系统和方法。 在一个实施例中，用于飞行器的飞行甲板仪表显示系统包括：飞行计划显示屏幕，其显示飞行器的计划飞行路径的至少一部分的图形表示，以及表示飞行器相对于飞机的飞行器的位置的符号 计划飞行路线; 其中所述飞行计划显示屏幕还显示沿着所述飞行器的计划飞行路径的至少一部分的图形表示定位的至少一个符号，其指示所接收的上行链路数据链路消息的适用点。

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

IPC: G01C21/00 ,  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。

公开(公告)号：US20140253585A1

公开(公告)日：2014-09-11

申请号：US13794089

申请日：2013-03-11

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Maria John Paul Dominic ,  Thomas D. Judd ,  Rakesh Kumar ,  Gurunadha Reddy Mallela ,  John Azariah Rajadurai ,  Saurabh Harshadbhai Gohil ,  David Pepitone

IPC: B64D45/00

CPC classification number: B64D45/00 ,  G01C23/00 ,  G08G5/0013 ,  G08G5/0021

Abstract: A graphical in-flight message representation system comprises a sensor configured to measure a characteristic of a flight of an aircraft and a communication device configured to send and receive in-flight messages. An in-flight message is a message communicated during the flight of the aircraft. The system also comprises a display unit configured to display a graphical flight progress indicator and one or more message icons, each of the one or more message icons corresponding to a respective in-flight message. The graphical flight progress indicator is representative of the characteristic of the flight measured by the sensor. Each of the one or more message icons are displayed in location relative to the graphical flight progress indicator based on the measured characteristic of the flight when the respective in-flight message was communicated.

Abstract translation: 图形飞行中消息表示系统包括被配置为测量飞行器的飞行特性的传感器和被配置为发送和接收飞行中消息的通信设备。 飞行中的消息是在飞机飞行期间传达的消息。 该系统还包括显示单元，其被配置为显示图形飞行进度指示符和一个或多个消息图标，所述一个或多个消息图标中的每一个对应于相应的飞行中消息。 图形飞行进度指示器代表传感器测量的飞行特性。 当相关的飞行中消息被传达时，基于所测量的飞行特性，一个或多个消息图标中的每一个显示在相对于图形飞行进度指示器的位置。

公开(公告)号：US09881504B2

公开(公告)日：2018-01-30

申请号：US14334568

申请日：2014-07-17

Applicant: Honeywell International Inc.

Inventor： Maria John Paul Dominic ,  Leonard Pereira ,  Siva Kommuri ,  Anil Kumar Pendyala ,  Rakesh Kumar ,  Xiaozhong He ,  Thomas D. Judd ,  David Pepitone

IPC: G06G5/00 ,  G08G5/00

CPC classification number: G08G5/0013 ,  G08G5/0021 ,  G08G5/0052

Abstract: In one embodiment, an aerospace system is provided. The aerospace system comprises at least one display unit configured to display flight data and a memory configured to store one or more flight plan associations. Each flight plan association is an association between a data link message and a respective waypoint in a flight plan. The aerospace system also comprises a processing unit configured to determine when each respective waypoint in the flight plan is reached based on a comparison of current location data to the flight plan. When each respective waypoint is reached, the processing unit is configured to identify any data link messages associated with the respective waypoint based on the flight plan associations and to direct the at least one display unit to display a respective notification for each identified data link message associated with the respective waypoint.

公开(公告)号：US20150199906A1

公开(公告)日：2015-07-16

申请号：US14156164

申请日：2014-01-15

Applicant: Honeywell International Inc.

Inventor： Victoria Judy ,  David Pepitone

IPC: G08G5/00

CPC classification number: G08G5/003 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0039

Abstract: In one embodiment an in-aircraft system that implements a flight planning module is provided. The flight planning module is configured to display on the display unit a pending flight plan and implement a first button associated with a display of the pending flight plan. The first button, if selected, directs the one or more processing units to convert the pending flight plan to a format for sending in a datalink message, and to cause the pending flight plan to be sent to a ground station in a downlink datalink message without human input to a message applications module, the message applications module including instructions to display information corresponding to datalink messages on a display unit and to maintain a message log of datalink messages.

Abstract translation: 在一个实施例中，提供了实现飞行计划模块的飞机内系统。 飞行计划模块被配置为在显示单元上显示待定飞行计划，并且实现与待决飞行计划的显示相关联的第一按钮。 第一个按钮（如果选择）指示一个或多个处理单元将待定飞行计划转换为用于在数据链路消息中发送的格式，并且使未完成的飞行计划在下行链路数据链路消息中发送到地面站，而没有 消息应用模块包括用于显示对应于显示单元上的数据链路消息的信息并维护数据链路消息的消息日志的指令。

公开(公告)号：US20140118188A1

公开(公告)日：2014-05-01

申请号：US14151281

申请日：2014-01-09

Applicant: Honeywell International Inc.

Inventor： Ratan Khatwa ,  David Pepitone

IPC: G01S7/20 ,  G01S13/95

CPC classification number: G01S7/20 ,  G01C23/00 ,  G01S13/9303 ,  G01S13/953 ,  G08G5/0021 ,  G08G5/0091 ,  Y02A90/18

Abstract: Systems and methods for improving situational awareness on an in-trails procedures display. A radar system transmits a radar signal and receives and stores weather radar reflectivity values into a three-dimensional buffer. A processor determines whether any of the stored weather reflectivity values indicate the presence of a weather hazard and generates one or more weather hazard icons based on the stored weather reflectivity values. An in-trail procedures display device displays the generated weather hazard icons. Wake vortex information for other aircraft is generated and outputted on the in-trail procedures display. Also, the processor receives a request for an altitude change and generates an alert when the aircraft is determined not to be cleared to transition to the requested altitude based on a projected transition, any existing weather hazards, wake vortices of proximate aircraft, and in-trail procedures.

Abstract translation: 系统和方法，用于提高情境认知程序的显示。 雷达系统发射雷达信号，并将天气雷达反射率值接收并存储到三维缓冲器中。 处理器确定所存储的天气反射率值中的任何一个是否表示存在天气危害，并且基于所存储的天气反射率值产生一个或多个天气危害图标。 录像过程显示设备显示生成的天气危害图标。 在其他飞行器的唤醒涡流信息被生成并且在轨迹上的程序显示输出。 此外，处理器接收高度变化的请求，并且当飞行器被确定为不被清除以基于预计的过渡，任何现有的天气危险，邻近飞机的尾流涡流， 跟踪程序。

公开(公告)号：US10330493B2

公开(公告)日：2019-06-25

申请号：US14559755

申请日：2014-12-03

Applicant: Honeywell International Inc.

Inventor： Raghu Shamasundar ,  Prasad Rao Piradi ,  Thomas D. Judd ,  David Pepitone ,  Abhishek Gupta ,  Adib Bouanani ,  Prashanth Ramanna

IPC: G01C23/00 ,  G06F3/0481

Abstract: Systems and methods for displaying position sensitive datalink messages on avionics displays are provided. In one embodiment, a flight deck instrument display system for an aircraft comprises: a flight plan display screen that displays a graphical representation of at least a part of an aircraft's planned flight path together with symbology representing a position of the aircraft with respect to the aircraft's planned flight path; wherein the flight plan display screen further displays at least one symbol positioned along the graphical representation of at least a part of the aircraft's planned flight path that indicates a point of applicability for a received uplink datalink message.

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。