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公开(公告)号：US20160063866A1
公开(公告)日：2016-03-03
申请号：US14475067
申请日：2014-09-02
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Helena Trefilova , Petr Casek
CPC classification number: G08G5/0004 , B64D45/00 , G01S13/9303 , G08G5/0008 , G08G5/0013 , G08G5/0021 , G08G5/0052 , G08G5/0078 , G08G5/025
Abstract: A display system for a subject aircraft is provided. The system includes a processing unit configured to receive air traffic spacing information associated with a lead aircraft and flight information associated with the subject aircraft and to generate display signals associated with the air traffic spacing information and the flight information; and a display unit coupled to the processing unit and configured to receive the display signals from the processing unit and to render a horizontal situation indicator with spacing symbology based on the air traffic spacing information and the flight information.
Abstract translation: 提供了一种用于主题飞机的显示系统。 该系统包括：处理单元，被配置为接收与主飞行器相关联的空中交通间隔信息和与主体航空器相关联的飞行信息，并且产生与空中交通间隔信息和飞行信息相关联的显示信号; 以及显示单元，其耦合到所述处理单元并且被配置为从所述处理单元接收所述显示信号，并且基于所述空中交通间隔信息和所述航班信息呈现具有间隔符号的水平状况指示符。
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公开(公告)号：US10916149B2
公开(公告)日：2021-02-09
申请号：US15907776
申请日：2018-02-28
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Zdenek Eichler , Robert Sosovicka , Jiri Svoboda , Helena Trefilova , Tomas Bouda
IPC: G08G5/00
Abstract: Methods and systems are provided for optimizing aircraft operations using uplink weather data to identify predicted turbulent conditions. The method comprises uploading current weather data to a flight management system (FMS) of an aircraft. Areas of turbulence are identified according to the uploaded weather data including areas of turbulence along the client flight trajectory stored in the FMS of the aircraft. An optimal turbulence penetration speed is planned for each identified area of turbulence. The estimated time of arrival (ETA) and minimum and maximum estimate time of arrival (ETA min/max) for the aircraft is recalculated based on the optimal turbulence penetration speeds. The recalculated ETA and ETA min/max is automatically transmitted to an air traffic control (ATC) authority with the FMS of the aircraft.
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Patent Agency Ranking
公开(公告)号：US20190266900A1
公开(公告)日：2019-08-29
申请号：US15907776
申请日：2018-02-28
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Zdenek Eichler , Robert Sosovicka , Jiri Svoboda , Helena Trefilova , Tomas Bouda
IPC: G08G5/00
Abstract: Methods and systems are provided for optimizing aircraft operations using uplink weather data to identify predicted turbulent conditions. The method comprises uploading current weather data to a flight management system (FMS) of an aircraft. Areas of turbulence are identified according to the uploaded weather data including areas of turbulence along the client flight trajectory stored in the FMS of the aircraft. An optimal turbulence penetration speed is planned for each identified area of turbulence. The estimated time of arrival (ETA) and minimum and maximum estimate time of arrival (ETA min/max) for the aircraft is recalculated based on the optimal turbulence penetration speeds. The recalculated ETA and ETA min/max is automatically transmitted to an air traffic control (ATC) authority with the FMS of the aircraft.
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公开(公告)号：US11094207B2
公开(公告)日：2021-08-17
申请号：US16682603
申请日：2019-11-13
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Ratan Khatwa , Melissa Ziarnick , Helena Trefilova , Pavel Klang , Stephen Whitlow
Abstract: Systems and methods directed to improvements in the presentation of CAVS procedures on an aircraft display system over what is conventionally available are provided. The provided systems and methods employ a vertical situation display (VSD), thereby presenting additional relevant visual approach information, such as a vertical distance between the ownship and the target aircraft, descent rates of the ownship and the target and an alerting function for the user-selected CAVS range. The provided systems and methods also capably receive and process user selections of target aircraft from both the lateral display and the VSD.
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5.发明申请公开(公告)号：US20190019422A1
公开(公告)日：2019-01-17
申请号：US15647471
申请日：2017-07-12
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Ratan Khatwa , Melissa Ziarnick , Helena Trefilova , Pavel Klang , Stephen Whitlow
Abstract: Systems and methods directed to improvements in the presentation of CAVS procedures on an aircraft display system over what is conventionally available are provided. The provided systems and methods employ a vertical situation display (VSD), thereby presenting additional relevant visual approach information, such as a vertical distance between the ownship and the target aircraft, descent rates of the ownship and the target and an alerting function for the user-selected CAVS range. The provided systems and methods also capably receive and process user selections of target aircraft from both the lateral display and the VSD.
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6.发明申请公开(公告)号：US20200168110A1
公开(公告)日：2020-05-28
申请号：US16682603
申请日：2019-11-13
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Ratan Khatwa , Melissa Ziarnick , Helena Trefilova , Pavel Klang , Stephen Whitlow
Abstract: Systems and methods directed to improvements in the presentation of CAVS procedures on an aircraft display system over what is conventionally available are provided. The provided systems and methods employ a vertical situation display (VSD), thereby presenting additional relevant visual approach information, such as a vertical distance between the ownship and the target aircraft, descent rates of the ownship and the target and an alerting function for the user-selected CAVS range. The provided systems and methods also capably receive and process user selections of target aircraft from both the lateral display and the VSD.
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公开(公告)号：US09501936B2
公开(公告)日：2016-11-22
申请号：US14475067
申请日：2014-09-02
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Helena Trefilova , Petr Casek
CPC classification number: G08G5/0004 , B64D45/00 , G01S13/9303 , G08G5/0008 , G08G5/0013 , G08G5/0021 , G08G5/0052 , G08G5/0078 , G08G5/025
Abstract: A display system for a subject aircraft is provided. The system includes a processing unit configured to receive air traffic spacing information associated with a lead aircraft and flight information associated with the subject aircraft and to generate display signals associated with the air traffic spacing information and the flight information; and a display unit coupled to the processing unit and configured to receive the display signals from the processing unit and to render a horizontal situation indicator with spacing symbology based on the air traffic spacing information and the flight information.
Abstract translation: 提供了一种用于主题飞机的显示系统。 该系统包括：处理单元，被配置为接收与主飞行器相关联的空中交通间隔信息和与主体航空器相关联的飞行信息，并且产生与空中交通间隔信息和飞行信息相关联的显示信号; 以及显示单元，其耦合到所述处理单元并且被配置为从所述处理单元接收所述显示信号，并且基于所述空中交通间隔信息和所述航班信息呈现具有间隔符号的水平状况指示符。
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