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公开(公告)号：US20140266807A1
公开(公告)日：2014-09-18
申请号：US13846424
申请日：2013-03-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dilip Kumar Behara , Naveen Venkatesh Prasad Nama , Aaron Gannon , Marc L. Lajeunesse
IPC: G01C23/00
CPC classification number: G01C23/00
Abstract: A system and method are provided for graphically displaying airspace data including speed restrictions on an aircraft display. The system comprises an avionics display system coupled to a processor that is configured to retrieve airspace data from a database, display the aircraft data on the display, and display a visual representation of the airspace. Then the processor may alter the format of the visual representation of the airspace to a second visual representation, if the airspace data meets predetermined criteria.
Abstract translation: 提供了一种系统和方法，用于图形地显示包括飞行器显示器上的速度限制的空域数据。 该系统包括耦合到处理器的航空电子显示系统，其被配置为从数据库检索空域数据，在显示器上显示飞行器数据，并且显示空域的视觉表示。 那么如果空域数据满足预定的标准，则处理器可以将空域的视觉表示的格式改变为第二视觉表示。
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公开(公告)号：US11604575B2
公开(公告)日：2023-03-14
申请号：US16701769
申请日：2019-12-03
Applicant: Honeywell International Inc.
Inventor： Ivan S. Wyatt , Katarina Alexis Morowsky , Aaron Gannon , Christopher Heine
IPC: G06F3/04847 , G06F3/0482 , H04L41/22
Abstract: Disclosed are methods, systems, and non-transitory computer-readable medium for managing configurations of multiple vehicle displays. For instance, a method may include: obtaining a configurable file for an electronic checklist; generating a graphical user interface (GUI) based on the configurable file; displaying the GUI on one of the multiple vehicle displays; receiving a user input on the GUI; and performing a window configuration setting process based on the user input. The method may also include: in response to the user input being a first user input type in a region associated with a context menu indicator: obtaining a window configuration function and a phase of flight variable; generating a context menu based on the window configuration function and the POF variable; and displaying the context menu on the GUI.
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公开(公告)号：US20190384490A1
公开(公告)日：2019-12-19
申请号：US16400930
申请日：2019-05-01
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Katarina Alexis Morowsky , Ivan Sandy Wyatt , Vincent Vu , Aaron Gannon
IPC: G06F3/0488 , B64D43/00 , G06F3/0485 , G06F3/0484
Abstract: A contextual awareness system for an aircraft and a method from controlling the same are provided. The aircraft, for example, may include, but is not limited to, a touch screen display, a memory configured to store rules defining a relationship between a plurality of data fields, and a processor configured to determine when a data field displayed on the touch screen display is selected, determine at least one data field which is related to the selected data field based upon the rules defining the relationship between a plurality of data fields, generate display data for the touch screen display, the display data comprising a virtual keyboard and a contextual awareness display area, the contextual awareness display area displaying the selected field and the at least one data field which is related to the selected data, and update the selected data field based upon input from the virtual keyboard.
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公开(公告)号：US20190016472A1
公开(公告)日：2019-01-17
申请号：US15651413
申请日：2017-07-17
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Katarina Alexis Morowsky , Ivan Sandy Wyatt , Aaron Gannon
IPC: B64D45/00
Abstract: A flight deck timer management system includes a database storing conditions representing a first monitoring mode defining at least a first rule, a first timing characteristic defining a first time period for compliance with the first rule, and a first advisory value relative to the first time period at which a first advisory is initiated. A control unit is configured to identify input states based on the input data, and to evaluate the input states in view of the first monitoring mode conditions. When the input states trigger the first monitoring mode, the control unit evaluates the input states in view of the first rule, initiates a first timer based on the first timing characteristic, monitors a first timing status of the first timer relative to the first advisory value, and generates display commands representing the first advisory when the first timer status reaches the first advisory value.
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25.发明授权公开(公告)号：US10053224B2
公开(公告)日：2018-08-21
申请号：US15171417
申请日：2016-06-02
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dave Pepitone , John Meeker , Mark Giddings , Ivan Sandy Wyatt , John Suddreth , Aaron Gannon
CPC classification number: B64D43/00 , G01C23/005 , G06F3/04817 , G06F3/14 , G06T11/60 , G06T2210/36 , G06T2210/61 , G08G5/003 , G09G5/02 , G09G5/391 , G09G2320/10 , G09G2340/0407 , G09G2380/12
Abstract: A system method for providing aircraft lateral navigation system capability feedback to a pilot includes determining, in a processor, when a flight plan has been received that includes a flight leg that needs to be captured by the aircraft. A determination is made, in the processor, when an armed signal has been received, where the armed signal indicating that an aircraft autopilot navigation mode (NAV) has been armed. The processor is used to command a display device to render the flight leg using a first display paradigm when the armed signal has not been received, and to render the flight leg using a second display paradigm when the armed signal has been received.
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Patent Agency Ranking
公开(公告)号：US09640081B2
公开(公告)日：2017-05-02
申请号：US14840908
申请日：2015-08-31
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Aaron Gannon , Ivan Sandy Wyatt , Troy Nichols , John G. Suddreth
CPC classification number: G08G5/025 , G08G5/0021 , G08G5/0047
Abstract: A dynamic runway indicator is displayed overlying a conformal runway for assisting a pilot in completing an approach to landing on a runway. The dynamic runway indicator includes a polygon, that by changing position with respect to the conformal runway, provides advanced instrumentation cues to the pilot for adjusting the aircraft flight path to a normal, or recommended, path to the runway for landing, thereby assisting the pilot to improve the accuracy and safety of the approach and landing.
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27.发明授权公开(公告)号：US09524142B2
公开(公告)日：2016-12-20
申请号：US14224370
申请日：2014-03-25
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Steve Grothe , Aaron Gannon , John Foster
CPC classification number: G06F3/162 , B64D43/00 , G06F3/017 , G08C23/04 , G08C2201/40
Abstract: A 3D gesture based interface for controlling audio information in flight deck applications is provided. The system and method utilize a set of simple, intuitive 3D gestures, and unburden the pilot of searching for specific audio device controls. The system and method are intuitive and enable the pilot to quickly silence or subdue non-essential audio information, before interfering with essential audio information.
Abstract translation: 提供了一种用于控制飞行甲板应用中的音频信息的基于3D手势的界面。 该系统和方法利用一套简单，直观的3D手势，并且解除了导频搜索特定音频设备控制的负担。 该系统和方法是直观的，并且能够在干扰基本音频信息之前使飞行员能够快速地沉默或者制止非必要音频信息。
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28.发明授权System and method for displaying predictive conformal configuration cues for executing a landing 有权用于显示执行着陆的预测保形配置线索的系统和方法公开(公告)号：US09418561B2
公开(公告)日：2016-08-16
申请号：US14558067
申请日：2014-12-02
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Aaron Gannon , Ivan Sandy Wyatt , Thea L. Feyereisen
CPC classification number: G08G5/0056 , G08G5/0021 , G08G5/0039 , G08G5/025
Abstract: A system and method for displaying predictive cues on an aircraft display system for executing a landing after an engine failure is provided. The system and method displays the cues for various aircraft configurations, and each cue is displayed in perspective (conformally) on a three dimensional graphical display of the surrounding terrain.
Abstract translation: 一种用于在飞机显示系统上显示用于执行发动机故障之后的着陆的预测线索的系统和方法。 系统和方法显示各种飞机配置的提示，并且每个提示以透视（保形）显示在周围地形的三维图形显示上。
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公开(公告)号：US09377325B2
公开(公告)日：2016-06-28
申请号：US13846424
申请日：2013-03-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dilip Kumar Behara , Naveen Venkatesh Prasad Nama , Aaron Gannon , Marc L. Lajeunesse
CPC classification number: G01C23/00
Abstract: A system and method are provided for graphically displaying airspace data including speed restrictions on an aircraft display. The system comprises an avionics display system coupled to a processor that is configured to retrieve airspace data from a database, display the aircraft data on the display, and display a visual representation of the airspace. Then the processor may alter the format of the visual representation of the airspace to a second visual representation, if the airspace data meets predetermined criteria.
Abstract translation: 提供了一种系统和方法，用于图形地显示包括飞行器显示器上的速度限制的空域数据。 该系统包括耦合到处理器的航空电子显示系统，其被配置为从数据库检索空域数据，在显示器上显示飞行器数据，并且显示空域的视觉表示。 那么如果空域数据满足预定的标准，则处理器可以将空域的视觉表示的格式改变为第二视觉表示。
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公开(公告)号：US20150277848A1
公开(公告)日：2015-10-01
申请号：US14224370
申请日：2014-03-25
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Steve Grothe , Aaron Gannon , John Foster
CPC classification number: G06F3/162 , B64D43/00 , G06F3/017 , G08C23/04 , G08C2201/40
Abstract: A 3D gesture based interface for controlling audio information in flight deck applications is provided. The system and method utilize a set of simple, intuitive 3D gestures, and unburden the pilot of searching for specific audio device controls. The system and method are intuitive and enable the pilot to quickly silence or subdue non-essential audio information, before interfering with essential audio information.
Abstract translation: 提供了一种用于控制飞行甲板应用中的音频信息的基于3D手势的界面。 该系统和方法利用一套简单，直观的3D手势，并且解除了导频搜索特定音频设备控制的负担。 该系统和方法是直观的，并且能够在干扰基本音频信息之前使飞行员能够快速地沉默或者制止非必要音频信息。
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