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公开(公告)号：US20140081485A1
公开(公告)日：2014-03-20
申请号：US13725739
申请日：2012-12-21
Applicant: Honeywell International Inc.
Inventor： Blake Wilson , Jary Engels , Ivan Sandy Wyatt , Roger W. Burgin
CPC classification number: G08G5/0047 , G01C23/005 , G08G5/0021 , G08G5/025
Abstract: Methods are provided for presenting procedure information for an airport on a display device onboard an aircraft. A method comprises displaying a map on a display device and displaying a briefing panel overlying a portion the map. The briefing panel includes a plurality of segments, wherein each segment is associated with a type of procedure information for the airport.
Abstract translation: 提供了用于呈现飞机上的显示装置上的机场的程序信息的方法。 一种方法包括在显示装置上显示地图，并显示覆盖地图部分的简报面板。 简报面板包括多个段，其中每个段与机场的一种程序信息相关联。
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公开(公告)号：US20250078664A1
公开(公告)日：2025-03-06
申请号：US18461155
申请日：2023-09-05
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Steven Smith , Jary Engels
IPC: G08G5/00
Abstract: A method and system for determining and displaying a turn to a heading entry for an aircraft has been developed. First, a preliminary heading selection and a preliminary turn direction are entered into an automated flight control system (AFCS) for an aircraft. The preliminary heading selection and the preliminary turn direction are displayed to a pilot of the aircraft. A subsequent heading selection is entered into the AFCS while the aircraft is engaged in turning to the preliminary heading selection in the preliminary turn direction. A shortest turn radius to the subsequent heading selection is determined. A determination is made if the shortest turn radius to the subsequent heading selection is the same direction and the preliminary turn direction and a notice is displayed to the pilot of the aircraft is the shortest turn radius to the subsequent heading selection is not the same direction and the preliminary turn direction.
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公开(公告)号：US10565883B2
公开(公告)日：2020-02-18
申请号：US15649138
申请日：2017-07-13
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Aaron Gannon , Jary Engels , Chris Hamblin
IPC: G08G5/00 , G01C23/00 , G09B5/02 , G09B19/16 , G06F3/0481 , G06F3/0482
Abstract: A practice airspace management system includes a control unit configured to receive user inputs from a first user and to generate a first training plan based on the user inputs. The control unit is further configured to generate display commands representing the first training plan on a navigation map. The practice airspace management system further includes a display device coupled to receive the display commands from the control unit and configured to display a navigation map view that includes the navigation map and a first training plan symbol representing the first training plan on the navigation map.
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Patent Agency Ranking
公开(公告)号：US20200026308A1
公开(公告)日：2020-01-23
申请号：US16202583
申请日：2018-11-28
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Ivan Sandy Wyatt , Luis Ventura Melendez , John Koenig , Jary Engels
Abstract: An aircraft flight control system and method are provided. The system provides a control module that receives inertial data, sensor data, and a target airspeed. The control module processes the received data with aircraft thrust and drag models to evaluate the aircraft energy state. Based on the aircraft energy state, the control module determines (i) a maximum predicted potential flight path “max PPFP”, defined by a maximum thrust at the target airspeed, and (ii) an idle predicted potential flight path, “idle PPFP,” defined by an idle thrust at the target airspeed. The control module generates display commands for a display system to display (i) the flight path angle, (ii) the max PPFP and (iii) the idle PPFP. In addition, the control module generates and displays a predicted flight path speed indicator (PFPS) when the FPA is above the max PPFP or below the idle PPFP.
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15.发明申请公开(公告)号：US20190291889A1
公开(公告)日：2019-09-26
申请号：US15935943
申请日：2018-03-26
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Thea L. Feyereisen , Gang He , Jary Engels , Subash Samuthirapandian
Abstract: Methods and systems are provided for generating an alert for an aircraft potentially exceeding speed limits in airspace with speed limitations. The method comprises retrieving a flight plan for the aircraft and identifying airspace with speed limitations along the flight plan. A speed profile is generated based on the in-flight aircraft's current position, speed and trajectory. Any predicted speed violations are identified by comparing the speed profile with the airspace with speed limitations along the flight plan. A predictive time window is calculated that allows for the in-flight aircraft to decelerate sufficiently to comply with the speed limits of the airspace with speed limitations. The predictive time window includes a zone for the aircraft to reduce its airspeed and a reaction buffer zone to allow the aircrew sufficient time to comply with instructions to decelerate the aircraft. Finally, an alert is generated for the crew of the in-flight aircraft upon entering the predictive time window.
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公开(公告)号：US20190019419A1
公开(公告)日：2019-01-17
申请号：US15649138
申请日：2017-07-13
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Aaron Gannon , Jary Engels , Chris Hamblin
CPC classification number: G08G5/0034 , G01C23/00 , G06F3/04815 , G06F3/0482 , G08G5/0013 , G08G5/0021 , G08G5/0039 , G09B5/02 , G09B19/165
Abstract: A practice airspace management system includes a control unit configured to receive user inputs from a first user and to generate a first training plan based on the user inputs. The control unit is further configured to generate display commands representing the first training plan on a navigation map. The practice airspace management system further includes a display device coupled to receive the display commands from the control unit and configured to display a navigation map view that includes the navigation map and a first training plan symbol representing the first training plan on the navigation map.
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17.发明申请公开(公告)号：US20170083206A1
公开(公告)日：2017-03-23
申请号：US14858725
申请日：2015-09-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Gang He , Jary Engels
IPC: G06F3/0481 , G06T15/00 , G08G5/00 , G09G5/377 , G01C23/00 , B64D43/00 , G06F3/0484 , G06T11/00
CPC classification number: G06F3/04817 , B64D43/00 , G01C23/005 , G06F3/04845 , G06T11/00 , G06T15/00 , G08G5/0021 , G08G5/025 , G09G5/377 , G09G2380/12
Abstract: Flight deck display systems and methods for generating cockpit displays including dynamic taxi turnoff icons are provided. In one embodiment, the flight deck display system includes a display device, a memory storing an airport map database, and a controller operably coupled to the display device and to the memory. The controller is configured to recall information from the airport map database pertaining to a runway cleared for usage by the aircraft. The controller further identifies a taxi exit along the runway based, at least in part, on the information recalled from the airport map database. The controller then generates a dynamic taxi turnoff icon on the display device including symbology representative of the runway and the location of the taxi exit along the runway.
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公开(公告)号：US09014879B2
公开(公告)日：2015-04-21
申请号：US14028691
申请日：2013-09-17
Applicant: Honeywell International Inc.
Inventor： Aaron Gannon , Ivan Sandy Wyatt , Jary Engels , Steven P. Grothe
CPC classification number: B64D45/00 , G01C23/005 , G08G5/0013 , G08G5/0021 , G10L15/26
Abstract: A system and method for validating data entry in response to an instruction received in an aircraft cockpit includes receiving, in an aircraft cockpit, an instruction that requires an aircraft pilot to manually enter a target value into an avionics system using an avionics system user interface. The received instruction is processed to determine the target value that should be set by the aircraft pilot using the avionics system user interface. Haptic feedback is to the avionics system user interface during the manual entry by the aircraft pilot.
Abstract translation: 用于响应于在飞行器驾驶舱中接收的指令来验证数据输入的系统和方法包括在飞行器驾驶舱中接收要求飞行员飞行员使用航空电子系统用户界面手动地将目标值输入到航空电子系统的指令。 处理接收到的指令以确定飞机飞行员应使用航空电子系统用户界面设置的目标值。 触觉反馈是航空器飞行员手动输入期间的航空电子系统用户界面。
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