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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：US20200295794A1
公开(公告)日：2020-09-17
申请号：US16817276
申请日：2020-03-12
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Katarina A. Morowsky , Ivan Sandy Wyatt , Christopher Heine
Abstract: Methods and apparatus are provided for displaying the operational parameters of a radio system located onboard an aircraft. The apparatus comprises a permanent radio display bar that shows an active radio frequency in use by the radio system and a variable radio display pad. The variable radio display pad shows multiple historical past radio frequencies previously used by the radio system and multiple predicted future radio frequencies for use along a flight plan of the aircraft. It includes a change command that allows a crew member to manually change the active radio frequency in the permanent radio display bar.
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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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公开(公告)号：US09666085B2
公开(公告)日：2017-05-30
申请号：US14541649
申请日：2014-11-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Aaron Gannon , Thea L. Feyereisen , Troy Nichols , Jerry Ball , Sean Caufield , John G. Suddreth , Ivan Sandy Wyatt
CPC classification number: G08G5/065 , B60K35/00 , G08G5/0021
Abstract: Methods and systems are provided for displaying a taxi clearance for an aircraft at an airport. One exemplary method involves receiving user input indicative of a constraining taxi path of a plurality of taxi paths at the airport, determining a first taxi portion between an initial location for the taxi clearance and the constraining taxi path, determining a second taxi portion between the constraining taxi path and a destination location for the taxi clearance, and displaying, on a display device associated with the aircraft, a taxi route comprising the first taxi portion, the second taxi portion, and the constraining taxi path between the first taxi portion and the second taxi portion.
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15.发明授权System and method for displaying optimized ownship position on a navigation display 有权用于在导航显示器上显示优化的自身位置的系统和方法公开(公告)号：US09563944B2
公开(公告)日：2017-02-07
申请号：US14243774
申请日：2014-04-02
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Thea L. Feyereisen , Ivan Sandy Wyatt , Gang He
CPC classification number: G06T7/0008 , G01C21/00 , G01C23/00 , G06F3/0485 , G06T11/60 , G06T2207/10016 , G06T2207/10028 , G06T2207/10032 , G06T2207/30232 , G06T2207/30241 , G08G5/0021 , G08G5/0052 , G09G5/14
Abstract: A display system and method for graphically representing a host aircraft comprises a display, a first source host aircraft position data and a second source of data representative of airspace in the vicinity of the host aircraft. A processor is coupled to the display, the first source, and the second source and is configured to (1) determine a position of the host aircraft that expands the visualization of an intended trajectory of the host aircraft, and (2) display the host aircraft at the position on the display.
Abstract translation: 用于图形地表示主机的显示系统和方法包括显示器，第一源主机飞行器位置数据和代表主机附近的空域的第二数据源。 处理器耦合到显示器，第一源和第二源，并且被配置为（1）确定扩展主机飞行器的预期轨迹的可视化的主机飞行器的位置，以及（2）显示主机 飞机在展示位置。
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Patent Agency Ranking
公开(公告)号：US20150371545A1
公开(公告)日：2015-12-24
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
IPC: G08G5/02
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.
Abstract translation: 一个动态跑道指示器显示在一个保形跑道上，以协助飞行员完成在跑道上着陆的方法。 动态跑道指示器包括多边形，其通过相对于保形跑道改变位置，向飞行员提供高级仪表线索，用于调整飞行器飞行路径到达跑道的正常或推荐路径以降落，从而辅助飞行员 提高进场和落地的准确性和安全性。
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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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公开(公告)号：US11356137B2
公开(公告)日：2022-06-07
申请号：US16817276
申请日：2020-03-12
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Katarina A. Morowsky , Ivan Sandy Wyatt , Christopher Heine
Abstract: Methods and apparatus are provided for displaying the operational parameters of a radio system located onboard an aircraft. The apparatus comprises a permanent radio display bar that shows an active radio frequency in use by the radio system and a variable radio display pad. The variable radio display pad shows multiple historical past radio frequencies previously used by the radio system and multiple predicted future radio frequencies for use along a flight plan of the aircraft. It includes a change command that allows a crew member to manually change the active radio frequency in the permanent radio display bar.
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公开(公告)号：US20200280333A1
公开(公告)日：2020-09-03
申请号：US16399555
申请日：2019-04-30
Applicant: Honeywell International Inc.
Inventor： Katarina Alexis Morowsky , Aaron J Gannon , Ivan Sandy Wyatt , Avery Burns , Balaji Srinivasan
IPC: H04B1/401 , H04B1/3822 , H04B1/44 , G06F3/0488 , G08G5/00
Abstract: A switching system comprises a three-way radio switch for an onboard radio system. The radio switch includes a manual standby frequency switch that receives and displays a standby frequency input by a user; an automated standby frequency switch that receives and displays a standby frequency automatically input by the system; and an active frequency switch that shows a currently selected frequency. The active frequency switch receives and displays the frequency from the manual standby frequency switch, or receives and displays the frequency from the automated standby frequency switch. A processor is operative to monitor frequencies of the radio system in real-time; compare the frequencies of the radio system with frequencies from a database containing regional radio frequencies; trigger an alert when the frequencies of the radio system do not match the frequencies from the database; and send an updated standby radio frequency to the automated standby frequency switch.
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公开(公告)号：US10606281B2
公开(公告)日：2020-03-31
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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