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1. 发明授权

US11549821B2 Runway landing alert system and method 有权
公开(公告)号：US11549821B2
公开(公告)日：2023-01-10
申请号：US16912358
申请日：2020-06-25
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Glen Burlingame , Yasuo Ishihara , Steve Johnson , James Ehlers , Esko Mannisto
IPC分类号： G06G7/70 , G01C23/00 , B64D45/00 , B64D45/08 , G08G5/00 , G08G5/02
摘要： Methods and apparatus are provided for generating a runway landing alert for an aircraft. The method comprises establishing a Runway Awareness Advisory System (RAAS) envelope for the designated target runway of the aircraft. A track of the aircraft is monitored with reference to a centerline of the target runway. Any deviation by the aircraft from the centerline of the target runway is detected and determined if it is within a margin of error. If the deviation is within the margin of error, an altitude parameter of the RAAS envelope is increased. If the aircraft is determined to still be maneuvering with respect to the centerline of the target runway, the altitude parameter of the RAAS envelope is decreased. Otherwise, an alert is generated if the aircraft is outside of the RAAS envelope.

2. 发明申请

US20230115810A1 RUNWAY LANDING ALERT SYSTEM AND METHOD 有权
公开(公告)号：US20230115810A1
公开(公告)日：2023-04-13
申请号：US18065429
申请日：2022-12-13
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Glen Burlingame , Yasuo Ishihara , Steve Johnson , James Ehlers , Esko Mannisto
IPC分类号： G01C23/00 , B64D45/00 , B64D45/08 , G08G5/00 , G08G5/02
摘要： Methods and apparatus are provided for generating a runway landing alert for an aircraft. The method comprises establishing an altitude parameter and a safety envelope for a designated target runway of the aircraft. A track of the aircraft is monitored with reference to a centerline of the target runway. Any deviation by the aircraft from the centerline of the target runway is detected and determined if it is within a margin of error. If the deviation is within the margin of error, an altitude parameter is increased. If the aircraft is determined to still be maneuvering with respect to the centerline of the target runway, the altitude parameter is decreased. Otherwise, an alert is generated if the aircraft is outside of the safety envelope.

3. 发明授权

US09731838B2 System and method for runway selection through scoring 有权
公开(公告)号：US09731838B2
公开(公告)日：2017-08-15
申请号：US14192088
申请日：2014-02-27
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Kevin J Conner , Yasuo Ishihara , Steve Johnson
IPC分类号： G08G5/00 , B64D45/00 , G08G5/02
CPC分类号： B64D45/00 , G08G5/0021 , G08G5/025
摘要： A system and method for selecting a runway, comprises retrieving runway feature data and aircraft data including aircraft heading with respect to the bearing of first and second runways. Runway boundary envelopes are created for each of the first and second runways, each having a predetermined score. A total score for each of the first and second runways is compared to determine which of the runways is selected.

4. 发明申请

US20170053539A1 SYSTEMS AND METHODS FOR DESTINATION SELECTION FOR VEHICLE INDICATIONS AND ALERTS 有权
标题翻译：用于车辆指示和警报的目的地选择的系统和方法
公开(公告)号：US20170053539A1
公开(公告)日：2017-02-23
申请号：US14831032
申请日：2015-08-20
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Thea L. Feyereisen , Steve Johnson , Gang He , Yasuo Ishihara , Ivan Sandy Wyatt
IPC分类号： G08G5/02 , G08G5/00
CPC分类号： G08G5/025 , G08G5/0021
摘要： A method for providing alerts or indications to an aircrew of an aircraft that is in-flight and approaching a destination airport includes receiving an aircrew runway selection from the aircrew of the aircraft, automatically generating a probable runway selection by the aircraft, and determining a position of the in-flight aircraft with reference to a threshold point. If the aircraft is prior to the threshold point, the method includes generating alerts and indications to the aircrew based solely on the received runway selection into the FMS from the aircrew of the aircraft and not on the automatically-generated probable runway selection from the aircraft. Alternatively, if the aircraft is past the threshold point, the method includes generating alerts and indications to the aircrew based solely on the automatically-generated probable runway selection from the aircraft and not on the received runway selection into the FMS from the aircrew of the aircraft.
摘要翻译：用于向飞行中和接近目的地机场的飞机的机组人员提供警报或指示的方法包括从飞行器的机组人员接收机组跑道选择，自动产生飞行器可能的跑道选择，以及确定位置参考一个临界点。如果飞行器在阈值点之前，则该方法仅仅基于从飞机的机组人员接收的进入FMS的跑道选择而不是从飞行器自动生成的可能的跑道选择来向机组人员生成警报和指示。或者，如果飞行器超过阈值点，则该方法包括仅基于从飞行器自动生成的可能的跑道选择而不是在从飞机的机组人员接收的进入FMS的跑道选择中产生对机组人员的警报和指示。

5. 发明授权

US09409654B2 System and method for improved low airspeed warning 有权
标题翻译：改进低空速警报的系统和方法
公开(公告)号：US09409654B2
公开(公告)日：2016-08-09
申请号：US14265723
申请日：2014-04-30
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Steve Johnson , Yasuo Ishihara , Charles Donald Bateman
IPC分类号： B64D45/00 , B64D43/02
CPC分类号： B64D45/00 , B64D43/02
摘要： A method and system are provided for generating a low airspeed warning in an aircraft. This method creates a scale factor that is a factor of engine thrust and aircraft altitude. A low airspeed threshold is determined that varies according to the aircraft altitude with respect to a predetermined altitude band and the engine thrust with respect to a predetermined engine thrust band. A low airspeed alert is generated in response to the determination of the low airspeed threshold. This method provides a pilot with earlier knowledge of low airspeed conditions when the aircraft is in a target altitude band, increasing the pilot's response time and thereby enhancing overall aircraft safety.
摘要翻译：提供一种用于在飞行器中产生低空速警告的方法和系统。该方法创建了一个比例因子，它是发动机推力和飞机高度的一个因素。确定根据相对于预定高度带的飞行器高度和相对于预定发动机推力带的发动机推力而变化的低空速阈值。响应于低空速阈值的确定而产生低空速警报。这种方法提供了一个飞行员，当飞机处于目标高度带时，具有较低的空速条件的知识，增加飞行员的响应时间，从而提高整体飞机的安全性。

6. 发明授权

US09399524B2 System and method for displaying runway landing information 有权
标题翻译：显示跑道着陆信息的系统和方法
公开(公告)号：US09399524B2
公开(公告)日：2016-07-26
申请号：US14519741
申请日：2014-10-21
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Gang He , Steve Johnson , Thea L Feyereisen
IPC分类号： G05D1/00 , B64D45/08 , G01C23/00 , B64D45/00
CPC分类号： B64D45/08 , B64D2045/008 , G01C23/00 , G01C23/005 , G08G5/0021 , G08G5/025
摘要： A system and method are disclosed for indicating to an aircrew of an aircraft a normalized runway icon to ensure visualization of a predicted touchdown point, runway length, stopping distance, energy state marking, and threat conditions, where normalization is referenced to typically available length for landing. Indications of present aircraft locations relative to the icons as well as alerts when thresholds are exceeded are provided.
摘要翻译：公开了一种系统和方法，用于向航空器的机组人员指示归一化的跑道图标，以确保预测的着陆点，跑道长度，停止距离，能量状态标记和威胁状况的可视化，其中归一化以通常可用的长度参考降落。提供了相对于图标的当前飞行器位置的指示以及当超过阈值时的警报。

7. 发明申请

US20160090193A1 SYSTEM AND METHOD FOR DISPLAYING RUNWAY APPROACH INFORMATION 有权
标题翻译：显示运行方式信息的系统和方法
公开(公告)号：US20160090193A1
公开(公告)日：2016-03-31
申请号：US14497565
申请日：2014-09-26
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Gang He , Steve Johnson , Thea L. Feyereisen
IPC分类号： B64D45/04 , G08G5/02
CPC分类号： B64D45/04 , G08G5/0021 , G08G5/025
摘要： A system and method are disclosed for indicating to an aircrew of an aircraft an unstable approach to a desired landing. When the energy state of the aircraft exceeds a threshold, a suggested airspeed in consideration of the energy state is displayed. Additionally, a landing spots on a displayed runway are shown indicating where the aircraft would land in view of the energy state and where the aircraft is recommended to land in view of the current aircraft type and weight. A text message may also be displayed that conveys the ability of the aircraft to land.
摘要翻译：公开了一种系统和方法，用于向飞机的机组人员指示对期望着陆的不稳定方法。当飞行器的能量状态超过阈值时，显示考虑能量状态的建议空速。另外，显示的跑道上的着陆点被示出表明飞机将考虑到能量状态而降落在哪里，并且考虑到目前的飞机类型和重量，飞机被推荐降落在哪里。还可以显示一条传达航空器着陆能力的短信。

8. 发明授权

US09293052B2 System and method for modulating alerts for an intended runway 有权
标题翻译：调整预期跑道的警报的系统和方法
公开(公告)号：US09293052B2
公开(公告)日：2016-03-22
申请号：US14060768
申请日：2013-10-23
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Kevin J Conner , Yasuo Ishihara , Steve Johnson
IPC分类号： G08G5/02 , G08G5/00 , G05D1/00 , G05D1/06
CPC分类号： G08G5/0021 , G05D1/0077 , G05D1/0676 , G08G5/0065 , G08G5/025
摘要： A system and method provide an alert to a pilot of an aircraft aurally with a given volume and inflection, and/or visually with a text message which includes color, font, and pitch (size). The alert is rendered in distinct fashion for the expected and unexpected cases, e.g., an intended runway and an unintended runway. In a preferred embodiment, the alert for the intended runway is changed to a confirmation level, or one that is less likely to interfere with other information flow, while the alert for the unintended runway would be provided in a more conspicuous manner.
摘要翻译：一种系统和方法向具有给定音量和拐点的声音的飞行员提供警报，和/或以视觉方式提供包括颜色，字体和音调（大小）的文本消息的警报。对于预期和意想不到的情况，例如预期的跑道和非预期的跑道，警报以不同的方式呈现。在优选实施例中，预期跑道的警报改变为确认级别，或者更不可能干扰其他信息流的警报，同时将以更显眼的方式提供非预期跑道的警报。

9. 发明申请

US20140368359A1 FLIGHT DECK DISPLAY SYSTEMS AND METHODS FOR VISUALLY INDICATING LOW SPEED CHANGE CONDITIONS DURING TAKEOFF AND LANDING 有权
标题翻译：飞行显示系统和方法，用于在起飞和着陆期间显示低速变化条件
公开(公告)号：US20140368359A1
公开(公告)日：2014-12-18
申请号：US13919431
申请日：2013-06-17
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Steve Johnson , Yasuo Ishihara , Kevin J. Conner
IPC分类号： G01P1/10 , G01P5/00
CPC分类号： G01P1/10 , G01C23/00 , G01P5/00
摘要： Embodiments of a flight deck display system deployed onboard an aircraft are provided, as are embodiments of a method carried-out by a flight deck display system. In one embodiment, the flight deck display system includes a cockpit display device and a controller. The controller is configured to: (i) establish the speed trend of the aircraft over a predetermined time period; (ii) generate a primary flight display on the cockpit display device including a speed trend vector graphic representative of the established speed trend; and (iii) alter the appearance of the speed trend vector graphic in a first predetermined manner if a low speed change condition is detected during at least one of aircraft takeoff and landing.
摘要翻译：提供了部署在飞行器上的飞行甲板显示系统的实施例，由飞行甲板显示系统执行的方法的实施例也是如此。在一个实施例中，驾驶舱显示系统包括驾驶舱显示装置和控制器。控制器被配置为：（i）在预定时间段内建立飞机的速度趋势; （ii）在驾驶舱显示装置上产生代表所建立的速度趋势的速度趋势矢量图形的主飞行显示; 以及（iii）如果在飞机起飞和着陆期间的至少一个中检测到低速变化条件，则以第一预定方式改变速度趋势矢量图形的外观。

10. 发明授权

US11472570B2 System and method for modulating premature descent protection envelope 有权
公开(公告)号：US11472570B2
公开(公告)日：2022-10-18
申请号：US16735261
申请日：2020-01-06
申请人： HONEYWELL INTERNATIONAL INC.
发明人： Yasuo Ishihara , Steve Johnson , Kevin J Conner
IPC分类号： B64D45/04 , G01C23/00 , G08G5/02 , G08G5/00 , G05D1/06 , G08G5/04
摘要： A system and method of shifting a premature descent protection envelope for an aircraft has been developed. First, a premature descent protection envelope (PDP) is determined including a first boundary at a first distance from the runway. Next, a nominal approach path is determined for approaching the runway and an approach path angle. Also, a flight path angle of the aircraft is determined. The first boundary is shifted in an upward direction from the runway in response to the aircraft being below the nominal approach path, and the flight path angle being greater than the nominal approach path angle.

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