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101.发明公开公开(公告)号：US20230211892A1
公开(公告)日：2023-07-06
申请号：US17646808
申请日：2022-01-03
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Thea Feyereisen , Ratan Khatwa , Gang He
CPC classification number: B64D43/00 , B64D45/00 , B64D2045/0085
Abstract: Systems and methods for presenting a qualitative risk assessment for an aircraft to perform a flight procedure. Methods include determining: a pilot support value that is representative of a human-machine interface (HMI) onboard the aircraft; a crew factors value representative of a number of pilots and respective experience; an equipment state value of the aircraft, representing available and functioning avionic systems; a type of procedure for the flight procedure; a remaining trip length; an airport facilities state value; an Airport facilities state value; a physical environment value; and, an environmental state value. The method calculates the qualitative risk assessment, as a function of the determined values/factors and presents the qualitative risk assessment in a predefined area on an avionic display in the aircraft.
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公开(公告)号：US11688291B2
公开(公告)日：2023-06-27
申请号：US16920114
申请日：2020-07-02
Applicant: HONEYWELL INTERNATIONAL INC.
CPC classification number: G08G5/065 , G01C21/3676 , G08G5/0021 , G08G5/0078
Abstract: Methods and systems of determining and displaying a taxiing route on an airport moving map. The methods and systems include computer implemented steps of: deriving a location of the ground traffic with respect to taxiways or runways at an airport and a direction of travel of the ground traffic, executing a route planning algorithm for determining a route including one or more taxiways and runways from an aircraft location to the taxi destination using, as inputs, airport data from an airport mapping database, the location of the ground traffic, the direction of travel of the ground traffic, and a taxi destination, and generating a display for the display device including an airport moving map based on airport data from the airport mapping database and including a graphical depiction of the route on the airport moving map.
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公开(公告)号：US11670181B2
公开(公告)日：2023-06-06
申请号：US17062781
申请日：2020-10-05
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Anoop S , Mohammed Ibrahim Mohideen , Gang He
CPC classification number: G08G5/025 , B64C29/0025 , B64D47/08 , G06T3/40 , G06T3/60 , G06T7/70 , G06T11/00
Abstract: The present disclosure relates to a vertical takeoff and landing, VTOL, vehicle having a landing aid and associated methods. The landing aid includes at least one processor is configured to: receive image data from an image capture device, receive altitude data from the altimeter, retrieve template landing pad image data for a target landing pad from the database, scale the template landing pad image data based on the altitude data, compare the scaled template landing pad image data and the image data received from the image capture device to locate the target landing pad therein, thereby providing target landing pad localization data, and control a function of the VTOL vehicle based on the target landing pad localization data.
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公开(公告)号：US20220122466A1
公开(公告)日：2022-04-21
申请号：US17112140
申请日：2020-12-04
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Thea Feyereisen , Rakshit R , Gang He
Abstract: Methods and systems are provided for guiding or otherwise assisting operation of an aircraft when diverting from a flight plan. One method involves determining a gliding trajectory for the aircraft based at least in part on a current altitude of the aircraft, providing a graphical representation of the gliding trajectory for the aircraft, identifying a plurality of landing locations within a range defined by the gliding trajectory from the aircraft, and for each landing location of the plurality of landing locations, providing a graphical representation of a respective landing location with respect to the gliding trajectory at a respective altitude associated with the respective landing location and at a respective distance with respect to a graphical representation of the aircraft corresponding to a respective geographic distance between a current location of the aircraft and the respective landing location.
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公开(公告)号：US20220005364A1
公开(公告)日：2022-01-06
申请号：US16920114
申请日：2020-07-02
Applicant: HONEYWELL INTERNATIONAL INC.
Abstract: Methods and systems of determining and displaying a taxiing route on an airport moving map. The methods and systems include computer implemented steps of: deriving a location of the ground traffic with respect to taxiways or runways at an airport and a direction of travel of the ground traffic, executing a route planning algorithm for determining a route including one or more taxiways and runways from an aircraft location to the taxi destination using, as inputs, airport data from an airport mapping database, the location of the ground traffic, the direction of travel of the ground traffic, and a taxi destination, and generating a display for the display device including an airport moving map based on airport data from the airport mapping database and including a graphical depiction of the route on the airport moving map.
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Patent Agency Ranking
公开(公告)号：US11104449B2
公开(公告)日：2021-08-31
申请号：US16250010
申请日：2019-01-17
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Jan Bilek , Thea L. Feyereisen , Gang He , Peter Chudy , Bryan Charles Weaver , Jakub Dluhos
IPC: B64D45/00 , G01W1/02 , G08G5/00 , G07C5/08 , G01C23/00 , B64D43/00 , G06F3/14 , G01W1/00 , G09G5/37
Abstract: A significant weather advisory system for an aircraft is disclosed. The system is configured to identify, from strategic weather data, current significant weather events from weather impacted areas projected to be intersected by a geographical corridor around a projected flight path and projected to occur during determined time intervals during which the airborne vehicle is expected to pass through the weather impacted areas; compare the current significant weather events to previously identified significant weather events and detect significant changes between the current significant weather events and the previously identified significant weather events; and generate a notification for display to the flight crew via an onboard notification system that identifies the detected significant change when a significant change is detected.
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公开(公告)号：US20210233419A1
公开(公告)日：2021-07-29
申请号：US16750560
申请日：2020-01-23
Applicant: HONEYWELL INTERNATIONAL INC.
Abstract: A flight deck system and a method for providing a flight crew with a ground path to a destination at an aerodrome for taxiing is disclosed. The flight deck system includes a controller configured to: set a destination point on the ground at the aerodrome for an airborne aircraft that is preparing to land; estimate a stopping point for the aircraft on a runway; and predict a ground path for the aircraft to follow at the aerodrome from the runway to the destination point. To predict the controller is further configured to: determine a starting point on the runway for the predicted ground path; and determine a runway exit point to a taxiway. The controller is further configured to cause the predicted ground path to be displayed on a flight deck display device.
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公开(公告)号：US20210225181A1
公开(公告)日：2021-07-22
申请号：US17062742
申请日：2020-10-05
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Thea Feyereisen , Gang He , Pramod Malviya , Zuowei He
Abstract: The present disclosure relates to aircraft display systems and methods for providing ground traffic collision threat awareness. Traffic data is received, optionally from an automatic dependent surveillance broadcast, ADSB, system, including location data for other vehicles. Threat level data is determined representing an urgency of a threat of a surface collision with another vehicle based on the traffic data. The threat level data and the location data for the another vehicle is encoded into graphical symbology for a primary flight display device and into graphical symbology for a navigation display device. The graphical symbology is displayed on the primary flight display device and on the navigation display device.
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公开(公告)号：US10732788B1
公开(公告)日：2020-08-04
申请号：US16247167
申请日：2019-01-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Hariharan Saptharishi , Gobinathan Baladhandapani , Gang He , Narayanan Srinivasan
IPC: G06F3/048 , G06F3/0481 , G10L15/22 , G08G5/00 , G10L15/18 , G06F3/0482 , G06F40/205
Abstract: A system for presenting broadcasted aeronautical information in an aircraft is provided. The system is configured to: capture a broadcasted aeronautical information message; parse the broadcasted message into a plurality of message components; extract a plurality of message features from the plurality of message components; categorize each message feature based on a flight phase to which the message feature pertains; group each categorized message feature into a predetermined one of a plurality of avionic subcategories; associate each subcategorized message feature with one of a plurality of context-based graphical elements, wherein each context-based graphical element is configured to display textual information descriptive of the message feature and/or graphical information descriptive of the message feature; and cause the display of descriptive information regarding a first category of the subcategorized message features via their associated context-based graphical element in a graphical user interface (GUI) display.
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110.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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