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公开(公告)号：US20210158708A1
公开(公告)日：2021-05-27
申请号：US16694649
申请日：2019-11-25
Applicant: Honeywell International Inc.
Inventor： Kiran Perikala , Tulasi Mohan Naraharisetty , Harikrishna Chitneni , Hari Krishna Jasti , Mohan Chandrashekarappa
Abstract: An apparatus and method for identifying potential aircraft fuel jettison and/or burn sites is provided.
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公开(公告)号：US12072206B2
公开(公告)日：2024-08-27
申请号：US17028036
申请日：2020-09-22
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Mohan Chandrashekarappa , Sridevi Nagaraja , Subhra Dey , Kiran Venkataramana , Babitha Jajur
IPC: G06F3/048 , B64D43/00 , G01C5/00 , G01C21/20 , G01C23/00 , G06F3/0482 , G06F3/0483 , G06F3/0484 , G06T11/20 , G08G5/00 , G10L15/26
CPC classification number: G01C23/005 , G01C5/005 , G01C21/20 , G08G5/0021
Abstract: Methods and systems of generating a data driven digital chart. The methods and systems include retrieving a data driven chart for a requested terminal area procedure chart from a database of data driven charts. The data driven charts describe digital terminal area procedure charts by way of data elements for each terminal area procedure chart including geodetic straights, arcs, text elements and symbols defined with respect to location. Some of the data elements are further defined with respect to altitude values assuming a standard atmospheric temperature value. The systems and methods include calculating compensated altitude values for the data elements of the retrieved data driven chart based on a deviation between the outside air temperature value and the standard atmospheric temperature value. The methods and systems include generating a presentation for a display device of the aircraft of the terminal area procedure chart.
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公开(公告)号：US20220121224A1
公开(公告)日：2022-04-21
申请号：US17115875
申请日：2020-12-09
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Mohan Chandrashekarappa , Sridevi Nagaraja , Kiran Venkataramana , Satish Hegde , Raghu Shamasundar
Abstract: A system and method for generating, supplying, and implementing an optimized descent approach profile for an aircraft includes transmitting a current flight plan from an onboard flight management system (FMS) to an off-board computing device. The optimized descent approach profile for the aircraft is computed, in the off-board computing device,. One or more new waypoints or points of interest that are not on the current descent approach profile, but which comprise the optimized descent approach profile, are identified in the off-board computing device. The new waypoints or points of interest are transmitted from the off-board system to the onboard FMS. The current descent approach profile is updated, in the FMS, to include the new waypoints or points of interest, thereby generating an updated flight plan. The updated flight plan is implementing in the onboard FMS.
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Patent Agency Ranking
4.发明申请公开(公告)号：US20210343160A1
公开(公告)日：2021-11-04
申请号：US16905191
申请日：2020-06-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Kiran Venkataramana , Mohan Chandrashekarappa , Sridevi Nagaraja , Babitha Jajur
Abstract: The present disclosure provides systems and methods for flight planning for an autonomous aerial vehicle. The systems and methods perform a processor executed process of receiving a request for flight planning and retrieving a model for the structure or the feature of interest from one or more databases. The request identifies a structure or a feature of interest to be surveyed by the autonomous aerial vehicle. The one or more databases include a database including models of terrain, airports and obstacles or a database including models of manufactured articles based on original equipment manufacturer (OEM) specifications or computer aided design (CAD) models. The process includes computing a flight plan that completely surveys the structure or completely surveys the feature of interest based on the retrieved model. The flight plan defines a search pattern with position values. The process includes uplinking the flight plan to the autonomous aerial vehicle.
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公开(公告)号：US11626024B2
公开(公告)日：2023-04-11
申请号：US16932517
申请日：2020-07-17
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Raghu Shamasundar , Mohan Chandrashekarappa , Philip Toews , Robert Brownlee , Srihari Jayathirtha , Kalimullah Khan , Kiran Venkataramana
IPC: G08G5/00 , H04L67/12 , H04L67/1097
Abstract: An avionics system in an aircraft for providing flight data from an onboard flight management computer (FMC) to requesting applications is disclosed. The system includes a flight management system (FMS) service layer executing on the FMC on a thread separate from a thread that executes FMS core functions. The FMS service layer provides a FMC networked node server for responding to queries from a plurality of external applications for data generated from the FMS core functions without interrupting the FMS core functions. The FMC networked node server is configured to: receive a request from a client application using a server specified API for data elements from a specified input flight plan; retrieve the specified input flight plan from the FMS core functions; extract the requested data elements; and output the requested data elements to the client application without affecting the active thread that executes FMS core functions.
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6.发明授权公开(公告)号：US11600185B2
公开(公告)日：2023-03-07
申请号：US16905191
申请日：2020-06-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Kiran Venkataramana , Mohan Chandrashekarappa , Sridevi Nagaraja , Babitha Jajur
Abstract: The present disclosure provides systems and methods for flight planning for an autonomous aerial vehicle. The systems and methods perform a processor executed process of receiving a request for flight planning and retrieving a model for the structure or the feature of interest from one or more databases. The request identifies a structure or a feature of interest to be surveyed by the autonomous aerial vehicle. The one or more databases include a database including models of terrain, airports and obstacles or a database including models of manufactured articles based on original equipment manufacturer (OEM) specifications or computer aided design (CAD) models. The process includes computing a flight plan that completely surveys the structure or completely surveys the feature of interest based on the retrieved model. The flight plan defines a search pattern with position values. The process includes uplinking the flight plan to the autonomous aerial vehicle.
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公开(公告)号：US20220034682A1
公开(公告)日：2022-02-03
申请号：US17028036
申请日：2020-09-22
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Mohan Chandrashekarappa , Sridevi Nagaraja , Subhra Dey , Kiran Venkataramana , Babitha Jajur
Abstract: Methods and systems of generating a data driven digital chart. The methods and systems include retrieving a data driven chart for a requested terminal area procedure chart from a database of data driven charts. The data driven charts describe digital terminal area procedure charts by way of data elements for each terminal area procedure chart including geodetic straights, arcs, text elements and symbols defined with respect to location. Some of the data elements are further defined with respect to altitude values assuming a standard atmospheric temperature value. The systems and methods include calculating compensated altitude values for the data elements of the retrieved data driven chart based on a deviation between the outside air temperature value and the standard atmospheric temperature value. The methods and systems include generating a presentation for a display device of the aircraft of the terminal area procedure chart.
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公开(公告)号：US20210327282A1
公开(公告)日：2021-10-21
申请号：US16932517
申请日：2020-07-17
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Raghu Shamasundar , Mohan Chandrashekarappa , Philip Toews , Robert Brownlee , Srihari Jayathirtha , Kalimullah Khan , Kiran Venkataramana
Abstract: An avionics system in an aircraft for providing flight data from an onboard flight management computer (FMC) to requesting applications is disclosed. The system includes a flight management system (FMS) service layer executing on the FMC on a thread separate from a thread that executes FMS core functions. The FMS service layer provides a FMC networked node server for responding to queries from a plurality of external applications for data generated from the FMS core functions without interrupting the FMS core functions. The FMC networked node server is configured to: receive a request from a client application using a server specified API for data elements from a specified input flight plan; retrieve the specified input flight plan from the FMS core functions; extract the requested data elements; and output the requested data elements to the client application without affecting the active thread that executes FMS core functions.
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