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11.发明授权公开(公告)号：US11341861B2
公开(公告)日：2022-05-24
申请号：US16183272
申请日：2018-11-07
Applicant: Honeywell International Inc.
Inventor： Sivakumar Kanagarajan , Jason Marcel Garde , Visvanathan Thanigai Nathan , Amrit Kaur Mann
Abstract: Systems and methods are disclosed for environmental data sharing and context-based relevance determination. One method comprises receiving, by an environmental condition response system of a receiving vehicle, environmental data associated with a sending vehicle. Then, the environmental condition response system of the receiving vehicle analyzes the received environmental data for relevance based on contextual information of the receiving vehicle. Based on determining that the received environmental data is relevant to the receiving vehicle, the environmental condition response system determines a remedial action and sends instructions to perform the remedial action to a corresponding vehicle component system of the receiving vehicle.
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公开(公告)号：US10366615B2
公开(公告)日：2019-07-30
申请号：US16103628
申请日：2018-08-14
Applicant: Honeywell International Inc.
Inventor： Mohan Gowda Chandrashekarappa , Visvanathan Thanigai Nathan , Mohammed Ibrahim Mohideen , Pranav Patel
IPC: G06K9/00 , G08G5/00 , G08G5/04 , H04N5/00 , B64D43/00 , B64D45/04 , G01C21/32 , G01C23/00 , G06T11/60
Abstract: A method of operating an augmented reality processed terrain and obstacle threat scouting service is provided. The method includes using at least one sensor of a monitoring vehicle to monitor terrain and obstacle data. The monitored terrain and obstacle data is compared with terrain and obstacle data in a terrain and obstacle database. A non-validated georeferenced delta is determined when the comparison of the monitored terrain and obstacle data with terrain and obstacle data in the terrain and obstacle database finds non-matching terrain and obstacle data. The non-validated georeferenced delta is transmitted to a ground distribution center, consumer vehicle and/or cloud based server. Non-validated georeferenced delta received at a consumer vehicle is differentiated from other terrain and obstacle data on a synthetic vision display. Non-validated georeferenced delta received at a ground distribution center is validated against at least one other source and validated and non-validated is distributed to subscribing consumers.
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公开(公告)号：US09643735B2
公开(公告)日：2017-05-09
申请号：US14722931
申请日：2015-05-27
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Ratan Khatwa , Sivakumar Kanagarajan , Visvanathan Thanigai Nathan
CPC classification number: B64D45/04 , B60T8/1703 , B64D45/00 , G05D1/0083 , G08G5/0013 , G08G5/0021 , G08G5/0091 , G08G5/025
Abstract: Flight deck systems are provided for integrating braking action information with flight deck runway functions. In one embodiment, the flight deck system includes a cockpit display device on which an airport display, such as a two dimensional or three dimensional Airport Moving Map, is generated. A controller is coupled to the cockpit display device and configured to produce a braking action graphic on the airport display indicative of the current braking action of a first runway approached for usage by the aircraft. The controller may determine the current braking action of the runway from braking action information received over a datalink. Further, in certain embodiments, the controller can assign the current braking action of the runway to a predetermined braking action category and produce the braking action graphic to visually identify the assigned braking action category.
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公开(公告)号：US09096330B2
公开(公告)日：2015-08-04
申请号：US14569853
申请日：2014-12-15
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Visvanathan Thanigai Nathan , Thanga Anandappan
IPC: G01C23/00 , G01P5/175 , B64D43/02 , G01P3/62 , G01P5/16 , G01P21/00 , G01P3/50 , G01P21/02 , G01P13/02
CPC classification number: B64D43/02 , G01C23/00 , G01P3/50 , G01P3/62 , G01P5/16 , G01P5/175 , G01P13/025 , G01P21/00 , G01P21/025
Abstract: A system and method are provided for calculating Mach number and true airspeed without reference to data from a pitot static sensor. The true airspeed and Mach number are calculated using the altitude information from GPS, IRS, Radio Altimeter and other onboard sensors other than the air data computer (ADC). The computed true airspeed or Mach number could be used to confirm the ADC information or in lieu of the ADC information when the ADC information is unreliable or unavailable.
Abstract translation: 提供了一种用于计算马赫数和真实空速的系统和方法，而不参考皮托静态传感器的数据。 使用GPS，IRS，无线电高度计和其他非空中数据计算机（ADC）板载传感器的高度信息计算真实的空速和马赫数。 当ADC信息不可靠或不可用时，计算的真实空速或马赫数可用于确认ADC信息或代替ADC信息。
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公开(公告)号：US08914164B1
公开(公告)日：2014-12-16
申请号：US13958307
申请日：2013-08-02
Applicant: Honeywell International Inc.
Inventor： Visvanathan Thanigai Nathan , Thanga Anandappan
CPC classification number: B64D43/02 , G01C23/00 , G01P3/50 , G01P3/62 , G01P5/16 , G01P5/175 , G01P13/025 , G01P21/00 , G01P21/025
Abstract: A system and method are provided for calculating Mach number and true airspeed without reference to data from a pitot static sensor. The true airspeed and Mach number are calculated using the altitude information from GPS, IRS, Radio Altimeter and other onboard sensors other than the air data computer (ADC). The computed true airspeed or Mach number could be used to confirm the ADC information or in lieu of the ADC information when the ADC information is unreliable or unavailable.
Abstract translation: 提供了一种用于计算马赫数和真实空速的系统和方法，而不参考皮托静态传感器的数据。 使用GPS，IRS，无线电高度计和其他非空中数据计算机（ADC）板载传感器的高度信息计算真实的空速和马赫数。 当ADC信息不可靠或不可用时，计算的真实空速或马赫数可用于确认ADC信息或代替ADC信息。
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Patent Agency Ranking
公开(公告)号：US11074819B2
公开(公告)日：2021-07-27
申请号：US16373089
申请日：2019-04-02
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Muthusankar Subramaniyan , Visvanathan Thanigai Nathan , Raghu Shamasundar , Vijayvenkatesh Srinivasan
Abstract: A method and system for providing cost data via an operating cost app for a flight associated with a flight plan, by a computing device including: obtaining cost data of the flight plan by executing the operating cost app to implement an operating cost integrator application integrated with the operating cost app to interface with a plurality of service providers for retrieving operating cost data of the flight plan from each of the service providers; obtaining, by the at least one processor, real-time aircraft performance parameters affecting the actual cost of the flight including: a landing time and a takeoff time; determining an actual cost of the flight by using software solutions of the operating cost app, and by calculating ground charges at the airport derived from the sensed data by the operating cost app and presenting the actual cost of the ground charge, via a display device for displaying.
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公开(公告)号：US10089894B1
公开(公告)日：2018-10-02
申请号：US15691581
申请日：2017-08-30
Applicant: Honeywell International Inc.
Inventor： Mohan Gowda Chandrashekarappa , Visvanathan Thanigai Nathan , Mohammed Ibrahim Mohideen , Pranav Patel
Abstract: A method of operating an augmented reality processed terrain and obstacle threat scouting service is provided. The method includes using at least one sensor of a monitoring vehicle to monitor terrain and obstacle data. The monitored terrain and obstacle data is compared with terrain and obstacle data in a terrain and obstacle database. A non-validated georeferenced delta is determined when the comparison of the monitored terrain and obstacle data with terrain and obstacle data in the terrain and obstacle database finds non-matching terrain and obstacle data. The non-validated georeferenced delta is transmitted to a ground distribution center, consumer vehicle and/or cloud based server. Non-validated georeferenced delta received at a consumer vehicle is differentiated from other terrain and obstacle data on a synthetic vision display. Non-validated georeferenced delta received at a ground distribution center is validated against at least one other source and validated and non-validated is distributed to subscribing consumers.
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18.发明申请公开(公告)号：US20160347473A1
公开(公告)日：2016-12-01
申请号：US14722931
申请日：2015-05-27
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Ratan Khatwa , Sivakumar Kanagarajan , Visvanathan Thanigai Nathan
CPC classification number: B64D45/04 , B60T8/1703 , B64D45/00 , G05D1/0083 , G08G5/0013 , G08G5/0021 , G08G5/0091 , G08G5/025
Abstract: Flight deck systems are provided for integrating braking action information with flight deck runway functions. In one embodiment, the flight deck system includes a cockpit display device on which an airport display, such as a two dimensional or three dimensional Airport Moving Map, is generated. A controller is coupled to the cockpit display device and configured to produce a braking action graphic on the airport display indicative of the current braking action of a first runway approached for usage by the aircraft. The controller may determine the current braking action of the runway from braking action information received over a datalink. Further, in certain embodiments, the controller can assign the current braking action of the runway to a predetermined braking action category and produce the braking action graphic to visually identify the assigned braking action category.
Abstract translation: 飞行甲板系统用于将制动动作信息与飞行甲板跑道功能相集成。 在一个实施例中，驾驶舱系统包括驾驶舱显示装置，在其上生成诸如二维或三维机场移动地图的机场显示。 控制器耦合到驾驶舱显示设备并且被配置为在机场显示器上产生指示飞机接近接近的第一跑道的当前制动动作的制动动作图形。 控制器可以通过数据链路接收的制动动作信息来确定跑道的当前制动动作。 此外，在某些实施例中，控制器可以将跑道的当前制动动作分配到预定的制动动作类别，并产生制动动作图形以目视识别所分配的制动动作类别。
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公开(公告)号：US20150100184A1
公开(公告)日：2015-04-09
申请号：US14569853
申请日：2014-12-15
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Visvanathan Thanigai Nathan , Thanga Anandappan
CPC classification number: B64D43/02 , G01C23/00 , G01P3/50 , G01P3/62 , G01P5/16 , G01P5/175 , G01P13/025 , G01P21/00 , G01P21/025
Abstract: A system and method are provided for calculating Mach number and true airspeed without reference to data from a pitot static sensor. The true airspeed and Mach number are calculated using the altitude information from GPS, IRS, Radio Altimeter and other onboard sensors other than the air data computer (ADC). The computed true airspeed or Mach number could be used to confirm the ADC information or in lieu of the ADC information when the ADC information is unreliable or unavailable.
Abstract translation: 提供了一种用于计算马赫数和真实空速的系统和方法，而不参考皮托静态传感器的数据。 使用GPS，IRS，无线电高度计和其他非空中数据计算机（ADC）板载传感器的高度信息计算真实的空速和马赫数。 当ADC信息不可靠或不可用时，计算的真实空速或马赫数可用于确认ADC信息或代替ADC信息。
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公开(公告)号：US08849480B2
公开(公告)日：2014-09-30
申请号：US13781961
申请日：2013-03-01
Applicant: Honeywell International Inc.
Inventor： Frank Rajkumar Elias , Visvanathan Thanigai Nathan
Abstract: A system for validating ground determination of gross weight of aircraft includes sensor(s) that generates information regarding ground determination of gross weight while parked at parking bay; processing device that receives information regarding ground determination of gross weight of the aircraft from sensor(s); and computer memory communicatively coupled to processing device. Processing device determines ground determination based on information regarding ground determination of gross weight generated by sensor. Processing device determines gross weight in air after takeoff based on indicated airspeed, angle of attack, and thrust applied to aircraft. Processing device determines error between ground determination and air determination of gross weight taking into account reduction in gross weight due to fuel consumed since receiving ground determination. Processing device updates information regarding relationship between ground determination and air determination of gross weight. Computer memory stores updated information regarding relationship for use next time aircraft parks at parking bay.
Abstract translation: 用于验证飞机总重量的地面确定的系统包括在停放在停车室时产生关于总重量的地面确定的信息的传感器; 处理装置，其接收关于来自传感器的飞行器总重量的地面确定的信息; 以及通信地耦合到处理设备的计算机存储器。 处理装置基于关于由传感器产生的总重量的地面确定的信息来确定地面确定。 加工装置根据指示的空速，迎角和向飞机施加的推力，确定起飞后空气中的总重量。 考虑到从接收地面确定以来燃料消耗的毛重减少，处理装置确定地面确定和总重量空气确定之间的误差。 处理装置更新关于地面确定与总重量的空气确定之间的关系的信息。 计算机存储器存储有关下一次在停车场的飞机停放时使用关系的更新信息。
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