公开(公告)号：US20210020055A1

公开(公告)日：2021-01-21

申请号：US16513442

申请日：2019-07-16

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Suresh Bazawada ,  Anil Kumar Songa ,  Vasudev Prakash Shanbhag ,  Anish Kumar Michaelas ,  Sai Phanidhar ,  Kanagaraj Karuppusamy ,  Siddaray Medegar ,  Harish M

IPC: G08G5/00 ,  B64D43/00

Abstract: Methods and systems are provided for presenting unmanned vehicles, such as drones, operating in the vicinity of a planned route of travel. One exemplary method involves displaying a graphical representation of a route for a vehicle on a display device onboard the vehicle, determining a range of an unmanned vehicle based on one or more signals associated with the unmanned vehicle, and displaying a graphical representation of the range of the unmanned vehicle on the display device when at least some of the range is within a threshold distance of the route.

公开(公告)号：US09401091B2

公开(公告)日：2016-07-26

申请号：US14026811

申请日：2013-09-13

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Mahesh Babu N ,  Suresh Bazawada

IPC: G08G3/02 ,  G08G5/04 ,  G08G7/02 ,  G08G9/02 ,  G08G5/00 ,  G01C23/00

CPC classification number: G08G3/02 ,  G01C23/00 ,  G08G5/0008 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0039 ,  G08G5/0052 ,  G08G5/0078

Abstract: A system and method for increasing the vertical situational awareness of a pilot of a host aircraft, comprises rendering symbology on a vertical situation display of the host aircraft, the symbology comprising (1) a traffic scenario including at least the host aircraft and a second aircraft, the second aircraft involved in an ITP transition, and (2) flight level allocation data assigned to the second aircraft by air traffic control.

Abstract translation: 一种用于增加主机飞行员的飞行员的垂直情境意识的系统和方法，包括对主机的垂直情况显示进行符号系统，所述符号系统包括（1）至少包括主机和第二飞行器的交通情景 ，涉及ITP转换的第二架飞机，以及（2）通过空中交通管制分配给第二架飞机的飞行高度分配数据。

公开(公告)号：US20160049080A1

公开(公告)日：2016-02-18

申请号：US14458882

申请日：2014-08-13

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Suresh Bazawada ,  Mahesh Babu N ,  Vasudev Prakash Shanbhag

IPC: G08G5/00

CPC classification number: G08G5/0013 ,  G08G5/0021 ,  G08G5/0039 ,  G08G5/0052 ,  G08G5/0078

Abstract: A method and apparatus is provided for reducing the ITP rejection ratio. After identifying a reference aircraft, the ITP criteria associated with the reference aircraft is evaluated. If the ITP transition time overlaps with a maneuver time of the reference aircraft, the ITP request is not transmitted. The flight plan of the reference aircraft is analyzed to detect an upcoming reference aircraft maneuver.

Abstract translation: 提供了一种降低ITP抑制比的方法和装置。 在确定参考飞机后，评估与参考飞机相关的ITP标准。 如果ITP转换时间与参考飞机的机动时间重叠，则不传输ITP请求。 分析参考飞机的飞行计划以检测即将到来的参考飞机机动。

公开(公告)号：US12208916B2

公开(公告)日：2025-01-28

申请号：US18069375

申请日：2022-12-21

Applicant: Honeywell International Inc.

Inventor： Sadguni Venkataswamy ,  Suresh Bazawada ,  Anil Kumar Songa ,  Mohammed Ibrahim Mohideen

IPC: B64D45/00 ,  G01C23/00 ,  B64C29/00

Abstract: A method of providing contextual display modes for a vertical takeoff and landing (VTOL) vehicle including obtaining aircraft flight information including a current position and altitude; retrieving vertiport information for a vertiport at the current position of the aircraft; displaying, to one or more operators of the aircraft, a takeoff synthetic vision display mode; transitioning, as the current altitude approaches the transitional altitude, from the takeoff synthetic vision display mode to a cruise synthetic vision display mode, wherein the cruise synthetic vision display mode represents the view from a cruise display viewpoint at the current altitude of the aircraft and at the current position of the aircraft; and displaying, in response to the current altitude equaling or exceeding the transitional altitude, the cruise synthetic vision display mode.

公开(公告)号：US20230222923A1

公开(公告)日：2023-07-13

申请号：US17655915

申请日：2022-03-22

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Anil Kumar Songa ,  Sadguni Venkataswamy ,  Siddaray Medegar ,  Suresh Bazawada ,  Candace Gunning

IPC: G08G5/00

CPC classification number: G08G5/0021 ,  G08G5/0013

Abstract: A flight deck system and method in an aircraft for enhancing controller pilot datalink communication (CPDLC) operation is disclosed. The flight deck system includes a controller configured to: receive a CPDLC message having a CPDLC message type from a flight operation center (FOC) having an FOC name; retrieve an expected response time for the CPDLC message from an expected response time database containing expected response times for a plurality of CPDLC message types for FOCs; generate a timer function that causes the display of a timer (e.g., countdown timer) on an aircraft display device that has a set duration based on the expected response time; signal the aircraft display device to display the timer; monitor communications from flight crew for a response to the CPDLC message; and signal the aircraft display device to end the display of the timer when a communication has been detected within the set duration.

公开(公告)号：US11107361B1

公开(公告)日：2021-08-31

申请号：US16993741

申请日：2020-08-14

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Anil Kumar Songa ,  Richard Mitchel Meldrum ,  Suresh Bazawada ,  Sadguni Venkataswamy ,  Dante Sadeghpour

IPC: G08G5/02 ,  G08G5/04

Abstract: Methods and systems for instrument landing system (ILS) alerting. The method may include: receiving an ILS localizer signal and traffic information; monitoring a signal-quality of the received ILS signal; annunciating on a display system onboard the aircraft an impending ILS auto-pilot disconnect alert when the signal-quality is determined to have decreased by more than a threshold; associating the ILS signal with stored ILS antenna information to thereby construct a three-dimensional ILS envelope with a point of origination at a location of an ILS localizer; presenting a map showing the aircraft at a current location, and the runway; and, using the traffic information to monitor a location and movement of an intruder traffic and predict an infringement of the intruder traffic on the ILS envelope. Responsive to the predicted infringement, the method may annunciate an ILS alert and transmit a notification to air traffic control or the intruder traffic.

公开(公告)号：US20210233412A1

公开(公告)日：2021-07-29

申请号：US17099911

申请日：2020-11-17

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Suresh Bazawada ,  Anil Kumar Songa ,  Jonathan Davis ,  Sadguni Venkataswamy

IPC: G08G5/00

Abstract: Provided are technologically improved systems and methods for reducing controller-pilot data link (CPDLC) rejection ratio on an aircraft. The system is programmed to receive a user provided tentative CPDLC request. The system receives traffic data from an external traffic data source and data from a navigation system and a sensor system. The system predicts whether the tentative CPDLC request will be accepted by air traffic control (ATC), based on the received data. The system further predicts a potential delay time until the ATC will accept the tentative CPDLC request. The system additionally provides one or more alternative CPDLC requests and their potential delay times when the system has predicted that the tentative CPDLC request will be rejected. The system displays this information and receives user selections based thereon. Upon receiving a user selection, a CPDLC request is sent to ATC in accordance with a predicted delay time.

公开(公告)号：US20160152351A1

公开(公告)日：2016-06-02

申请号：US14557845

申请日：2014-12-02

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Vasudev Prakash Shanbhag ,  Mahesh Babu N ,  Suresh Bazawada

IPC: B64F5/00 ,  G07C5/08 ,  G07C5/12 ,  G02B27/01

CPC classification number: G07C5/12 ,  G02B27/0093 ,  G02B27/017 ,  G02B27/0172 ,  G02B27/0179 ,  G02B2027/0127 ,  G02B2027/014 ,  G02B2027/0141 ,  G02B2027/0187 ,  G07C5/0808

Abstract: Systems and methods are disclosed for verifying a vehicle component. In various embodiments, a system for verifying a vehicle component may comprise a near-to-eye (NTE) display system that includes an NTE tracking controller, a controller communicatively coupled to the NTE tracking controller, and a component database communicatively coupled to the controller. The controller may be configured to receive component data from the component database and communicate the component data to the NTE tracking controller based upon focus data, where the focus data is based upon a head position of an operator.

Abstract translation: 公开了用于验证车辆部件的系统和方法。 在各种实施例中，用于验证车辆部件的系统可以包括近距离（NTE）显示系统，其包括NTE跟踪控制器，通信地耦合到NTE跟踪控制器的控制器以及通信地耦合到控制器的组件数据库 。 控制器可以被配置为从组件数据库接收组件数据，并且基于焦点数据将组件数据传送到NTE跟踪控制器，其中焦点数据基于操作者的头部位置。

公开(公告)号：US11769417B2

公开(公告)日：2023-09-26

申请号：US17024979

申请日：2020-09-18

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Anil Kumar Songa ,  Sabu Mathew ,  Suresh Bazawada ,  Sadguni Venkataswamy

IPC: G08G5/00 ,  G06F3/14 ,  B64D45/00 ,  B64D43/02 ,  G08G5/02

CPC classification number: G08G5/0047 ,  B64D43/02 ,  B64D45/00 ,  G06F3/14 ,  G08G5/003 ,  G08G5/006 ,  G08G5/0034 ,  G08G5/0039 ,  G08G5/025

Abstract: A method is provided for displaying information on a display device of an aircraft. The method comprises determining, by the processor, a first point along a flight path when a flight mode associated with a flight plan will be armed; determining, by the processor, a second point along the flight path when the flight mode associated with the flight plan will be engaged; determining, by the processor, a third point along the flight path when the flight mode associated with the flight plan will be disengaged; generating, by the processor, graphics data that represents the first point, the second point and the third point; incorporating, by the processor, the graphics data into a user interface that displays the flight path; and generating, by the processor, the user interface for display on the display device of the aircraft.

公开(公告)号：US20200312164A1

公开(公告)日：2020-10-01

申请号：US16365307

申请日：2019-03-26

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Suresh Bazawada ,  Anil Kumar Songa ,  Vasudev Prakash Shanbhag

IPC: G08G5/00 ,  G06F3/0484 ,  G06F3/0481

Abstract: Systems and methods for detecting and representing traffic maneuvers are provided. The method includes receiving traffic information for a neighbor traffic. The method may use the neighbor traffic information to calculate a volume around the neighbor traffic, defined by min max thresholds related to the traffic information. The traffic information is monitored until the default time elapses, to thereby determine a delta latitudinal position, a delta longitudinal position, a delta altitude, a delta pitch, and a delta roll, of the neighbor traffic during the default time; and a traffic maneuver is identified upon the occurrence of one or more of (i) the delta latitudinal position exceeded the maximum latitudinal threshold, (ii) the delta longitudinal position exceeded the maximum longitudinal threshold, and (iii) the delta altitude exceeded the magnitude of the maximum altitude threshold. An enhanced symbolic indicator of the traffic maneuver is rendered on a map image.