公开(公告)号：US11386069B2

公开(公告)日：2022-07-12

申请号：US16716716

申请日：2019-12-17

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Philip Toews ,  Daniel E. Lewis ,  Richard Snyder ,  I-Ping Fessler ,  Robert Brownlee

IPC: G06F7/00 ,  G06F16/23 ,  G06F9/54 ,  H04L67/10

Abstract: A method in an aircraft for the validation of variable data is provided. The method comprises: receiving a request from an application program to retrieve data attributes for at least one data item to be entered via a GUI provided by the application program; requesting, from the flight management engine using an API, the data attributes for the at least one data item, wherein the data attributes identify at least one limit for data entry for the at least one data item including a minimum and/or maximum value for the at least one data item; receiving the requested data attributes from the flight management engine; and transmitting the data attributes to the application program; wherein the application program restricts data entry for the at least one data item in conformance with each limit provided by the data attributes for the at least one data item.

公开(公告)号：US11328610B2

公开(公告)日：2022-05-10

申请号：US16043854

申请日：2018-07-24

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Sripathi Ramachandra ,  Mark Pearson ,  Greg Carlucci ,  Richard Snyder

IPC: G08G5/00 ,  G06F16/9537 ,  B64D43/00

Abstract: Systems and methods of searching stored flight plan information using a custom search query including at least one aircraft parameter condition or environmental parameter condition. The systems and method include receiving, using a user interface module, a custom search query comprising an aircraft parameter condition or an environmental condition; searching, using a processor module, stored flight plan information for instances in the stored flight plan information that satisfy the aircraft parameter condition or environmental condition; and displaying, using a display module, the instances in the stored flight plan information that satisfy the aircraft parameter condition or environmental condition.

公开(公告)号：US11043130B2

公开(公告)日：2021-06-22

申请号：US16100763

申请日：2018-08-10

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Sripathi Ramachandra ,  Greg Carlucci ,  Richard Snyder ,  Mohammed Ibrahim Mohideen ,  Mark Pearson ,  Hyden Lopez ,  Christopher Raj Mariadoss

IPC: G08G5/00 ,  B64C13/04 ,  B64D43/00 ,  G06T11/00 ,  G06T11/20

Abstract: An aircraft and a method for operating the same may include, but is not limited to, a flight management system, a vertical situation display, and a processor configured to determine a first variable, a second variable and a third variable, determine flight plan data for the first, second and third variables, generate display data for the vertical situation display, the display data including the scale of the first second and third variables and a vector corresponding to the flight plan data of the first variable and second variable scaled to the first scale and the second scale, wherein the scale of the third variable is non-linear and varies based upon the flight plan data corresponding to the third variable relative to the vector, and output the generated display data to the vertical situation display for display on the vertical situation display.

公开(公告)号：US20210182274A1

公开(公告)日：2021-06-17

申请号：US16716716

申请日：2019-12-17

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Philip Toews ,  Daniel E. Lewis ,  Richard Snyder ,  I-Ping Fessler ,  Robert Brownlee

IPC: G06F16/23 ,  G06F9/54

Abstract: A method in an aircraft for the validation of variable data is provided. The method comprises: receiving a request from an application program to retrieve data attributes for at least one data item to be entered via a GUI provided by the application program; requesting, from the flight management engine using an API, the data attributes for the at least one data item, wherein the data attributes identify at least one limit for data entry for the at least one data item including a minimum and/or maximum value for the at least one data item; receiving the requested data attributes from the flight management engine; and transmitting the data attributes to the application program; wherein the application program restricts data entry for the at least one data item in conformance with each limit provided by the data attributes for the at least one data item.

公开(公告)号：US10797945B2

公开(公告)日：2020-10-06

申请号：US15884835

申请日：2018-01-31

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Phillip Toews ,  Rajeev Mohan ,  Ravish Udupa ,  Richard Snyder ,  Robert Brownlee ,  Brian Walter ,  Daniel E. Lewis

IPC: G06F15/177 ,  H04L12/24 ,  H04L29/08 ,  G08G5/00 ,  G06F15/00 ,  H04L29/06

Abstract: Methods for providing a flight management service in a cloud computing environment, the method includes: receiving, an object request by a server from a mobile device wherein the server is located in the cloud computing environment including: at least a flight management system (FMS) connected to a stateless object; processing, by the connected FMS hosted by the server, the object request generating a resource object for a particular flight plan wherein the resource object includes a data set; storing, by the connected FMS, the data set at the stateless object in the cloud environment; and sending, by the server, an object response from the connected FMS to the mobile device, for accessing the data set of the stateless object for the particular flight plan.

公开(公告)号：US20190279514A1

公开(公告)日：2019-09-12

申请号：US15912942

申请日：2018-03-06

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Sripathi Ramachandra ,  Mark Pearson ,  Greg Carlucci ,  Richard Snyder ,  Balaji Srinivasan

IPC: G08G5/00 ,  G01C23/00

Abstract: Methods and systems for a flight display system are provided. The method includes: commanding a vertical situation display (VSD) and a lateral navigation display (ND) to render, concurrently, a viewing segment of a flight plan. The method includes receiving a user input selecting a section of the viewing segment, the user input being received on only one of the VSD and the ND. The method continues by commanding, concurrently, the VSD and the ND to visually distinguish the section, and to demark the section on the VSD with starting points and ending points. The method identifies a flight parameter, and for the flight parameter, includes (a) determining which display, among the VSD and the ND, is appropriate for the rendering of flight parameter information; (b) generating flight parameter information based on (a); and (c) overlaying the flight parameter information on the appropriate display.

公开(公告)号：US20190213891A1

公开(公告)日：2019-07-11

申请号：US15867666

申请日：2018-01-10

Applicant: Honeywell International Inc.

Inventor： Richard Snyder ,  Rajeev Mohan ,  Rajesh Chaubey ,  Ravish Udupa ,  Sharanabasappa Advani

IPC: G08G5/00

CPC classification number: G08G5/0039 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0026 ,  G08G5/006 ,  G08G5/0078 ,  G08G5/0082 ,  G08G5/0091 ,  G08G5/025

Abstract: A system and methods for enhancing operator situational awareness are disclosed. For example, one method includes monitoring a plurality of radio transmissions associated with a plurality of vehicles in a first traffic flow pattern, monitoring a second traffic flow pattern in a vicinity of a vehicle of the plurality of vehicles, monitoring at least one weather value for a destination site for the plurality of vehicles, proposing a destination approach for the vehicle in response to the monitoring, evaluating an impact of the proposed destination approach on an existing travel path for the vehicle, and generating a second travel path for the vehicle in response to the evaluating.