Honeywell International Inc.

Greg Carlucci

Richard Snyder

Mark Pearson

Sripathi Ramachandra

Balaji Vasan Srinivasan

Mohammed Ibrahim Mohideen

Mitch Fletcher

Ted Bonk

William Todd Smithgall

Karel Mundel

PraveenKumar Ayyathurai

Udipi Ranga Ananthram

Hyden Lopez

Samrat Kar

Christopher Raj Mariadoss

Balaji Srinivasan

Methods and systems are provided for presenting an energy state associated with an aircraft with respect to an operating envelope region for a procedure to restart an engine of the aircraft. One method involves providing a graphical user interface display having a first reference axis corresponding to a first energy state parameter and a second reference axis corresponding to a second energy state parameter different from the first energy state parameter, providing a graphical representation of an operating envelope region associated with a procedure for starting an engine of the aircraft with respect to the first and second reference axes, obtaining current values for the first and second energy state parameters for the aircraft, and providing a graphical representation of the aircraft positioned with respect to the first and second reference axes based on the current values for the first and second energy state parameters.

Engine relight visualization methods and systems

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.

Custom search queries for flight data

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.

Multi-dimensional uni-vectored flight display for aircraft

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.

Multiple flight data reference for a specific selection on a vertical and lateral display

A node comprises a host computer operable to execute application tasks and to transmit data; a local time-triggered Ethernet switch operable to enforce temporal constraints on time-triggered data; and a time-triggered Ethernet controller coupled to the local time-triggered Ethernet switch and operable to be coupled to a time-triggered Ethernet switch in each of a plurality of other control nodes. The time-triggered Ethernet controller is further operable to communicate with the plurality of other control nodes to synchronize a local clock to establish a global time base and to provide a signal to the host computer for the host computer to synchronize execution of the application tasks by the host computer with the execution of application tasks in each of the plurality of other control nodes.

System and method for a cross channel data link

Growing community of inventors

Phoenix, AZ, United States of America

Greg Carlucci