Honeywell International Inc.

Philip Toews

Robert Brownlee

Richard Snyder

Raghu Shamasundar

Daniel Eugene Lewis

Srihari Jayathirtha

Kalimulla Khan

Rajeev Mohan

Mohan Gowda Chandrashekarappa

Kiran Mancheiah Venkataramana

Mark Pearson

Mahesh Sivaratri

Sreenivasan Govindillam K

Susan L McCullough

Ravikumar Selvarajan

John Beckwith

Todd Wisner

Lior Attias

Salvatore Bottiglieri

Helen Edelson

Parker LeBlanc

Kalimullah Khan

I-Ping Fessler

Vehicle systems and methods are provided for updating vehicle systems in response to an update event at one of the vehicle systems, such as, for example, an update at a flight management system (FMS) of an aircraft. One method involves the FMS obtaining event data from an external source indicative of an update event, updating flight data at the FMS to an updated state based at least in part on the event data, and then adding the event data to an event queue after updating the flight data at the FMS to the updated state. One or more other vehicle systems can asynchronously retrieve the event data from the event queue and independently update in response to the event data.

Vehicle systems and methods for nonsynchronous redundancy management

Methods, systems, and apparatuses are provided for flight management to configure an aircraft configuration (config) file accessible by the avionic system wherein an avionic service is implemented by a flight management system (FMS) for corroborating allowance of access using one of a set of validation procedures for corroboration prior to execution of a request for content to the config file including validating that a user request for a session is authorized based on user identification data, that a client request by an Electronic Flight Bag (EFB) application for a session is authorized based on client identification data, and in response to the client request, determining that an EFB application request is encrypted and performing a decrypt procedure of the EFB application request based on private key data of a private key; and encrypting an EFB application response based on public key data of a public key from the config file.

Methods, systems and apparatuses to configure a flight management system (FMS)

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.

Distributed connected aircraft cockpit flight management system as a network node with API service capabtilities

A system includes an aircraft avionics system and a portable computing device. The aircraft avionics system is configured to run one or more embedded avionics applications. The portable computing device is in operable communication with the aircraft avionics system and is configured to run one or more portable device applications. Each portable device application has resident therein a software development kit having libraries and utilities that enables the portable device application to: establish a secure connection with the aircraft avionics system, establish and maintain a required protocol with the embedded avionics application, and communicate with the embedded avionics application as specified by an application programming interface definition.

System and method to facilitate communication of an application resident on a portable computing device with an application resident in aircraft avionics

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.

System and method for offboard validation of variable parameters

Systems and methods are disclosed for brokering data exchanges between on-board and off-board systems of a vehicle. One method comprises receiving, at a data broker engine, one or more data requests from an origination system, wherein each of the one or more data requests specifies at least one or more of a request type and a target system. Then the data broker engine determines whether the request type is a one-time transmission, a periodic transmission, an event-triggered transmission, or a change-triggered transmission. Following the determination, the data broker engine retrieves data from the target system based on the determined request type and transmits the data to the origination system.

Data broker engine for managing data exchanges between on-board and off-board systems

Methods and systems are provided for accessing data in a networked system. In one embodiment, a method includes: receiving a request for information from a first system; evaluating a display system to determine a communication request to be generated to obtain the information; and generating a request to a second system based on the communication request.

Methods and systems for non-intrusive system data pipe

A keyboard module configured for use in an avionics touchscreen system is disclosed. The keyboard module is configured to display, via a visual display in the avionics touchscreen system and responsive to a selection of an application program generated widget for focus via a touchscreen surface in the avionics touchscreen system, a virtual keyboard. The virtual keyboard includes a text box widget configured to display clip data stored in clipboard memory provided by the avionics touchscreen system, a copy widget configured to cause data in a first widget provided by the application program that is in focus to be copied to the clipboard memory, and a paste widget configured to cause the clip data in the clipboard memory and displayed in the text box widget to be pasted to a second widget provided by the application program that is in focus.

System and method of providing clipboard cut and paste operations in an avionics touchscreen system

Growing community of inventors

Phoenix, AZ, United States of America

Philip Toews