The Boeing Company

John Patrick Baron

Steven J Avila

Daniel J Ellis

Antonio Sanchez

Steve J Avila

Nha Thanh Nguyen

Khashayar Borumand

Ryan Kevin Torgerson

Timothy Allen Caviness

Randy L Parrott

Darin Richard Pankratz

Severn T Allen

An aircraft interface device comprising two or more data interface devices, an external data transceiver, a power module, a domain switch, and a controller is disclosed. The two or more data interface devices communicate data, the external data transceiver communicate to an external communication device, and the power module provides power to the two or more data interface devices and the external data transceiver. The two or more data interface devices comprise a first data interface device that communicates with avionics equipment when the first data interface device is powered and a second data interface device that communicates with non-avionics equipment when the second data interface device is powered. The domain switch selectively provides power from the power module to at least one of the two or more data interface devices. The controller provides a data communication path between the selectively powered data interface device and the external data transceiver for the external communication device.

Aircraft interface device

A method and system for an electrically switchable window system for an aerospace vehicle. The electrically switchable window system comprises electrically switchable windows and a window controller system connected to the electrically switchable windows. The window controller system receives a group of wireless signals from an onboard network system that controls systems in the aerospace vehicle and changes voltages applied to the electrically switchable windows when the group of wireless signals are received. The changes in the voltages change an amount of light passing through the electrically switchable windows.

Wirelessly controlled electrically switchable window system

Systems and methods according to one or more embodiments are provided for universal aircraft broadband control within an aircraft flight deck. In one example, a system includes a control panel and a switch coupled to the control panel. The system further includes a controller coupled to the switch and configured to determine a switch position based on a switch position signal associated with a position of the switch, receive a conditioned aircraft signal associated with parameters of an aircraft, and provide a controller control signal to control whether transmissions occur from an aircraft antenna based on at least one of the switch position signal and the conditioned aircraft signal.

Universal broadband control panel systems and methods

Systems and methods according to one or more embodiments are provided for an aircraft flight crew secure communication path to multiple aircraft data domains. In one example, a system includes one or more data interface devices configured to communicate data. A power module is configured to provide power to the one or more data interface devices, and a switch coupled between the power module and each of the one or more data interface devices is configured to selectively provide power from the power module to at least one of the one or more data interface devices. A data transceiver is configured to couple to an external communication device, and a controller coupled between the one or more data interface devices and the data transceiver is configured to provide a data communication path between the selectively powered data interface device and the data transceiver for the external communication device.

Flight crew connectivity systems and methods

The present disclosure provides a system, method, and apparatus for a virtual trainer for a control panel for a vehicle. In one or more embodiments, the disclosed system comprises a device with a screen, where the virtual trainer is loaded onto the device, and the virtual trainer is to display, on the screen of the device, available selections relating to different functions for the vehicle, as shown on the control panel for the vehicle. In one or more embodiments, the vehicle is a multi-passenger vehicle. In at least one embodiment, the vehicle is an aircraft, a terrestrial vehicle, or a marine vehicle. In some embodiments, the device is mobile or stationary. In one or more embodiments, the device is a tablet device and/or the control panel itself. In at least one embodiment, the screen of the device is a touch screen.

Attendant control panel virtual trainer

A method and apparatus for retrofitting an aircraft. Connection points for a reinforcement structure are located. The reinforcement structure is associated with the airframe during original manufacturing of the aircraft and accommodates forces from an antenna system attached to the reinforcement structure. The antenna system includes an antenna selected from a plurality of types of antennas. An antenna adapter plate in the antenna system is attached to the reinforcement structure connected to the airframe of the aircraft during the original manufacturing of the aircraft using the connection points. The antenna is attached to the antenna adapter plate, wherein the antenna adapter plate is configured to receive any one of the plurality of types of antennas. The reinforcement structure is configured to handle loads from any one of the plurality of types of antennas and the antenna adapter plate attached to the connection points.

Growing community of inventors

Bothell, WA, United States of America

John Patrick Baron