Honeywell International Inc.

Sandra J Howe-Ryberg

Darshan Gandhi

Thomas D Judd

David B Goldstein

David Lowell Miller

Sharon C Eaglestone

An aerospace communication system comprises a communication management unit; a first communication device configured to transmit and receive data over a first communication network; and a second communication device configured to transmit and receive data over a second communication network. The first communication device is coupled to a corresponding interface of the communication management unit. The second communication device is communicatively separated from the communication management unit by the first communication device such that the communication management unit is unaware of the second communication device. The first communication device includes routing logic configured to determine whether to send each message received from the communication management unit over the first communication network or to the second communication device for transmission over the second communication network.

SATCOM data unit with wireless device

A subassembly for an integrated wireless module is provided. The subassembly includes an integrated-wireless-module input/output (I/O) connector, a modem controller; at least one internal antenna, and at least two modem connectors communicatively coupled to the modem controller, the modem connectors configured to interface with at least two modems. The modem controller digitally selects to one of: communicatively couple one of the at least two modem connectors to one of the at least one internal antenna; communicatively couple one of the at least two modem connectors to the integrated-wireless-module I/O connector; and communicatively couple a first one of the at least two modem connectors to one of the at least one internal antenna and communicatively couple a second one of the at least two modem connectors to the integrated-wireless-module I/O connector.

Integrated wireless module

Systems and methods for aircraft on-ground determination are provided. In one embodiment, an onboard motion controlled wireless avionics datalink gateway comprises: a wireless radio chipset module; and a velocity interlock coupled to an aircraft motion sensor and the wireless radio chipset module. The wireless radio chipset module is configured to establish one or more intra-aircraft radio communication links with one or more onboard avionics system, and wherein the wireless radio chipset module is configure to establish one or more external radio communication links with at least one ground-based wireless communication system. The aircraft motion sensor is configured to output to the velocity interlock an aircraft motion signal indicative of a velocity of an aircraft in which the gateway is installed. The velocity interlock enables and disables the one or more intra-aircraft radio communication links and the one or more external radio communication links based on the aircraft motion signal.

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Renton, WA, United States of America

Sandra J Howe-Ryberg