Abstract: In connection with processing asynchronous streams of aircraft telemetry data, data processing logic is developed to run on multiple aircraft, even if different avionics equipment are installed on the aircraft. An electronic inventory system tracks all data available on affected aircraft. A set of “global” data elements applicable to all aircraft in a fleet is defined and is tracked in the electronic inventory system, with relationship to the underlying native data elements and specific aircraft. The global units are derived as appropriate, for each specific aircraft avionics environment. An interface enables definition of data processing logic that is integrated with the electronic inventory system and ensures the general validity of the defined logic. The data processing logic is deployed to one or more aircraft in a function integrated with the electronic inventory system, to ensure the validity of the data processing logic for each aircraft specified as a deployment target.

Abstract: The power supply and cooling provided by existing aircraft system line replaceable units (LRUs) or other devices supports new cards that are installed in previously empty slots or which replace existing original cards and which are not limited in functionality and do not require licensing of any proprietary technology included in the LRU. These new cards can include components such as processors, memory, and/or storage that significantly improve the performance of the LRU, and/or add new functionality—all without exceeding the power supply and cooling capability of the LRU. A network and avionics bus interface can be added to a portion of the new card and electrically coupled to the circuitry and electronic components on the new card, so that one or more cables connected to the interface can be connected to externally accessible standard avionics buses and network connectors added to a chassis of the LRU.

Abstract: A global, broadband communications and computing system Platform for commercial aircraft selects a “current best” communication link from multiple available links. Onboard network access components, such as Wi-Fi and GSM pico-cells, enable wired/wireless devices to use the aircraft's broadband communications links. The Platform uses virtualization and distributed systems computing technology to create a system of systems that extends an airline company's ground communications and computing systems server(s) onboard aircraft in the fleet, regardless of model, age, or manufacturer. The Platform can host airline operational applications and services onboard the aircraft. An onboard system collects data from multiple aircraft systems, tags it with trusted time and origin metadata, and securely transmits it to a ground portion of the Platform in real time (or as links are available), and receives data for distribution to appropriate onboard systems.

Abstract: The power supply and cooling provided by existing aircraft system line replaceable units (LRUs) or other devices supports new cards that are installed in previously empty slots or which replace existing original cards and which are not limited in functionality and do not require licensing of any proprietary technology included in the LRU. These new cards can include components such as processors, memory, and/or storage that significantly improve the performance of the LRU, and/or add new functionality—all without exceeding the power supply and cooling capability of the LRU. A network and avionics bus interface can be added to a portion of the new card and electrically coupled to the circuitry and electronic components on the new card, so that one or more cables connected to the interface can be connected to externally accessible standard avionics buses and network connectors added to a chassis of the LRU.