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: 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.