DATA CONCENTRATION SYSTEM

A distributed system for monitoring an aircraft or a gas turbine engine for an aircraft with many sense devices positioned at different locations. Data acquisition units receive an electric signal from one sense device, or a plurality of electric signals from various sense devices, convert it or the...

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Bibliographische Detailangaben
Hauptverfasser:	Pichon, Bertrand, Mazouni, Sophiane, Blouët, Christophe, Corne, Adrien, Brodard, Pierre-Alain, Vez, Dominique
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AVIATION BLASTING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ENGINE PLANTS IN GENERAL GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A distributed system for monitoring an aircraft or a gas turbine engine for an aircraft with many sense devices positioned at different locations. Data acquisition units receive an electric signal from one sense device, or a plurality of electric signals from various sense devices, convert it or them to digital sensor data. The data acquisition units have access to a digital network, which is an integral part of the distributed system of the invention and enables the transmission and distribution of the digital sensor data in this manner. The invention can use several digital networks.